ISO_16750-3-2007

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INTERNATIONAL ISOSTANDARD 16750-3

Second edition2007-08-01

Road vehicles — Environmental

conditions and testing for electrical and electronic equipment — Part 3:

Mechanical loads

Véhicules routiers — Spécifications d'environnement et essais des équipements électrique et électronique — Partie 3: Contraintes mécaniques

---`,,`,`,,`,,`-`-``,,```,`,```,,,,``,``,,,,```--Reference numberISO 16750-3:2007(E)

ISO 2007

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ISO 16750-3:2007(E)

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ISO 16750-3:2007(E)

Contents Page

Foreword............................................................................................................................................................iv 1 2 3 4 4.1 4.2 4.3 4.4 4.5 5 6

Scope.....................................................................................................................................................1 Normative references...........................................................................................................................1 Terms and definitions...........................................................................................................................1 Tests and requirements.......................................................................................................................2 Vibration................................................................................................................................................2 Mechanical shock...............................................................................................................................19 Free fall................................................................................................................................................21 Surface strength/scratch and abrasion resistance.........................................................................22 Gravel bombardment..........................................................................................................................22 Code letters for mechanical loads....................................................................................................22 Documentation....................................................................................................................................22

--```,,,,``,``,,,,```,`,```,,``-`-`,,`,,`,`,,`---Annex A (informative) Guideline for the development of test profiles for vibration tests........................24 Annex B (informative) Recommended mechanical requirements for equipment depending on the

mounting location...............................................................................................................................35 Bibliography.....................................................................................................................................................36

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iii

ISO 16750-3:2007(E)

Foreword

ISO (the International Organization for Standardization) is a worldwide federation of national standards bodies (ISO member bodies). The work of preparing International Standards is normally carried out through ISO technical committees. Each member body interested in a subject for which a technical committee has been established has the right to be represented on that committee. International organizations, governmental and non-governmental, in liaison with ISO, also take part in the work. ISO collaborates closely with the International Electrotechnical Commission (IEC) on all matters of electrotechnical standardization. International Standards are drafted in accordance with the rules given in the ISO/IEC Directives, Part 2. The main task of technical committees is to prepare International Standards. Draft International Standards adopted by the technical committees are circulated to the member bodies for voting. Publication as an International Standard requires approval by at least 75 % of the member bodies casting a vote.

Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. ISO shall not be held responsible for identifying any or all such patent rights.

ISO 16750-3 was prepared by Technical Committee ISO/TC 22, Road vehicles, Subcommittee SC 3, Electrical and electronic equipment.

This second edition cancels and replaces the first edition (ISO 16750-3:2003), which has been technically revised.

ISO 16750 consists of the following parts, under the general title Road vehicles — Environmental conditions and testing for electrical and electronic equipment: ⎯ Part 1: General ⎯ Part 2: Electrical loads ⎯ Part 3: Mechanical loads ⎯ Part 4: Climatic loads ⎯ Part 5: Chemical loads

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---`,,`,`,,`,,`-`-``,,```,`,```,,,,``,``,,,,```--INTERNATIONAL STANDARD ISO 16750-3:2007(E)

Road vehicles — Environmental conditions and testing for electrical and electronic equipment — Part 3:

Mechanical loads

1 Scope

This part of ISO 16750 applies to electric and electronic systems/components for road vehicles. This part of ISO 16750 describes the potential environmental stresses, and specifies tests and requirements recommended for the specific mounting location on/in the vehicle. This part of ISO 16750 describes the mechanical loads.

2 Normative references

The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies.

ISO 16750-1, Road vehicles — Environmental conditions and testing for electrical and electronic equipment — Part 1: General

ISO 16750-4, Road vehicles — Environmental conditions and testing for electrical and electronic equipment — Part 4: Climatic loads

IEC 60068-2-6, Environmental testing — Part 2: Tests — Test Fc: Vibration (sinusoidal) IEC 60068-2-14, Environmental testing — Part 2: Tests — Test N: Change of temperature IEC 60068-2-29, Environmental testing — Part 2: Tests — Test Eb and guidance: Bump IEC 60068-2-32, Environmental testing — Part 2: Tests — Test Ed: Free fall

IEC 60068-2-, Environmental testing — Part 2: Test methods — Test Fh: Vibration, broad-band random (digital control) and guidance

--```,,,,``,``,,,,```,`,```,,``-`-`,,`,,`,`,,`---3 Terms and definitions

For the purposes of this document, the terms and definitions given in ISO 16750-1 apply.

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ISO 16750-3:2007(E)

4 Tests and requirements

4.1 Vibration

4.1.1 General

The vibration test methods specified consider various levels of vibration severities applicable to on-board electrical and electronic equipment. It is recommended that vehicle manufacturer and supplier choose the test method, the environmental temperature and vibration parameters depending on the specific mounting location. The specified values apply to direct mounting in defined mounting locations. The use of a bracket for mounting can result in higher or lower loads. If the device under test (DUT) is used in the vehicle with a bracket, then all vibration and mechanical shock testing shall be done with this bracket.

Carry out the vibration test with the DUT suitably mounted on a vibration table. The mounting method(s) used shall be noted in the test report. Carry out the frequency variation by logarithmic sweeping of 0,5 octave/minute for sinusoidal tests and the sinusoidal part of sine on random tests. The objective of the recommended vibration tests is to avoid malfunctions and breakage mainly due to fatigue in the field. Testing for wear has special requirements and is not covered in this part of ISO 16750. Loads outside the designated test frequency ranges shall be considered separately.

NOTE Deviations from the load on the DUT can result if vibration testing is carried out in accordance with this part of ISO 16750 on a heavy and bulky DUT, as mounting rigidity and dynamic reaction on the vibrator table excitation are different compared to the situation in the vehicle. This deviation can be minimized by applying the average control method (see Annex A).

Application of the weighted average control method in accordance with IEC 60068-2- shall be agreed upon. Subject the DUT during the vibration test to the temperature cycle in accordance with IEC 60068-2-14, with electric operation in accordance with Figure 1. Alternatively, a test at constant temperature may be agreed between customer and supplier.

Operate the DUT electrically as indicated in Figure 1 at Tmin (short functional test after the DUT has reached Tmin completely). This functional test shall be as short as possible, i.e. only long enough to check the proper performance of the DUT. This minimizes self-heating of the DUT. Additional electrical operation of the DUT takes place between 210 min and 410 min of the cycle (see Figure 1). Additional drying of test chamber air is not permitted.

Because in the vehicle vibration stress can occur together with extremely low or high temperatures, this interaction between mechanical and temperature stress is simulated in the test, too. The failure mechanism is, for example, a plastic part of a system/component that mellows due to the high temperature and cannot withstand the acceleration under this condition.

