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Commission Directive 2010/22/EU of 15 March 2010 amending, for the purposes of their adaptation to technical progress, Council Directives 80/720/EEC, 86/298/EEC, 86/415/EEC and 87/402/EEC and Directives 2000/25/EC and 2003/37/EC of the European Parliament and of the Council relating to the type-approval of agricultural or forestry tractors (Text with EEA relevance) (repealed)
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This is the original version (as it was originally adopted).
The technical requirements for the EC type-approval of rear-mounted roll-over protection structures of narrow-track wheeled agricultural or forestry tractors shall be those set out in point 3 of Code 7 of the OECD Decision C(2008) 128 of October 2008, with the exception of points 3.1.4 (Test report), 3.3.1 (Administrative extensions), 3.4 (Labeling) and 3.6 (Seat belt anchorage performance), reading as follows:
Tests made using special rigs are intended to simulate such loads as are imposed on a protective structure, when the tractor overturns. These tests enable observations to be made on the strength of the protective structure and any brackets attaching it to the tractor and any parts of the tractor which transmit the test load.
Tests may be performed in accordance with the dynamic procedure or the static procedure. The two methods are deemed equivalent.
Note: A complete tractor is not required for the static strength test; however, the protective structure and parts of the tractor to which it is attached represent an operating installation, hereinafter referred to as ‘the assembly’.
Components which may create a hazard in the clearance zone must also be fitted on the tractor (or the assembly) so that they may be examined to see whether the requirements of the Acceptance Conditions in 3.1.3 have been fulfilled. All components of the tractor or the protective structure including weather protective must be supplied or described on drawings.
The reference mass M, used in the formulae to calculate the height of the fall of the pendulum block, the loading energies and the crushing forces, must be at least the mass of the tractor, excluding optional accessories but including coolant, oils, fuel, tools plus the protective structure. Not included are optional front or rear weights, tyre ballast, mounted implements, mounted equipment or any specialised components.
The sequence of tests, without prejudice to the additional tests mentioned in sections 3.2.1.1.6, 3.2.1.1.7, 3.2.2.1.6 and 3.2.2.1.7, is as follows:
impact (dynamic test) or loading (static test) at the rear of the structure (see 3.2.1.1.1 and 3.2.2.1.1);
rear crushing test (dynamic or static test) (see 3.2.1.1.4 and 3.2.2.1.4);
impact (dynamic test) or loading (static test) at the front of the structure (see 3.2.1.1.2 and 3.2.2.1.2);
impact (dynamic test) or loading (static test) at the side of the structure (see 3.2.1.1.3 and 3.2.2.1.3);
crushing at the front of the structure (dynamic or static test) (see 3.2.1.1.5 and 3.2.2.1.5).
after each test in the dynamic test procedure, it shall be free from tears or cracks, as defined in 3.2.1.2.1. If during the dynamic test, significant tears or cracks appear, an additional impact test or crushing test as defined in 3.2.1.1.6 or 3.2.1.1.7 must be performed immediately after the test which caused these tears or cracks to appear;
during static test, at the point when the energy required is attained in each horizontal load test prescribed or in the overload test the force must be greater than 0,8 F;
if during a static test, cracks or tears appear as a result of the application of the crushing force, an additional crushing test as defined in 3.2.2.1.7 must be performed immediately after the crushing test which caused these cracks or tears to appear;
during the tests other than the overload test, no part of the protective structure must enter the clearance zone as defined in 1.6 of Annex I;
during the tests other than the overload test, all parts of the clearance zone shall be secured by the structure, in accordance with 3.2.1.2.2 and 3.2.2.2.2;
during the tests the protective structure must not impose any constraints on the seat structure;
the elastic deflection, measured in accordance with 3.2.1.2.3 and 3.2.2.2.3 shall be less than 250 mm.
The pendulum pivot points must be rigidly fixed so that their displacement in any direction does not exceed 1 per cent of the height of fall.
A rig as shown in Figure 7.7 shall be capable of exerting a downward force on a protective structure through a rigid beam approximately 250 mm wide connected to the load-applying mechanism by means of universal joints. Suitable axle stands shall be provided so that the tractor tyres do not bear the crushing force.
The following measuring apparatus is needed:
device for measuring the elastic deflection (the difference between the maximum momentary deflection and the permanent deflection, see Figure 7.8).
device for checking that the protective structure has not entered the clearance zone and that the latter has remained within the structure’s protective during the test (see section 3.2.2.2.2).
at start of test, under zero load: ± 2°,
during test, under load: 10° above and 20° below the horizontal. These variations must be kept to a minimum.
If the tractor moves, the entire test shall be repeated, unless the system for measuring the deflections taken into account for plotting the force versus deflection curve is connected to the tractor.
