Flexible hydraulic latch

Aeronautics and astronautics – Aircraft structure – Passenger or crew accommodation

Reexamination Certificate

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Details

C244S129400

Reexamination Certificate

active

06951319

ABSTRACT:
A latching system includes a flexible hydraulic latch male portion, and a receiving rail female portion. The receiving rail female portion receives the hydraulic latch male portion therein. The latching system includes a hydraulic system for providing hydraulic fluid into the flexible hydraulic latch. The latching system includes a controlling device for controlling operation and hydraulic fluid insertion by the hydraulic system into the flexible hydraulic latch. The latching system includes an ejection system coupled to the hydraulic system or flexible hydraulic latch for reducing hydraulic fluid pressure within the flexible hydraulic latch during an ejection evolution.

REFERENCES:
patent: 2784926 (1957-03-01), Bonza et al.
patent: 2863681 (1958-12-01), Robbins
patent: 3040393 (1962-06-01), Dailey
patent: 3074520 (1963-01-01), Grubelich
patent: 4531856 (1985-07-01), Gebelius
patent: 6425707 (2002-07-01), Baxter
patent: 6485029 (2002-11-01), Moody et al.
Kirkhill Rubber-TA Mfg. Team, Aviation and Aerospace Products, www.kirkhill.com, Aug. 30, 2002, (3 pgs), U.S.
Presray Corporation, Bustom Rubber Fabrications, www.presray.com, Aug. 30, 2002, (1 pg), U.S.
Sealmaster, Seal Master Custom-Built Inflatable Seal, www.sealmaster.com, Aug. 30, 2002, (4 pgs), U.S.

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