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---`,,`,`,,`,,`-`-``,,```,`,```,,,,``,``,,,,```--ISO 16750-3:2007(E)

Key

T temperature, °C

t time, min a Operating mode 3.2 in accordance with ISO 16750-1.

b One cycle.

Figure 1 — Temperature profile for the vibration test

Table 1 — Temperature versus time for the vibration test

Duration Temperature

min °C 0 20 60 −40 150 −40 210 20 300 Tmax a 410

Tmax a

480 20 a For Tmax, see ISO 16750-4.

--```,,,,``,``,,,,```,`,```,,``-`-`,,`,,`,`,,`---4.1.2 Tests 4.1.2.1

Test I — Passenger car, engine

4.1.2.1.1 Purpose

This test checks the DUT for malfunctions and breakage caused by vibration. The vibrations of a piston engine can be split up into two kinds:

⎯ sinusoidal vibration that results from the unbalanced mass forces in the cylinders, and ⎯ random noise due to all other vibration-schemes of an engine, e.g. closing of valves.

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ISO 16750-3:2007(E)

In the lowest frequency range from 10 Hz to 100 Hz, the influence of rough-road conditions is taken into account. The main failure to be identified by this test is breakage due to fatigue.

NOTE Road profile usually has negligible impact on engine mounted components. Shock inputs are effectively isolated by the suspension of motor mounting systems.

--```,,,,``,``,,,,```,`,```,,``-`-`,,`,,`,`,,`---The test profiles specified in the following clauses (4.1.2.1.2 to 4.1.2.1.3) apply to loads generated by (four stroke) reciprocating engines.

It is recommended to perform this test as a mixed mode vibration test in accordance with IEC 60068-2-80. Alternatively these tests may be performed sequentially. 4.1.2.1.2 Test

4.1.2.1.2.1 Sinusoidal vibration

Perform the test in accordance with IEC 60068-2-6. Unlike in IEC 60068-2-6, a sweep rate of 0,5 octave/minute or less shall be used. Use a test duration of 22 h for each plane of the DUT.

NOTE The test duration is based on A.4. The temperature in the chamber is above room temperature (RT) at the end of the test (2,75 temperature cycles).

Use curve 1 in Table 2 and Figure 2 for DUT intended for mounting on engines with five cylinders or less. Use curve 2 in Table 2 and Figure 2 for DUT test intended for mounting on engines more than five cylinders or more.

Both curves may be combined to cover all engine types in one test.

Key

X frequency, Hz Y maximum acceleration, m/s2 1 2

curve 1 (u five cylinders) curve 2 (> five cylinders)

Figure 2 — Vibration severity curves

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ISO 16750-3:2007(E)

Table 2 — Values for maximum acceleration versus frequency

Curve 1

(see Figure 2)

Maximum

Frequency

acceleration

Hz 100 200 240 m/s2 100 200 200

Curve 2

(see Figure 2)

Maximum

Frequency

acceleration

m/s2 100 150 150

Combination

Frequency

Maximum acceleration

m/s2 100 150 200

Hz 100 150 440 Hz 100 150 200 270 100 440 100

240 200 255 150 440 150

4.1.2.1.2.2 Random vibration

Perform the test in accordance with IEC 60068-2-. Use a test duration of 22 h for each plane of the DUT.

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The r.m.s. acceleration value shall be 181 m/s2.

The power spectral density (PSD) versus frequency is illustrated in Figure 3 and Table 3.

NOTE

The PSD values (random vibration) are reduced in the frequency range of the sinusoidal vibration test.

Key

X frequency, Hz

Y power spectral density, (m/s2)2/Hz

Figure 3 — PSD of acceleration versus frequency

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ISO 16750-3:2007(E)

Table 3 — Values for frequency and PSD

Frequency

PSD Hz

(m/s2)2/Hz

10 10 100 10 300 0,51 500 20 2 000

4.1.2.1.3 Requirement Breakage shall not occur.

As defined in ISO 16750-1, functional status class A is required during operating mode 3.2, and functional status class C during periods with other operating modes. 4.1.2.2

Test II — Passenger car, gearbox

4.1.2.2.1 Purpose

This test checks the DUT for malfunctions and breakage caused by vibration.

The vibrations of a gearbox can be split up into two kinds, which result partly from sinusoidal vibration from unbalanced mass forces of the engine (e.g. dominating orders) in the frequency range from 100 Hz to 440 Hz, and vibration from the friction of the gear wheels and other schemes, which are tested in the random part. In the lowest frequency range from 10 Hz to 100 Hz, the influence of rough-road conditions is taken into account. The main failure to be identified by this test is breakage due to fatigue.

The test profiles specified in the following clauses apply to loads generated by gearbox vibrations. Changing the gears can create additional mechanical shock and shall be considered separately.

It is recommended to perform this test as a mixed mode vibration test in accordance with IEC 60068-2-80. Alternatively these tests may be performed sequentially. 4.1.2.2.2 Test

4.1.2.2.2.1 Sinusoidal vibration

Perform the test in accordance with IEC 60068-2-6. Unlike in IEC 60068-2-6, a sweep rate of 0,5 octave/minute or less shall be used. Use a test duration of 22 h for each plane of the DUT.

NOTE The test duration is based on A.4. The temperature in the chamber is above RT at the end of the test (2,75 temperature cycles).

The amplitude versus frequency is illustrated to in Figure 4 and Table 4.

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---`,,`,`,,`,,`-`-``,,```,`,```,,,,``,``,,,,```--ISO 16750-3:2007(E)

Key

X frequency, Hz Y maximum acceleration, m/s2

Figure 4 — Maximum versus frequency

Table 4 — Values for maximum acceleration versus frequency

Frequency

Maximum acceleration

m/s2

100 30 200 60 440 60

4.1.2.2.2.2 Random vibration

Perform the test in accordance with IEC 60068-2-. Use a test duration of 22 h for each plane of the DUT. The r.m.s. acceleration value shall be 96,6 m/s2.

--```,,,,``,``,,,,```,`,```,,``-`-`,,`,,`,`,,`---NOTE The PSD values (random vibration) are reduced in the frequency range of the sinusoidal vibration test.

The PSD versus frequency is illustrated to in Figure 5 and Table 5.

Key

X frequency, Hz

Y power spectral density, (m/s2)2/Hz

Figure 5 — PSD of acceleration versus frequency

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ISO 16750-3:2007(E)

Table 5 — Values for frequency and PSD

Frequency

PSD (m/s2)2/Hz

10 10 100 10 300 0,51 500 5 2 000

4.1.2.2.3 Requirement Breakage shall not occur.

As defined in ISO 16750-1, functional status class A is required during operating mode 3.2, and functional status class C during periods with other operating modes. 4.1.2.3

Test III — Passenger car, flexible plenum chamber

--```,,,,``,``,,,,```,`,```,,``-`-`,,`,,`,`,,`---4.1.2.3.1 Purpose

This test checks the DUT for malfunctions and breakage caused by vibration.

