PRICES include / exclude VAT
Homepage>BS Standards>49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.035 Components for aerospace construction>BS EN 4156:2013 Aerospace series. Rod ends, with self-aligning double row ball bearings and threaded shank in steel. Inner ring and balls in corrosion resisting steel. Dimensions and loads. Inch series
Sponsored link
immediate downloadReleased: 2013-12-31
BS EN 4156:2013 Aerospace series. Rod ends, with self-aligning double row ball bearings and threaded shank in steel. Inner ring and balls in corrosion resisting steel. Dimensions and loads. Inch series

BS EN 4156:2013

Aerospace series. Rod ends, with self-aligning double row ball bearings and threaded shank in steel. Inner ring and balls in corrosion resisting steel. Dimensions and loads. Inch series

Format
Availability
Price and currency
English Secure PDF
Immediate download
180.00 EUR
You can read the standard for 1 hour. More information in the category: E-reading
Reading the standard
for 1 hour
18.00 EUR
You can read the standard for 24 hours. More information in the category: E-reading
Reading the standard
for 24 hours
54.00 EUR
English Hardcopy
In stock
180.00 EUR
Standard number:BS EN 4156:2013
Pages:16
Released:2013-12-31
ISBN:978 0 580 82944 4
Status:Standard
DESCRIPTION

BS EN 4156:2013


This standard BS EN 4156:2013 Aerospace series. Rod ends, with self-aligning double row ball bearings and threaded shank in steel. Inner ring and balls in corrosion resisting steel. Dimensions and loads. Inch series is classified in these ICS categories:
  • 49.035 Components for aerospace construction

This European Standard specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing and threaded shank in steel, inner ring and balls in corrosion resisting steel.

They consist of:

  • a rod end comprising:

    • either seals or shields;

    • an optional longitudinal groove for locking purpose;

  • an inner ring with balls.

These rod ends are intended for use with flight control rods or rods for aerospace structures.

They are intended to be used in the temperature range: – 54 °C to 150 °C.

However, being lubricated with the following greases:

  • very high pressure grease, ester type (code A), operational range – 73 °C to 121 °C according MIL-PRF-23827 type II

  • very high pressure grease, synthetic hydrocarbons, general purpose (code B), operational range − 54 °C to 177 °C (see EN 2067), according MIL-PRF-81322.

  • very high pressure grease, lithium type (code C) operational range – 73 °C to 121 °C according MIL-PRF-23827 type I.

Their field of application when lubricated with codes A and C grease is limited to 121 °C.