AIRCRAFT POWER PLANT DRIVE SYSTEM Russian patent published in 2016 - IPC F02K1/76 

Abstract RU 2575224 C2

FIELD: transport.

SUBSTANCE: power plant drive comprising nacelle, turbojet and channel for air circulation there between has the housing, connectors, first airflow control shutter first member and transmission means. Said connectors allow attachment of said housing to said nacelle and its displacement relative thereto and about two rotational axes. First airflow control shutter actuator extends from the housing and comprises the first point for attachment of the first actuator to said shutter. Second thrust reverser shutter actuator extends from the housing and comprises the second point for attachment of the second actuator to said shutter. Note here that said housing is arranged between said first and second attachment points. Transmission means comprise the input, first output connected therewith and second output connected with the second actuator. Said means can selectively transmit the motion fed to the first output for airflow control shutter displacement or to second output for thrust reverser airflow control shutter displacement. Another invention of the set relates to power plant including aforesaid drive system.

EFFECT: decreased overall dimensions, reduced strains originating between the housing and actuators.

14 cl, 5 dwg

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RU 2 575 224 C2

Authors

Rodrigez Fernand

Dates

2016-02-20Published

2011-10-21Filed