This test is applicable to equipment to be mounted on a flexible plenum chamber but not rigidly attached. The vibrations in this mounting location are sinusoidal and mainly induced by the pulsation of the intake air. The main failure to be identified by this test is breakage due to fatigue. 4.1.2.3.2 Test

Perform the test in accordance with IEC 60068-2-6. Unlike in IEC 60068-2-6, a sweep rate of 0,5 octave/minute or less shall be used. Use a test duration of 22 h for each plane of the DUT.

NOTE The test duration is based on A.4. The temperature in the chamber is above RT at the end of the test (2,75 temperature cycles).

The amplitude versus frequency is illustrated in Figure 6 and Table 6.

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ISO 16750-3:2007(E)

--```,,,,``,``,,,,```,`,```,,``-`-`,,`,,`,`,,`---Key

X frequency, Hz

Y maximum acceleration, m/s2

Figure 6 — Maximum acceleration versus frequency

Table 6 — Values for maximum acceleration versus frequency

Frequency

Maximum acceleration

m/s2

100 90 200 180 325 180 500 80 1 500

4.1.2.3.3 Requirement Breakage shall not occur.

As defined in ISO 16750-1, functional status class A is required during operating mode 3.2, and functional status class C during periods with other operating modes. 4.1.2.4

Test IV — Passenger car, sprung masses (vehicle body)

4.1.2.4.1 Purpose

This test checks the DUT for malfunctions and breakage caused by vibration.

Vibration of the body is random vibration induced by rough-road driving. The main failure to be identified by this test is breakage due to fatigue.

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ISO 16750-3:2007(E)

4.1.2.4.2 Test

Perform the test in accordance with IEC 60068-2- random vibration. Use a test duration of 8 h for each plane of the DUT.

The r.m.s. acceleration value shall be 27,8 m/s2.

The PSD versus frequency is illustrated in Figure 7 and Table 7.

NOTE

The test duration is based on A.5.

Key

X frequency, Hz

Y power spectral density, (m/s2)2/Hz

Figure 7 — PSD of acceleration versus frequency

Table 7 — Values for PSD and frequency

Frequency

PSD (m/s2)2/Hz

10 20 55 6,5 180 0,25 300 0,25 360 0,14 1 000

0,14

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ISO 16750-3:2007(E)

4.1.2.4.3 Requirement Breakage shall not occur.

As defined in ISO 16750-1, functional status class A is required during operating mode 3.2, and functional status class C during periods with other operating modes. 4.1.2.5

Test V — Passenger car, unsprung masses (wheel, wheel suspension)

4.1.2.5.1 Purpose

This test checks the DUT for malfunctions and breakage caused by vibration.

Vibration of unsprung masses is random vibration induced by rough-road driving. The main failure to be identified by this test is breakage due to fatigue.

--```,,,,``,``,,,,```,`,```,,``-`-`,,`,,`,`,,`---Loads with frequencies lower than 20 Hz are not covered by the test profile specified here. In practice, high amplitudes can occur below 20 Hz; therefore, loads acting on the DUT in this frequency range shall be considered separately. 4.1.2.5.2 Test

Perform the test in accordance with IEC 60068-2- random vibration use a test duration of 8 h for each plane of the DUT.

The r.m.s. acceleration is 107,3 m/s2.

The PSD versus frequency is illustrated in Figure 8 and Table 8.

NOTE

The test duration is based on A5.

Key

X frequency, Hz

Y power spectral density, (m/s2)2/Hz

Figure 8 — PSD of acceleration versus frequency

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ISO 16750-3:2007(E)

Table 8 — Values for PSD and frequency

Frequency

PSD Hz

(m/s2)2/Hz

20 200 40 200 300 0,5 800 0,5 1 000 3 2 000

4.1.2.5.3 Requirement Breakage shall not occur.

As defined in ISO 16750-1, functional status class A is required during operating mode 3.2, and functional status class C during periods with other operating modes. 4.1.2.6

Test VI — Commercial vehicle, engine, gearbox

4.1.2.6.1 Purpose

This test checks the DUT for malfunctions and breakage caused by vibration. The vibrations of a piston-engine can be split up into two kinds:

⎯ sinusoidal vibration which results from unbalanced mass forces, and

⎯ random noise due to all other vibration sources of an engine, e.g. closing of valves.

Because the gearbox is rigidly attached to the engine, this test can also be used for systems/components mounted at the gearbox (no sufficient number of measurements on gearbox-mounted systems/components has been performed up to now). The main failure to be identified by this test is breakage due to fatigue. The test profiles specified in the following apply to loads generated by (four stroke) reciprocating engines. It is recommended to perform this test as a mixed mode vibration test in accordance with IEC 60068-2-80. Alternatively, these tests may be performed sequentially.

If the DUT has natural frequencies below 30 Hz, an additional test shall be carried out with a duration of 32 h in all critical planes of the DUT.

NOTE

The temperature in the chamber is above RT at the end of the test (11,75 cycles).

4.1.2.6.2 Test

4.1.2.6.2.1 Sinusoidal vibration

Perform the test in accordance with IEC 60068-2-6. Unlike in IEC 60068-2-6, a sweep rate of 0,5 octave/minute or less shall be used. Use a test duration of 94 h for each plane of the DUT (equivalent to approximately 20 hours/octave).

The amplitude versus frequency is illustrated in Figure 9 and Table 9.

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---`,,`,`,,`,,`-`-``,,```,`,```,,,,``,``,,,,```--ISO 16750-3:2007(E)

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--```,,,,``,``,,,,```,`,```,,``-`-`,,`,,`,`,,`--- Key

X frequency, Hz

Y maximum acceleration, m/s2

Figure 9 — Maximum acceleration versus frequency

Table 9 — Values for maximum acceleration versus frequency

Frequency

Amplitude of displacement

Maximum acceleration

m/s2

(11,4) 120 120 90 90 60 60 20 0,72 65 0,72 260 — 260 — 350 — 350 — 520 —

4.1.2.6.2.2 Random vibration

Perform the test in accordance with IEC 60068-2-. The test duration is as follows: ⎯ standard:

94 h for each plane of the DUT (see Figure 10 and Table 10);

⎯ for natural frequencies, fn, below 30 Hz: 32 h additionally for each critical plane of the DUT (see

Table 11).

