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>UNE EN 4854-2:2019 - 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, wide series - Part 2: Dimensions and loads (Endorsed by Asociación Española de Normalización in December of 2019.)
sklademVydáno: 2019-12-01
UNE EN 4854-2:2019 - 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, wide series - Part 2: Dimensions and loads (Endorsed by Asociación Española de Normalización in December of 2019.)

UNE EN 4854-2:2019

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, wide series - Part 2: Dimensions and loads (Endorsed by Asociación Española de Normalización in December of 2019.)

Material aeroespacial. Rodamiento, plano esférico, en acero resistente a la corrosión con revestimiento autolubricante, par de arranque bajo y coeficiente de fricción bajo, ciclos de servicio elevados bajo oscilaciones bajas en diferentes condiciones de funcionamiento, serie ancha. Parte 2: Dimensiones y cargas (Ratificada por la Asociación Española de Normalización en diciembre de 2019.)

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Označení normy:UNE EN 4854-2:2019
Počet stran:16
Vydáno:2019-12-01
Status:Norma
DESCRIPTION

UNE EN 4854-2:2019

This European Standard specifies the characteristics of 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, wide series for aerospace applications. 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 to be subjected under low dynamic radial loads and slow rotations in the temperature range of "55°C to 120 °C ("67 °F to 248 °F).

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