| 摘要 |
<p>This invention relates in general to (a) guard(s)(54)/cap(s) and/or screen(s) (10A) apparatus, single and/or multiple formation, for the nacelle/air inlet for numerous jets, turbojet, turboprop and turboshaft engines, such as helicopters, VTOL/VSTOL aircraft, power plants or the like. This apparatus contains the rotational system(s) (14a) as well as the engine shaft attached apparatus (32b) 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 (12a) for particle collector without limiting engine thrust.</p> |