NOTE

The PSD-values (random vibration) are reduced in the frequency range of the sinusoidal vibration test.

The PSD versus frequency is illustrated in Figure 10 and Tables 10 and 11.

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ISO 16750-3:2007(E)

Key

X frequency, Hz

Y power spectral density, (m/s2)2/Hz 1 2

standard random test profile

additional profile in case of fn < 30 Hz

Figure 10 — PSD of acceleration versus frequency

Table 10 — Values for PSD and frequency

Frequency

PSD (m/s2)2/Hz

10 14 20 28 30 28 180 0,75 300 0,75 600 20 2 000

NOTE

r.m.s. acceleration value = 177 m/s2.

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ISO 16750-3:2007(E)

Table 11 — Values for PSD and frequency, additional test in case of

natural frequencies, fn, of DUT below 30 Hz

Frequency

PSD (m/s2)2/Hz

10 50 30 30 45 0,1 NOTE

r.m.s. acceleration value = 28,6 m/s2.

4.1.2.6.3 Requirement Breakage shall not occur.

As defined in ISO 16750-1, functional status class A is required during operating mode 3.2, and functional status class C during periods with other operating modes. 4.1.2.7

Test VII — Commercial vehicle, sprung masses

4.1.2.7.1 Purpose

This test checks the DUT for malfunctions and breakage caused by vibration.

Vibration on sprung masses is random vibration induced by rough-road driving. The main failure to be identified by this test is breakage due to fatigue. 4.1.2.7.2 Test

Perform the test in accordance with IEC 60068-2-, random vibration, using a test duration of 32 h for each plane of the DUT.

The PSD versus frequency is illustrated to in Figure 11 and Tables 12 and 13.

Key

X frequency, Hz

Y power spectral density, (m/s2)2/Hz 1 standard random test profile

2 additional profile in case of fn < 30 Hz

Figure 11 — PSD of acceleration versus frequency

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ISO 16750-3:2007(E)

Table 12 — Values for PSD and frequency

Frequency

PSD (m/s2)2/Hz

10 18 20 36 30 36 180 1 2 000

NOTE

r.m.s. acceleration value = 57,9 m/s2.

--```,,,,``,``,,,,```,`,```,,``-`-`,,`,,`,`,,`---Table 13 — Values for PSD and frequency, additional test in case of

natural frequencies, fn, of DUT below 30 Hz

Frequency

PSD (m/s2)2/Hz

10 50 20 36 30 36 45 16 NOTE

r.m.s. acceleration value = 33,7 m/s2.

4.1.2.7.3 Requirement Breakage shall not occur.

As defined in ISO 16750-1, functional status class A is required during operating mode 3.2, and functional status class C during periods with other operating modes. 4.1.2.8

Test VIII — Commercial vehicle, decoupled cab

4.1.2.8.1 Purpose

This test checks the DUT for malfunctions and breakage caused by vibration.

Vibration on a decoupled commercial vehicle cab is random vibration induced by rough-road driving. The main failure to be identified by this test is breakage due to fatigue. 4.1.2.8.2 Test

Perform the test in accordance with IEC 60068-2-, random vibration. Test duration: 32 h for each plane of the DUT.

The PSD versus frequency is illustrated in Figure 12 and Table 14.

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ISO 16750-3:2007(E)

Key

X frequency, Hz

Y power spectral density, (m/s2)2/Hz 1 vertical 2 lateral

3 longitudinal

Figure 12 — PSD of acceleration versus frequency

Table 14 — Values for PSD and frequency

Frequency

PSD (m/s2)2/Hz

vertical longitudinal lateral 10 20 3 10 13 — — 10 19 — 3 — 20 20 — — 50 — 0,1 0,1 100 0,1 — — 500 0,1 0,1 0,1 2 000

r.m.s. acceleration value

0,01

21,3 m/s2 11,8 m/s2 13,1 m/s2

4.1.2.8.3 Requirement Breakage shall not occur.

As defined in ISO 16750-1, functional status class A is required during operating mode 3.2, and functional

status class C during periods with other operating modes.

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--```,,,,``,``,,,,```,`,```,,``-`-`,,`,,`,`,,`---ISO 16750-3:2007(E)

4.1.2.9 Test IX — Commercial vehicle, unsprung masses

4.1.2.9.1 Purpose

This test checks the DUT for malfunctions and breakage caused by vibration.

Vibration on unsprung masses is vibration induced by rough-road driving. The main failure to be identified by this test is breakage due to fatigue. 4.1.2.9.2 Test

Perform the random vibration test VII as in 4.1.2.7.2, and in addition the sinusoidal vibration test described below.

Carry out the sinusoidal vibration test at RT.

The sinusoidal vibration test in accordance with Table 15 describes the maximum amplitudes of acceleration on wheels and wheel suspension and the respective frequencies. If natural frequencies of the DUT below 40 Hz can be ruled out, the test can be carried out with a test frequency of 35 Hz, so that it can be performed on an electro-mechanical test stand.

Table 15 — Values for maximum acceleration and frequency in case of

lowest natural frequency, fn, of a DUT < 40 Hz

Plane in accordance with

plane in vehicle

Frequency

Hz 8 to 16

longitudinal, lateral

--```,,,,``,``,,,,```,`,```,,``-`-`,,`,,`,`,,`---Maximum acceleration

m/s2

150 120 100 300 250 200

Duration min 4 10 20 4 10 20

No. of cycles (approx.)

2 800 7 000 21 000 2 800 7 000 21 000

8 to 16 8 to 32 8 to 16

vertical 8 to 16 8 to 32

Table 16 — Values for maximum acceleration and frequency in case of lowest natural frequency, fn,

of a DUT W 40 Hz

Plane in accordance with

plane in vehicle

Frequency

Maximum acceleration

No. of cycles (approx.)

Hz m/s2

35 150 2 800 longitudinal, lateral

35 120 7 000 35 100 21 000 35 300 2 800 vertical

35 250 7 000 35 200 21 000

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ISO 16750-3:2007(E)

4.1.2.9.3 Requirement Breakage shall not occur.

As defined in ISO 16750-1, functional status class A is required during operating mode 3.2, and functional status class C during periods with other operating modes.

4.2 Mechanical shock

4.2.1 Test for devices in or on doors and flaps 4.2.1.1 Purpose

This test checks the DUT for malfunctions and breakage caused by shock of door slamming.

The load occurs on closures when slammed shut. Failure mode is mechanical damage (e.g. a detached capacitor inside the housing of an electronic control module due to the high accelerations caused by door slamming). 4.2.1.2 Test

Choose one of the profiles indicated in Table 17 and perform the test in accordance with IEC 60068-2-29 using the following test parameters: ⎯ operating mode of the DUT: ⎯ shock form (pulse shapes):

1.2 (see ISO 16750-1); half-sinusoidal.