A rig as shown in Figure 7.7 shall be capable of exerting a downward force on a protective structure through a rigid beam approximately 250 mm wide, connected to the load-applying mechanism by means of universal joints. Suitable axle stands must be provided so that the tractor tyres do not bear the crushing force.
The following measure devices are also needed:
device for measuring the elastic deflection (the difference between the maximum momentary deflection and the permanent deflection, see Figure 7.8).
device for checking that the protective structure has not entered the clearance zone and that the latter has remained within the structure’s protective during the test (section 3.3.2.2.2).
The suspended height of the block shall be adjusted and necessary steps taken so as to prevent the block from turning about the point of impact.
The point of impact is that part of the protective structure likely to hit the ground first in a rearward overturning accident, normally the upper edge. The position of the centre of gravity of the block is 1/6 of the width of the top of the protective structure inwards from a vertical plan parallel to the median plane of the tractor touching the outside extremity of the top of the protective structure.
If the structure is curved or protruding at this point, wedges enabling the impact to be applied thereon must be added, without thereby reinforcing the structure.
The wire ropes must be tensioned so that the tyres undergo the deflections given in 3.1.5.6.2. With the wire ropes tensioned, the wedging beam shall be placed in front of and tight against the rear wheels and then fixed to the ground.
H = 2,165 × 10–8 M L2
or
H = 5,73 × 10–2 I
The pendulum block is then released and strikes the protective structure.
H = 25 + 0,07 M
for tractor with a reference mass of less than 2 000 kg;
H = 125 + 0,02 M
for tractor with a reference mass of more than 2 000 kg.
The suspended height of the pendulum block shall be adjusted and the necessary steps taken so as to prevent the block from turning about the point of impact.
The point of impact is that part of the protective structure likely to hit the ground first if the tractor overturned sideways while travelling forward, normally the upper edge. The position of the centre of gravity of the block is 1/6 of the width of the top of the protective structure inwards from a vertical plane parallel to the median plane of the tractor touching the outside extremity of the top of the protective structure.
If the structure is curved or protruding at this point, wedges enabling the impact to be applied thereon must be added, without thereby reinforcing the structure.
The wire ropes must be tensioned so that the tyres undergo the deflections given in 3.1.5.6.2. With the wire ropes tensioned, the wedging beam shall be placed behind and tight against the rear wheels and then fixed to the ground.
H = 25 + 0,07 M
for tractor with a reference mass of less than 2 000 kg;
H = 125 + 0,02 M
for tractor with a reference mass of more than 2 000 kg.
The pendulum block is then released and strikes the protective structure.
if the protective structure is a rear two-post rollbar, the above formula shall apply,
for other types of protective structure, the height shall be whichever is greater from the formula applied above and that selected below:
H = 2,165 × 10–8 ML2
or
H = 5,73 × 10–2 I
The pendulum block is then released and strikes the protective structure.
With the wire ropes tensioned, the wedging beam shall be placed on the ground, pushed tight against the tyres on the side opposite that which is to receive the impact and then fixed to the ground. It may be necessary to use two beams or wedges if the outer sides of the front and rear tyres are not in the same vertical plane. The prop shall then be placed as indicated in Figure 7.6 against the rim of the most heavily loaded wheel opposite to the point of impact, pushed firmly against the rim and then fixed at its base. The length of the prop shall be such that it makes an angle of 30 ± 3° with the ground when in position against the rim. In addition, its thickness shall, if possible, be between 20 and 25 times less than its length and between 2 and 3 times less than its width. The props shall be shaped at both ends as shown in the details on Figure 7.6.
H = 25 + 0,20 M
for tractors with a reference mass of less than 2 000 kg;
H = 125 + 0,15 M
for tractors with a reference mass of more than 2 000 kg.
if the protective structure is a rear two-post rollbar, the selected height shall be whichever is greater from the formulae applicable above and below:
H = (25 + 0,20 M) (B6 + B) / 2B
for tractor with a reference mass of less than 2 000 kg;
H = (125 + 0,15 M) (B6 + B) / 2B
for tractor with a reference mass of more than 2 000 kg.
for other types of protective structures, the selected height shall be whichever is greater from the formulae applicable above and below:
H = 25 + 0,20 M
for tractor with a reference mass less than 2 000 kg;
H = 125 + 0,15 M
for tractor with a reference mass of more than 2 000 kg.
The pendulum block is then released and strikes the protective structure.
The beam shall be positioned over the rear uppermost structural member(s) and the resultant of crushing forces shall be located in the tractor’s median plane A force Fv shall be applied where:
Fv = 20 M
The force Fv shall be maintained for five seconds after the cessation of any visually detectable movement of the protective structure.
