The Boeing Company

Chris T Jasklowski

Kent Edmund Karnofski

Jason Joseph Jackowski

Michael Jay Burghdoff

Jason J Jackowski

Systems and methods are provided for a flexible band electrical component mount that includes a flexible band configured to receive one or more electrical components. The flexible band may be configured to couple to and/or wrap around at least a portion of an aircraft propulsor. The electrical components may be configured to output data from the aircraft propulsor and/or data related to operation of the aircraft propulsor. Such flexible bands may be configured to receive a plurality of electrical components and may be configured to wrap around the portion of the aircraft propulsor a plurality of times.

Flexible band electrical component mounts and methods

Pressurized fluid is stored while a jet engine is running. After engine shutdown, the fluid is used to drive a pneumatic or hydraulic turning motor that rotates the engine's High Pressure (HP) rotor. The rotation encourages even heat distribution across the HP rotor and thus prevents bowing of the HP rotor.

Engine turning motor via pneumatic or hydraulic motor

An aircraft includes a jet engine and a telescopic tube assembly positioned on the jet engine. The telescopic tube assembly includes one end portion of the telescopic tube assembly which is associated with a thrust reverser translating sleeve of the jet engine and an opposing end portion of the telescopic tube assembly which is associated with a fixed portion of the of the jet engine. A jet engine includes a telescopic tube assembly positioned on the jet engine. The telescopic tube assembly includes one end portion of the telescopic tube assembly which is associated with a thrust reverser translating sleeve of a jet engine and an opposing end portion of the telescopic tube assembly which is associated with a fixed portion of the of the jet engine.

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Redmond, WA, United States of America

Chris T Jasklowski