The DUT shall be fixed on the shaker in a direction to generate the effect of acceleration in the same direction as it occurs in vehicle use.

Table 17 — Number of shocks

Location

Driver's door, cargo door Passenger's doors Trunk lid, tailgate Engine hood

Shock profile 1 500 m/s2; 11 ms

13 000 6 000 2 400 720

Shock profile 2 300 m/s2; 6 ms

--```,,,,``,``,,,,```,`,```,,``-`-`,,`,,`,`,,`---100 000 50 000 30 000 3 000

4.2.1.3 Requirement

Functional status shall be class C as defined in ISO 16750-1.

4.2.2 Test for devices on rigid points on the body and on the frame 4.2.2.1 Purpose

This test checks the DUT for malfunctions and breakage caused by shock to body and frame.

The load occurs when driving over a curb stone at high speed etc. Failure mode is mechanical damage (e.g. a detached capacitor inside the housing of an electronic control module due to the occurring high accelerations).

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4.2.2.2 Test

Perform the test in accordance with IEC 60068-2-29 using the following test parameters: ⎯ operating mode of the DUT: 3.2 (see ISO 16750-1); ⎯ pulse shape. ⎯ acceleration: ⎯ duration: ⎯ number of shocks:

half-sinusoidal; 500 m/s2; 6 ms;

10 per test direction.

Acceleration due to the shock in the test shall be applied in the same direction that the acceleration of the shock occurs in the vehicle. If the direction of the effect is not known, the DUT shall be tested in all six spatial directions.

4.2.2.3 Requirement

Functional status shall be class A as defined in ISO 16750-1. 4.2.3 Test for devices in or on the gearbox 4.2.3.1 Purpose

This test checks the DUT for malfunctions and breakage caused by shock of gear shifting. This test is applicable to DUT intended for mounting in or on the gearbox.

The loads occur during pneumatic powered gear-shifting operations. Failure mode is mechanical damage (e.g. a detached capacitor inside the housing of an electronic control module due to the high accelerations caused by pneumatically powered gear-shifting operations). 4.2.3.2 Test

Perform the test in accordance with IEC 60068-2-29 using the following test parameters: ⎯ operating mode of the DUT: 3.2 (see ISO 16750-1); ⎯ pulse shape:

half-sinusoidal;

⎯ typical maximum acceleration:

⎯ for commercial vehicles: 3 000 m/s2 to 50 000 m/s2 ⎯ for passenger cars: ⎯ typical duration: ⎯ temperature: ⎯ number of shocks:

to be agreed between customer and supplier; < 1 ms;

to be agreed between customer and supplier; to be agreed between customer and supplier.

The aforementioned values for commercial vehicles occur primarily during pneumatically supported gear-shifting operations (150 000 gear-shifting operations are typical if a range-change system is fitted).

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The actual shock stresses depend both on the installation position of the gearbox and also on the design features of the gearbox: in individual cases, it shall be ascertained by means of suitable measurements (recommended sampling frequency 25 kHz or more). A test shall be arranged between the manufacturer and the user.

The acceleration due to the shock in the test shall be applied in the same direction that the acceleration of the shock occurs in the vehicle. If the direction of the effect is not known, the DUT shall be tested in all six spatial directions.

4.2.3.3 Requirement

Functional status shall be class A as defined in ISO 16750-1.

4.3 Free fall

4.3.1 Purpose

This test checks the DUT for malfunctions and breakage caused by free fall.

A system/component may drop down to the floor during handling (e.g. at the manufacturing line of the car manufacturer). If a system/component is visibly damaged after a fall, it will be replaced, but if it is not visibly damaged, it will be installed in the car and then it shall work correctly. Failure mode is mechanical damage (e.g. a detached capacitor inside the housing of an electronic control module due to the high accelerations when the DUT hits the ground). 4.3.2 Test

Parts that obviously will be damaged by the fall shall not be checked (e.g. headlights). Parts that may withstand falling without visible damage shall be checked as follows:

Perform the test sequence in accordance with IEC 60068-2-32 using the following test parameters: ⎯ number of DUT: ⎯ falls per DUT: ⎯ drop height: ⎯ impact surface: ⎯ orientation of the DUT:

3; 2;

1 m free fall or the height of handling in accordance with agreement; concrete ground or steel plate;

1st fall of each DUT at a different dimensional axis; 2nd fall with the given DUT at the same dimensional axis, but on the opposite side of the housing;

⎯ operating mode of the DUT: 1.1 (see ISO 16750-1); ⎯ temperature:

shall be agreed between customer and supplier.

The DUT shall be visually examined after the falls. 4.3.3 Requirement

Hidden damage is not permitted. Minor damage of the housing is permitted as long as this does not affect the performance of the DUT. Proper performance shall be proven following the test. Functional status shall be class C as defined in ISO 16750-1.

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ISO 16750-3:2007(E)

4.4 Surface strength/scratch and abrasion resistance

Tests and requirements shall be agreed upon between manufacturer and customer (e.g. marking and labelling on control elements and keys shall remain visible).

4.5 Gravel bombardment

This test checks the resistance against gravel bombardment (in exposed mounting locations, e.g. front end).

5 Code letters for mechanical loads

For code letters for mechanical loads, see Table 18.

6 Documentation

For documentation, the designations outlined in ISO 16750-1 shall be used.

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Table 18 — Coding in relation to tests and requirements

Requirement in accordance with

4.1.2.1.2.1 4.1.2.1.2.2 4.1.2.6.2.1 4.1.2.6.2.2 4.1.2.2.2 4.1.2.3.2 4.1.2.4.2 4.1.2.5.2 4.1.2.7.2 4.1.2.8.2 4.1.2.9.2 4.2.1.2 4.2.2.2 4.2.3.2 Mechanical shock Code letter Mechanical shock Severity 1 Mechanical shock Severity 2 Test I sinusoidal Test VI sinusoidal A B C D E F G H I J K L M N O P Q R S T U V Z

curve 1 curve 2

yes — — — — — — — — — — — — yes yes — — — — — — — — — — — — yes — — — yes — — — — — — — — — — yes — — — — yes — — — — — — — — — yes — — — — yes — — — — — — — — yes yes — — — — yes — — — — — — yes — — yes — — — — yes — — — — — — — yes — yes — — — — — yes — — — — — — — — yes — — — — — yes — — — — — — — yes yes — — — — — — yes yes — — — — — — yes — — — — — — — — yes — — — — — yes — — — — — — — — yes — — — — yes yes — — — — — — — — yes — — yes — — yes — — — — — — — — yes — — — yes — yes — — — — — — — — — — yes — — — yes — — — — — — — — — yes — — — — yes — — — — — — — — — yes — — — yes yes — — — — — — — — — yes — yes — — yes — — — — — — — — — yes — — yes — yes — — — — — — — — — — yes — — yes yes — — yes — — — — — — — — — — — yes — — — — — — — yes — — — — — — yes upon agreement

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Free fall Test VIII Test I random Test VI random Test VII Test IV Test IX Test III Test V Test II 4.3.2 ISO 16750-3:2007(E)

Annex A (informative)

Guideline for the development of test profiles for vibration tests

A.1 Purpose

The purpose of this guideline is to ensure that the user of this part of ISO 16750 is able to develop test profiles from vibration measurements in a reproducible way and thus avoid errors.