Where the rear part of the protective structure roof will not sustain the full crushing force, the force shall be applied until the roof is deflected to coincide with the plane joining the upper part of the protective structure with that part of the rear of the tractor capable of supporting the tractor when overturned.
The force shall then be removed, and the crushing beam repositioned over that part of the protective structure which would support the tractor when completely overturned. The crushing force Fv shall then be applied again.
The beam shall be positioned across the front uppermost structural member(s) and the resultant of crushing forces shall be located in the tractor’s median plane. A force Fv shall be applied where:
Fv = 20 M
The force Fv shall be maintained for five seconds after the cessation of any visually detectable movement of the protective structure.
Where the front part of the protective structure roof will not sustain the full crushing force, the force shall be applied until the roof is deflected to coincide with the plane joining the upper part of the protective structure with that part of the front of the tractor capable of supporting the tractor when overturned.
The force shall then be removed, and the crushing beam repositioned over that part of the protective structure which would support the tractor when completely overturned. The crushing force Fv shall then be applied again.
If cracks or tears which cannot be considered negligible appear during an impact test, a second, similar test, but with a height of fall of:
H’ = (H × 10–1) (12 + 4a) (1 + 2a)–1
shall be performed immediately after the impact tests causing these tears or cracks to appear, “a” being the ratio of the permanent deformation (Dp) to the elastic deformation (De):
a = Dp / De
as measured at the point of impact. The additional permanent deformation due to the second impact shall not exceed 30 per cent of the permanent deformation due to the first impact.
In order to be able to carry out the additional test, it is necessary to measure the elastic deformation during all the impact tests.
If during a crushing test, significant cracks or tears appear, a second, similar, crushing test, but with a force equal to 1,2 Fv shall be performed immediately after the crushing tests which caused these tears or cracks to appear.
After each test all structural members, joints and fastening systems shall be visually examined for fractures or cracks, any small cracks in unimportant parts being ignored.
Any tears caused by the edges of the pendulum weight are to be ignored.
During each test the protective structure shall be examined to see whether any part it has entered a clearance zone round the driving seat as defined in 1.6.
Furthermore, the clearance zone shall not be outside the protection of the protective structure. For this purpose, it shall be considered to be outside the protection of the structure if any part of it would come in contact with flat ground if the tractor overturned towards the direction from which the test load is applied. For estimating this, the front and rear tyres and track width setting shall be the smallest standard fitting specified by the manufacturer.
The elastic deflection shall be measured (810 + av) mm above the seat index point, in the vertical plane in which the load is applied. For this measurement, any apparatus similar to that illustrated in Figure 7.8 may be used.
After the final crushing test, the permanent deflection of the protective structure shall be recorded. For this purpose, before the start of the test, the position of the main roll-over protective structure members in relation to the seat index point shall be used.
The load application point shall be that part of the roll-over protective structure likely to hit the ground first in a rearward overturning accident, normally the upper edge. The vertical plane in which the load is applied shall be located at a distance of one third of the external width of the upper part of the structure from the median plane.
If the structure is curved or protruding at this point, wedges enabling the load to be applied thereon shall be added, without thereby reinforcing the structure.
Eil = 2,165 × 10–7 M L2
or
Eil = 0,574 × I
Eil = 500 + 0,5 M
If the structure is curved or protruding at this point, wedges enabling the load to be applied thereon shall be added, without thereby reinforcing the structure.
Eil = 500 + 0,5 M
if the protective structure is a rear two-post rollbar the preceding formula shall also apply,
for other types of protective structures, the energy shall be whichever is the higher of the above or either of the following as selected:
Eil = 2,165 × 10–7 ML2
or
Eil = 0,574 I
Eis = 1,75 M
Eis = 1,75 M
or
Eis = 1,75 M (B6 + B)/2B
All provisions are identical to those given in 3.2.1.1.4.
All provisions are identical to those given in 3.2.1.1.5.
An overload test shall be carried out in all cases where the force decreases by more than 3 per cent during the last 5 per cent of the deflection reached when the energy required is absorbed by the structure (see Figure 7.10).
The overload test involves the gradual increase of the horizontal load by increments of 5 per cent of the initial energy requirement up to a maximum of 20 per cent of energy added (see Figure 7.11).
The overload test is satisfactory if, after each increase by 5, 10, or 15 per cent in the energy required, the force decreases by less than 3 per cent for a 5 per cent increment and remains greater than 0,8 Fmax.
The overload test is satisfactory if, after the structure has absorbed 20 per cent of the added energy, the force exceeds 0,8 Fmax.
Additional cracks or tears and/or entry into or lack of protective of the clearance zone due to elastic deflection are permitted during the overload test. However, after the removal of the load, the structure shall not enter the clearance zone, which shall be completely protected.
