BS EN 4854-3:2019
$189.07
Aerospace series. Bearing, spherical plain, in corrosion resisting steel with self-lubricating liner, low starting torque and low friction coefficient, elevated duty cycles under low oscillations at different operating conditions – Technical specification
Published By | Publication Date | Number of Pages |
BSI | 2019 | 46 |
This European Standard specifies the required characteristics, inspection and test methods, qualification and acceptance conditions for spherical plain bearings in corrosion resisting steel with self-lubricating liner, low starting torque and low friction coefficient, elevated duty cycles under low oscillations at different operating conditions.
This standard applies whenever referenced.
These self-lubricating spherical plain bearings are intended for use in fixed or moving parts of the aircraft structure especially for control mechanism and operating systems. The bearings are designed subjected under low dynamic radial loads and slow rotations in the temperature range of −55 °C to 120 °C (−67 °F to 248 °F).
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.
PDF Catalog
PDF Pages | PDF Title |
---|---|
2 | undefined |
7 | 1 Scope 2 Normative references |
8 | 3 Terms and definitions |
11 | 4 Requirements, inspection and test methods |
22 | 5 Quality management system 5.1 Product qualification 5.2 Acceptance conditions 5.2.1 Inspections and tests to be carried out by the manufacturer 5.2.2 User’s quality control |
23 | 6 Packaging 7 Certificate of conformity |
28 | Annex A (normative)Verification of permissible and ultimate static loads (Cs, Ca) A.1 Permissible radial loads (Cs) A.1.1 Principle A.1.2 Method A.2 Ultimate radial static load A.2.1 Principle A.2.2 Method |
29 | A.3 Permissible axial static load (Ca) A.3.1 Principle A.3.2 Method A.4 Ultimate axial static load A.4.1 Principle A.4.2 Method |
32 | Annex B (normative)Verification of dynamic radial loads (Cdyn) B.1 Principle |
33 | B.2 Verification B.2.1 High and medium surface pressure tests B.2.1.1 Testing under various environmental conditions at 100 % Cdyn B.2.1.2 Testing under various environmental conditions at 50 % Cdyn B.2.2 Low surface pressure tests B.2.2.1 Testing under various environmental conditions at 5 MPa B.2.2.2 Testing under various environmental conditions at 3 MPa B.2.2.3 Testing under various environmental conditions at 1 MPa |
34 | B.2.3 Test sequence |
35 | B.2.3.1 General B.2.3.2 Method |
39 | Annex C (normative)Fluids — Essential characteristics C.1 Cleaning agent C.2 De-icing and anti-icing fluids C.3 Mineral fluid for hydraulic transmission C.4 Phosphate ester hydraulic fluid C.5 Fuel for turbine engine C.6 Silicon fluid Wacker AK 10 |
40 | C.7 Salt laden atmosphere |
41 | Annex D (normative)Peeling strength and bond integrity D.1 Peeling strength D.1.1 Principle D.1.2 Method |
42 | D.2 Bond integrity D.2.1 Peelable liner types D.2.2 Non-peelable liner types |
43 | Annex E (normative)Friction coefficient |