Engine with upstream and rotationally attached guard

Gas separation – Aircraft anti-ingestion means

Reexamination Certificate

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Details

C055S394000, C055S396000, C055S401000, C055S406000, C055S521000, C060S039092

Reexamination Certificate

active

06872232

ABSTRACT:
This invention relates in general to a guard(s)/cap(s) and/or screen(s) apparatus (single and/or multiple formation) for the nacelle/air inlet for numerous jets, turbojet, turboprop and turboshaft engines—(Helicopters and other VTOL/VSTOL aircraft) such as power plants or the like. This apparatus contains the rotational system(s) as well as the engine shaft attached apparatus and/or pole that allows the mechanism to function by auto induced movement,without limiting engine thrust. Additional security measures have been introduced to the guard(s)/cap(s) and/or screen(s) apparatus, which includes a centrifuge chamber/manifold for particle collector without limiting engine thrust.

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Supplemental European Search Report for 00991684.2 dated Dec. 20, 2002.

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