Multi-spectral air inlet shield and associated inlet structure

Aeronautics and astronautics – Aircraft power plants

Reexamination Certificate

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Details

C137S015100, C454S071000, C181S229000, C055S505000

Reexamination Certificate

active

10958481

ABSTRACT:
A multi-spectral shield and associated inlet structure is provided for reducing the signature of an air inlet port defined within an exterior wall of an aircraft, ship, or land-based vehicle across radar and infrared wavelengths. The multi-spectral inlet shield includes a plate disposed in front of the air inlet port. The plate is sized to visibly eclipse the air inlet port, when viewed from a direction perpendicular to the plate. The plate is supported in this position by a plate mount or splitter that extends from within the air inlet port and attaches to the plate. A support may optionally combine with the splitter to support the plate in this position. Air passes behind the plate and into the air inlet port via a channel defined around at least a portion of the plate.

REFERENCES:
patent: 2398322 (1946-04-01), Neumann
patent: 2766677 (1956-10-01), Silverman
patent: 2942683 (1960-06-01), Moyer
patent: 3120876 (1964-02-01), Lirette
patent: 3477358 (1969-11-01), Howard
patent: 3509568 (1970-04-01), Manning et al.
patent: 5728979 (1998-03-01), Yazici et al.
patent: 6634597 (2003-10-01), Johnson et al.
patent: 6923107 (2005-08-01), Zurek et al.

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