Menu
0
Total price
0 €
PRICES include / exclude VAT
Homepage>BS EN 4540:2011 Aerospace series. Bearings, spherical plain, in corrosion resisting steel with self-lubricating liner elevated load under low oscillations. Technical specification
Sponsored link
sklademVydáno: 2012-01-31
BS EN 4540:2011 Aerospace series. Bearings, spherical plain, in corrosion resisting steel with self-lubricating liner elevated load under low oscillations. Technical specification

BS EN 4540:2011

Aerospace series. Bearings, spherical plain, in corrosion resisting steel with self-lubricating liner elevated load under low oscillations. Technical specification

Format
Availability
Price and currency
Anglicky Secure PDF
Immediate download
298.32 €
You can read the standard for 1 hour. More information in the category: E-reading
Reading the standard
for 1 hour
29.83 €
You can read the standard for 24 hours. More information in the category: E-reading
Reading the standard
for 24 hours
89.50 €
Anglicky Hardcopy
In stock
298.32 €
Označení normy:BS EN 4540:2011
Počet stran:42
Vydáno:2012-01-31
ISBN:978 0 580 65443 5
Status:Standard
DESCRIPTION

BS EN 4540:2011


This standard BS EN 4540:2011 Aerospace series. Bearings, spherical plain, in corrosion resisting steel with self-lubricating liner elevated load under low oscillations. Technical specification is classified in these ICS categories:
  • 49.035 Components for aerospace construction
This European Standard specifies the required characteristics, inspection and test methods, qualification and acceptance conditions for spherical plain bearings in corrosion resisting steel, self aligning with self lubricating liner designed to withstand (under load) slight swivelling and slow rotations only. This standard applies whenever referenced. These bearings prEN 4538-1, prEN 4538-2, prEN 4539-1 and prEN 4539-2 are for actuator applications and for use in the temperature range - 54 °C to 163 °C and for EN 4538-003 and EN 4539-003 for use in the temperature range - 54 °C to 120 °C. The liner may be of a fabric or composite material bonded to the inside diameter of the outer ring or in a composite material moulded into a pre-formed cavity between the inner and outer rings. The duty cycle (Annex E, normative) has been established on the basis of a civil aircraft aileron surface application.