Composite cylinder for use in aircraft hydraulic actuator

Details Composite cylinder for use in aircraft hydraulic actuator Composite cylinder for use in aircraft hydraulic actuator

1992-05-13

1995-05-16

Look, Edward K.

Expansible chamber devices

Cylinder detail

With reinforcing member

921701, 921711, F01B 1102, F16J 1000

Patent

active

054150795

ABSTRACT:
A composite cylinder constructed from a cylindrical liner having an outer surface which is dome shaped adjacent each end. A plurality of layers of resin impregnated carbon filaments are wound on the outer surface of the liner and over the dome shaped portions. Preferably the filaments are helically wound and are wound at an angle with respect to the access of the cylindrical liner such that radial stress as applied during operation will not tend to displace the filaments wound over the dome shaped portions of the liner. The composite cylinder is useful as an integral part of a hydraulic actuator used to position flight control surfaces on aircraft.

REFERENCES:
patent: 3537484 (1970-11-01), McLarty
patent: 4039006 (1977-08-01), Inoue et al.
patent: 4132382 (1979-01-01), Jackson
patent: 4189985 (1980-02-01), Harris
patent: 4685384 (1987-08-01), Dirkin et al.
patent: 4697499 (1987-10-01), Dirkin et al.
patent: 4773306 (1988-09-01), Dirkin
patent: 4802404 (1989-02-01), Dirkin
patent: 4867044 (1989-09-01), Holtrop
patent: 4971846 (1990-11-01), Lundy

Affiliated with

Also associated with

Rating

Composite cylinder for use in aircraft hydraulic actuator does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Composite cylinder for use in aircraft hydraulic actuator, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Composite cylinder for use in aircraft hydraulic actuator will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-631487