A.2 General

The process of creating test profiles should be clarified using the recommended documentation. The process for creating test profiles is described in Table A.1.

A.3 Average control method

Generally, the responses of a DUT (response level at the natural frequencies) mounted in the vehicle and mounted on the vibration table differ. This is because of the different mounting rigidity and the different dynamic feedback for both cases.

In order to be able to reproduce the vibration tests in the laboratory, it is necessary that the vibration fixture be as stiff as possible and therefore normally much stiffer than in the car.

It should also be taken into account that the mounting points of the DUT move normally in phase on the vibration fixture, whereas the mounting points in the vehicle might not move in phase at the specific natural frequencies of the DUT. This is because of the higher stiffness of the test fixture compared to the mounting situation in the vehicle.

Furthermore, the dynamic feedback of the DUT during the vibration test (attenuation of the excitation) is minimized by the vibration control unit.

This leads to much higher response peaks in case of resonance during the shaker test compared to the response in the vehicle with similar excitation at least for heavy/bulky DUT.

To avoid overtesting, it might be necessary to apply the average control method in accordance with IEC 60068-2-.

Recommended weighting: Averaged control signal = (3 × excitation) + (1 × response of the DUT).

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Table A.1 — Development of test profiles for vibration tests

Documentation

Item

Description of the

vehicle

Recommended documentation/parameters Technical data (e.g. power, maximum r/min, nominal speed, volume, kind of engine, number of cylinders) Dynamometer and/or road

Proving ground/ test track description

Road surfaces (e.g. Belgian block, washboard, hip hop)

Full load

Df = 1/(fsample × b)

LSB = least significant bit

Reference for creating sine tests or the sinusoidal part of a sine on random test

Comments

Engine-mounted Boundary conditions

Body-mounted

Driving speed Sampling frequency Block length, b

Vehicle data

gathering

W 2,5 times of fmax W 2k (where k is the slope)

Resolution LSB < 0,1 % of maximum value Filtering techniques and methods

Anti-aliasing filter at fmax with > 48 db/oct High pass filter (ffilter < fmin) to avoid offset Peak-hold

“Hanning” for stationary signals (no transient signal) No windowing for transient signals (crest factor > 6)

Peak-hold FFT Windowing

Data analysis

r.m.s. versus speed/time

Signal characteristic Reference for creating random

Arithmetically averaged PSD from the time windows with

(sinusoidal/random part tests or the random part of a

the highest r.m.s. value

of signal) sine on random test

Waterfall diagram

Auto-correlation for stationary signals

Methods and

For example, describe all key points including data

processes used to

reduction (averaging/enveloping)

develop the test profile Methods and

procedures used to determine the test duration

Test profile development

For engine mounted components For body mounted components

Explain assumptions and models used to correlate field stress and service life with test stress and duration, e.g. as in MIL standard 810 with M-value based on most critical material

Take the r/min distribution into account

Take the mileage of bad road conditions into account

M-value = gradient of the S/N (stress versus number) curve

Rationale for the

methods — Processes

and engineering judgement Test parameters

For example, the tests in 4.1.3

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ISO 16750-3:2007(E)

A.4 Engine rotational speed distribution

There is a general relation between the rotational speed (r/min) and the vibration level. The vibration level increases with higher rotational speed (see Figure A.1 and Table A.2).

For fatigue testing, it is sufficient to consider the speed range with the highest acceleration levels. This is normally the range between 0,9 × nnominal and nmax, where nnominal is the engine speed with maximum power and nmax is the maximum safe engine speed.

To assess the test duration, it is necessary to take into account different r/min distributions and the vehicle life time. All available r/min distributions show that the r/min range from 0,9 × nnominal to nmax is normally not used very often.

For this part of ISO 16750, three distributions were chosen:

a) an r/min distribution published in SAE [2], in which 55 cars were investigated (70 000 km; 10 000 trips) b) a “worst case” r/min distribution recorded during temperature measurements with the aim of reaching very

high temperatures, the vehicles therefore being driven in a very high r/min range; c) a weighted distribution, consisting of:

1) SAE publication = 80 %, 2) “worst case”

= 20 %.

This leads to a relevant distribution of 0,5 % in the r/min range from 0,9 × nnominal to nmax. Thus, testing 22 h along each axis is equal to approximately 4 400 h lifetime in the car. With an average speed of 40 km/h, this represents a mileage of 176 000 km.

Taking into account other lifetimes, mileages and r/min distributions, the test engineer is allowed to change the test duration proportionally.

The recommended maximum test duration for practical reasons is 100 h per axis. For most vibration environments, equivalent fatigue damage is easily accomplished within this duration.

--```,,,,``,``,,,,```,`,```,,``-`-`,,`,,`,`,,`--- Key

X r/min — normalized to nnominal Y1 r.m.s. — normalized, %

Y2 r/min — probability (weighted distribution), %

1 r.m.s. level versus engine speed, n u 0,9 × nnominal 2

r.m.s. level versus engine speed, n > 0,9 × nnominal

Figure A.1 — r.m.s. acceleration level and weighted r/min distribution versus engine speed

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Table A.2 — r.m.s. acceleration level and r/min distribution versus engine speed

n/nnominal

r.m.s. level versus r/min (normalized)

r/min probability a

(px) %

r/min probability b

(px′) %

Weighted r/min distribution c (20px + 80px′)/100

1,82 1,82 4,56 4,56 5,67 5,67 4,38 4,38 4,40 4,40 5,19 5,19 5,62 5,62 5,59 5,59 3,87 3,87 3,43 3,43 1,82 1,82 1,42 1,42 0,71 0,71 0,55 0,55 0,35 0,35 0,23 0,23 0,14 0,14 0,08 0,08 0,06 0,06 0,04 0,04 0,04 0,04 0,01 0,01 0,01 0,01 0,00 0,00 0,050 — 0,075 — 0,100 — 0,125 — 0,150 7,0 0,175 6,3 0,200 6,1 0,225 7,2 0,250 7,4 0,275 8,4 0,300 10 0,325 11 0,350 12 0,375 13 0,400 14 0,425 15 0,450 17 0,475 18 0,500 20 0,525 22 0,550 24 0,575 26 0,600 29 0,625 31 0,650 34 0,675 36 0,700 39 0,725 42 0,750 46 0,775 50 0,800 54 0,825 59 0,850 63 0,875 67 0,900 72 0,925 77 0,950 84 0,975 90 1,000 98 1,025 96 1,050 100 1,075 92 1,100 86 1,125 85 1,150 79 1,175 77 1,200 79 1,225 79 a b c

