Invention Application
- Patent Title: Adaptive Engine Exhaust Signature Suppressor
- Patent Title (中): 自适应发动机排气签名抑制器
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Application No.: US15090013Application Date: 2016-04-04
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Publication No.: US20160333797A1Publication Date: 2016-11-17
- Inventor: Robert Michael Laramee , David L. Miller
- Applicant: Bell Helicopter Textron Inc.
- Applicant Address: US TX Fort Worth
- Assignee: Bell Helicopter Textron Inc.
- Current Assignee: Bell Helicopter Textron Inc.
- Current Assignee Address: US TX Fort Worth
- Main IPC: F02C9/20
- IPC: F02C9/20 ; F02C3/04 ; B64D33/04 ; F02C7/141

Abstract:
An exhaust system has an engine exhaust plane associated with an entrance to the exhaust system, an exhaust exit plane associated with an exit of the exhaust system, a forward cap movable relative to the engine exhaust plane and configured to selectively intersect the engine exhaust plane, and an aft cap movable relative to the exhaust exit plane and configured to selectively intersect the exhaust exit plane.
Public/Granted literature
- US10457409B2 Adaptive engine exhaust signature suppressor Public/Granted day:2019-10-29
Information query
IPC分类: