Title:
AIRCRAFT PROTECTION METHOD AND SYSTEM
Document Type and Number:
WIPO Patent Application WO2005039978
Kind Code:
A3
Abstract:
In the operation of a turbojet engine of an aircraft, a method of reducing the infrared radiation in the engine's exhaust; comprising: 1) releasing infrared radiation masking material selected from the group consisting of liquid nitrogen, water, and calcined aluminum and combinations thereof into the engine's exhaust so that the infrared radiation in the exhaust is reduced.
Inventors:
PERRICONE NICHOLAS V (US)
Application Number:
PCT/US2004/033548
Publication Date:
December 08, 2005
Filing Date:
October 12, 2004
Export Citation:
Assignee:
PERRICONE NICHOLAS V (US)
International Classes:
B64D33/04; F02C7/00; F02K1/28; F02K1/82; B64D; (IPC1-7): F02K1/28
Foreign References:
| US3327480A | 1967-06-27 | |||
| US5269132A | 1993-12-14 |
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