0,56 0,56 0,02 0,02 8,00 8,00 5,75 5,75 3,06 3,06 4,70 4,70 5,69 5,69 5,06 5,06 3,95 3,95 3,23 3,23 2,26 2,26 1,56 1,56 1,34 1,34 1,20 1,20 1,00 1,00 0,79 0,79 0,57 0,57 0,40 0,40 0,31 0,31 0,22 0,22 0,19 0,19 0,06 0,06 0,04 0,04 0,02 0,02 2,14 2,14 5,69 5,69 5,09 5,09 4,04 4,04 4,73 4,73 5,31 5,31 5,61 5,61 5,72 5,72 3,85 3,85 3,48 3,48 1,71 1,71 1,39 1,39 0,55 0,55 0,39 0,39 0,19 0,19 0,09 0,09 0,03 0,03 0,01 0,01 0,00 0,00 0,00 0,00 0,00 0,00 0,00 0,00 0,00 0,00 0,00 0,00 “Worst case” distribution. SAE distribution.

Cumulative weighted r/min distribution (n > 0,9 nnominal) is 0,5 %; test duration of 22 h corresponds to 4 400 h in the vehicle.

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A.5 Fatigue calculation

A.5.1 Example for passenger cars, body mounted (sprung masses)

A verification is made as to whether a 8 h random vibration test is sufficient to cover the stress in the vehicle which occurs during the vehicle's lifetime.

NOTE The measurements and calculations are made on an electronic control unit (ECU). This is intended to be an example. The presented methods are neither restricted to ECUs, nor to body-mounted components.

A.5.2 Procedure

A.5.2.1 Carry out vibration measurement in the car on the test track (road bumps) and during the random vibration test on the ECU with at least two measurement points, one at the ECU mounting location (input or excitation) and one to measure the response on the printed circuit board (PCB).

A.5.2.2 Determine the load distribution on the PCB by means of a cycle counting method (see A.5.5, A.5.6 and Figure A.2) during the measuring time. A.5.2.3 Choose the car lifetime and the “bad road percentage” (both are selectable parameters).

A.5.2.4 Calculate the expected PCB load distribution by multiplying the count result in each class with the

factors:

⎯ test duration/measuring time during test;

⎯ car lifetime × percentage of bad roads/measuring time in car.

A.5.2.5 The new load distributions are used to calculate the fatigue limit that corresponds to a damage of 1. These calculations are based on:

⎯ the “Woehler hypothesis” and modifications (“Haibach”), and

⎯ the “Palmgren–Miner hypotheses of linear damage accumulation” (for details, see A.5.7 and Figure A.3). ⎯ Table A.5 shows the short result of the fatigue calculation for different models of stress versus number of

load cycles (S/N model).

A.5.3 Conclusions

A.5.3.1 General

The results of the chosen example show that the stress (fatigue limits) which results from a test duration of 8 h is about 1,7 (1,37–2,06) times higher than the stress in the vehicle during 5 400 h on a test track.

Measurements and calculations like this have been done for more than 20 years and in many applications. The results are always similar and confirm that a test duration of 8 h is sufficient. A.5.3.2 Additional confirmations

From field experience, there have been no failures known to be caused by vibration in more than 20 years. Comparisons between the chosen test tracks and measurements on selected public rough roads show that these test tracks are much more severe than public bad roads.

The selected parameters (car lifetime of 6 000 h, 90 % rough road part) are absolutely worst case. Normally, the calculation is done with less than 50 % rough road part.

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A.5.4 Test parameters

The test parameters are as follows: ⎯ test equipment: ⎯ mounting assembly: ⎯ control point: ⎯ direction:

⎯ r.m.s. acceleration value ⎯ test spectra:

electro-dynamic shaker; ECU firmly fixed on the shaker; on the shaker;

C, perpendicular to PCB; 33 m/s2; see below.

Table A.3 — Example of a random vibration test, parameters

Frequency

PSD a (m/s2)/2/Hz

10 20 30 20 200 0,5 1 000

0,1

The chosen spectra is slightly different to the spectra documented in 4.1.2.4.2.

At the resonance of the ECU (about 600 Hz) the difference is negligible.

A.5.5 Results

The test results shown in Table A.4 are based on the following parameters: ⎯ load distribution from a measuring time of 19,91 s, calculated for an 8 h test;

⎯ load distribution from a measuring time of 3,69 s on the rough road (road bumps, 50 km/h), calculated for

5 400 h (car lifetime 6 000 h, rough road part 90 %).

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Table A.4 — Test results

8 h random vibration test

Acceleration class

ai m/s2

No. of cycles per class

5 400 h rough road driving

Acceleration class

ai m/s2

No. of cycles per class

403,4 6 509 129,4 2 636 719 377,4 9 402 112,7 2 636 719 351,3 18 082 104,4 7 910 156 325,3 43 396 96,04 5 273 438 299,3 104 150 87,69 7 910 156 273,3 203 237 79,34 7 910 156 247,2 434 680 70,99 7 910 156 221,2 721 815 62, 18 457 031 195,2 1 160 835 54,28 10 546 875 169,2 1 595 516 45,93 47 460 938 143,1 2 104 692 37,58 84 375 000 117,1 2 438 116 29,23 152 929 688 91,09 2 606 636 20,88 271 582 031 65,06 2 345 538 12,53 690 820 313

Table A.5 — Short result of the fatigue calculation for different models of stress versus

number of load cycles (S/N model)

Calculated fatigue level

Fatigue Slope, k, for the random cycles of the of S/N model Hypotheses vibration test S/N model graph (24 “S/N models”)

m/s2

3,5 5

2 000 000

7 10 3,5 5

10 000 000

7 10 3,5 5

50 000 000

7 10

Needed fatigue level for 5400 h rough road driving

Comparison

(24 “S/N models”)

m/s2

165 133 144 131 136 130 132 130 126 112 118 112 116 113 117 115 91 87 93 91 97 96 102 101 --```,,,,``,``,,,,```,`,```,,``-`-`,,`,,`,`,,`---

Haibach 250 Miner 229 Haibach 246 Miner 236 Haibach 252 Miner 249 Haibach 267 Miner 266 Haibach 173 Miner 169 Haibach 187 Miner 184 Haibach 205 Miner 203 Haibach 229 Miner 229 Haibach 112 Miner 112 Haibach 137 Miner 137 Haibach 1 Miner 1 Haibach 196 Miner 196 OK OK OK OK OK OK OK OK OK OK OK OK OK OK OK OK OK OK OK OK OK OK OK OK Copyright International Organization for Standardization Provided by IHS under license with ISO

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A.5.6 Determination of the load distribution from the measured time history

There is one maximum between two zero crossings.

In each class (acceleration level), the number of maxima during the measuring time are counted.

The result of this counting method gives the number of half cycles for each class, or in other words, the load distribution from the measured time history.

The load distribution for the test duration is achieved by using a factor of (test time/measuring time) for each class, e.g. (8 h × 3 600 s/h) / 19,9 s = 1 447.

The load distribution for the car lifetime is achieved by using a factor of (car lifetime × percentage of rough roads/measuring time) for each class, e.g. (6 000 h × 0,9 × 3 600 s/h) / 3,69 s = 5 268 293.

Key X time Y class, m/s2

Number of half cycles in each class.

Figure A.2 — Counting method for the load distribution

A.5.7 Calculation of the fatigue limits

For the determination of the fatigue limit, aD, one S/N model shall be chosen. The S/N model is described by the slope, k, and the fatigue number, ND. Afterwards any starting value for aD is chosen.

From the chosen S/N model, it is possible to calculate the number of cycles to failure, Ni, for each acceleration level, ai, and the corresponding cycle number, ni.

In accordance with Palmgren–Miners hypothesis, the partial damage, si, at each level, ai, is defined by the following equation:

si=

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The whole damage, S, is defined by the following equation:

∑si

Damage occurs per definition for S W 1.

With the arbitrarily chosen starting value for aD, the damage will definitely be either < 1 or > 1. By means of iteration, the aD value is varied until a damage of “1” occurs.

Without very extensive investigations and experiments, it is impossible to know whether the chosen S/N model is realistic. Therefore, it makes sense to cover a wide range for each S/N parameter (e.g. from specialised literature). 24 models are currently used (e.g. “2 separate hypothesis”, “4 slopes k” and “3 fatigue limit cycles ND”).

Even if some of these models are unrealistic, others have more potential and it is hoped that at least one of the 24 models is sufficiently realistic. However, even if this is not the case, the quality of the comparison is not influenced too much, so long as the same model is used or the same assumptions are made for both situations (car and test), because in a comparison some false assumptions are compensated.

If all 24 aD values produced by the test are higher than the ones needed in the car, then the stress in the car is permissible. The load distribution from the selected example and the corresponding S/N graph (one model) are shown in Table A.6 and Figure A.3.

Key

X number of cycles Y acceleration level

1 slope, k

2 Haibach modification slope, 2k−1 3 Palmgren–Miner

∑

⎛⎜ni⎞⎜⎝N⎟i⎟⎠

u1 Figure A.3 — Palmgren–Miner hypotheses — Linear damage accumulation, S

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Table A.6 — Comparison of load distribution of random vibration test and one field measurement

Random vibration test

(8 h)

acceleration

m/s2 403,40 377,40 351,30 325,30 299,30 273,30 247,20 221,20 195,20 169,20 143,10 117,10 91,09 65,06 39,04

No. of cycles,

6 509 9 402 18 082 43 396 104 150 203 237 434 680 721 815 1 160 835 1 595 516 2 104 692 2 438 116 2 606 636 2 345 538 1 823 343

Corresponding S/N model graph (2 × 106; k = 5; aD = 229 m/s2) acceleration

m/s2

403,4 377,4 351,3 325,3 299,3 273,3 247,2 229,0 229,0 — — — — — —

No. of S/N cycles

276 718 349 387 448 993 587 650 786 574 1 081 121 1 536 185 2 000 000 1 000 000 000

— — — — — —

Measurement in car; road bumps

(5 400 h)

acceleration

m/s2 129,40 112,70 104,40 96,04 87,69 79,34 70,99 62, 54,28 45,93 37,58 29,23 20,88 12,53 4,176

No. of cycles,

n 2 636 719 2 636 719 7 910 156 5 273 438 7 910 156 7 910 156 7 910 156 18 457 031 10 546 875 47 460 938 84 375 000 152 929 688 271 582 031 690 820 313 3 158 7 063

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ISO 16750-3:2007(E)

Key

X number of cycles Y acceleration, m/s2 1

random vibration test (8 h)

corresponding Woehler graph to random vibration test (2 × 106; k = 5; aD = 229 m/s2)

2 measurement in car 3

Figure A.4 — Load distribution and S/N curve (one model)

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ISO 16750-3:2007(E)

Annex B (informative)

Recommended mechanical requirements for equipment

depending on the mounting location

Table B.1 indicates recommended mechanical requirements for equipment depending on the mounting location.

Table B.1 — Mounting location

Mounting location

Recommended tests and requirements

(Code letter see ISO 16750-1) passenger cars

to body to frame

on the flexible plenum chamber, not rigidly attached

Engine compartment

in the flexible plenum chamber, not rigidly attached on the engine in the engine

on the transmission/retarder in the transmission/retarder without special requirement

Passenger compartment

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D, K K, L

C C A, B, J A, B, J U,V U,V D, E, K, L D, E, K, L D, E, K, L D, E, K, L D, E, K, L

exposed to direct solar radiation exposed to radiated heat

Luggage compartment/ load compartment

luggage compartment/load compartmentto body to frame underbody/ wheel housing

sprung masses unsprung masses

D, E, K, L H, I, O, T F, G, R, S F, G, R, S F, G, R, S F, G, R, S

in/on passenger compartment door

Mounting on the exterior

to engine compartment cover to luggage compartment lid/door to trunk lid/door in cavity

open towards interior open towards exterior

D, E, K, L D, E, K, L D, E, K, L

in special compartments

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ISO 16750-3:2007(E)

Bibliography

[1] IEC 60068-2-80, Environmental testing — Part 2-80: Tests — Test Fi: Vibration — Mixed mode [2] SAE 2005-01-1071, Cae Virtual Test of Air Intake Manifolds Using Coupled Vibration and Pressure

Pulsation Loads [3] MIL-STD-810F, Department of Defense Test Method Standard for Environmental Engineering

Considerations and Laboratory Tests

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ISO 16750-3:2007(E)

ICS 43.040.10

Price based on 36 pages

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ISO_16750-3-2007