Invention Application
WO2014126855A1 SYSTEMS AND METHODS FOR CONTROLLING A MAGNITUDE OF A SONIC BOOM
审中-公开
用于控制SONIC BOOM磁头的系统和方法
- Patent Title: SYSTEMS AND METHODS FOR CONTROLLING A MAGNITUDE OF A SONIC BOOM
- Patent Title (中): 用于控制SONIC BOOM磁头的系统和方法
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Application No.: PCT/US2014/015585Application Date: 2014-02-10
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Publication No.: WO2014126855A1Publication Date: 2014-08-21
- Inventor: FREUND, Donald
- Applicant: GULFSTREAM AEROSPACE CORPORATION , FREUND, Donald
- Applicant Address: P.O. Box 2206 M/S B-06 Savannah, Georgia 31402 US
- Assignee: GULFSTREAM AEROSPACE CORPORATION,FREUND, Donald
- Current Assignee: GULFSTREAM AEROSPACE CORPORATION,FREUND, Donald
- Current Assignee Address: P.O. Box 2206 M/S B-06 Savannah, Georgia 31402 US
- Agency: RODACK, Seth
- Priority: US61/764,659 20130214
- Main IPC: B64C3/20
- IPC: B64C3/20
Abstract:
A method of controlling a magnitude of a sonic boom caused by off-design condition operation of a supersonic aircraft at supersonic speeds includes, but is not limited to the step of operating the supersonic aircraft at supersonic speeds and at an off-design condition. The supersonic aircraft has a pair of swept wings having a plurality of composite plies oriented at an angle such that an axis of greatest stiffness is non-parallel with respect to a rear spar of each wing of the pair of swept wings. The method further includes, but is not limited to the step of reducing wing twist caused by operation of the supersonic aircraft at supersonic speeds at the off-design condition with the composite plies. The method still further includes, but is not limited to, minimizing the magnitude of the sonic boom through reduction of wing twist.
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