If cracks or tears which cannot be considered as negligible appear during a crushing test, a second, similar crushing, but with a force of 1,2 Fv shall be applied immediately after the crushing test which caused the cracks or tears to appear.
After each test all structural members, joints and attachment systems shall be visually examined for fractures or cracks, any small cracks in unimportant parts being ignored.
During each test the protective structure shall be examined to see whether any part of it has entered a clearance zone as defined in 1.6 of Annex I.
In addition, an examination shall be made to determine whether any part of the clearance zone is outside the protection of the structure. For this purpose it is considered to be outside the protection of the roll-over protective structure if any part of it would have come in contact with the ground plane if the tractor had overturned in the direction from which the impact came. For this purpose the front and rear tyres and track setting are assumed to be the smallest specified by the manufacturer.
The elastic deflection shall be measured (810 + av) mm above the seat index point, in the vertical plane in which the load is applied. For this measurement, any apparatus similar to that illustrated in Figure 7.8 may be used.
After the final crushing test, the permanent deflection of the protective structure shall be recorded. For this purpose, before the start of the test, the position of the main roll-over protective structure members in relation to the seat index point shall be used.
Extension to other tractor models
When technical modifications occur on the tractor, the protective structure or the method of attachment of the protective structure to the tractor, the testing station that has carried out the original test can issue a ‘technical extension report’ in the following cases:
The impact and crushing tests need not be carried out on each model of tractor, provided that the protective structure and tractor comply with the conditions referred to hereunder 3.3.2.1.1 to 3.3.2.1.5.
This procedure has to be followed when the provisions of paragraph 3.3.2.1 are not fulfilled, it may not be used when the method of attachment of the protective structure to the tractor does not remain of the same principle (e.g. rubber supports replaced by a suspension device):
Modifications having no impact on the results of the initial test (e.g. weld attachment of the mounting plate of an accessory in a non-critical location on the structure), addition of seats with different SIP location in the protective structure (subject to checking that the new clearance zone(s) remain(s) within the protection of the deflected structure throughout all tests).
Modifications having a possible impact on the results of the original test without calling into question the acceptability of the protective structure (e.g. modification of a structural component, modification of the method of attachment of the protective structure to the tractor). A validation test can be carried out and the test results will be drafted in the extension report.
The following limits for this type extension are fixed:
no more than 5 extensions may be accepted without a validation test;
the results of the validation test will be accepted for extension if all the acceptance conditions of the Code are fulfilled and:
if the deflection measured after each impact test does not deviate from the deflection measured after each impact test in the original test report by more than ± 7 % (in case of a dynamic test);
if the force measured when the required energy level has been reached in the various horizontal load tests does not deviate from the force measured when the required energy has been reached in the original test by more than ± 7 % and the deflection measured(1) when the required energy level has been reached in the various horizontal load tests does not deviate from the deflection measured when the required energy has been reached in the original test by more than ± 7 % (in case of a static test).
more than one protective structure modifications may be included in a single extension report if they represent different options of the same protective structure, but only one validation test can be accepted in a single extension report. The options not tested shall be described in a specific section of the extension report.
Increase of the reference mass declared by the manufacturer for a protective structure already tested. If the manufacturer wants to keep the same approval number it is possible to issue an extension report after having carried out a validation test (the limits of ± 7 % specified in 3.3.2.2.2.2 are not applicable in such a case).
Steel with an as-rolled thickness less than 2,5 mm and with a carbon content less than 0,2 per cent is considered to meet this requirement.
Structural members of the protective structure made from materials other than steel shall have equivalent low temperature impact resistance.
Minimum Charpy V-notch impact energies
a Indicates preferred size. Specimen size shall be no less than largest preferred size that the material permits. | ||
b The energy requirement at – 20 °C is 2,5 times the value specified for – 30 °C. Other factors affect impact energy strength, i.e. direction of rolling, yield strength, grain orientation and welding. These factors shall be considered when selecting and using steel. | ||
Specimen size | Energy at | Energy at |
---|---|---|
-30 °C | -20 °C | |
mm | J | Jb |
10 × 10a | 11 | 27,5 |
10 × 9 | 10 | 25 |
10 × 8 | 9,5 | 24 |
10 × 7,5a | 9,5 | 24 |
10 × 7 | 9 | 22,5 |
10 × 6,7 | 8,5 | 21 |
10 × 6 | 8 | 20 |
10 × 5a | 7,5 | 19 |
10 × 4 | 7 | 17,5 |
10 × 3,5 | 6 | 15 |
10 × 3 | 6 | 15 |
10 × 2,5a | 5,5 | 14 |
Permanent + elastic deflection measured at the point when the required energy level is obtained.” ’
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