Invention Grant
US08380371B2 Method of generating variable thrust cutback during aircraft departure
有权
在飞机起飞期间产生可变推力裁减的方法
- Patent Title: Method of generating variable thrust cutback during aircraft departure
- Patent Title (中): 在飞机起飞期间产生可变推力裁减的方法
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Application No.: US11954086Application Date: 2007-12-11
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Publication No.: US08380371B2Publication Date: 2013-02-19
- Inventor: Michael K. DeJonge
- Applicant: Michael K. DeJonge
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: General Electric Company
- Agent William Scott Andes; David J. Clement
- Main IPC: G08B23/00
- IPC: G08B23/00 ; G08B21/00 ; G06F17/00 ; G01C23/00 ; G01C21/00

Abstract:
A method of producing a variable thrust cutback of an aircraft during aircraft departure is provided. The method includes the steps of storing expected sound exposure levels for an aircraft in memory, and storing a sound exposure level limit for a navigation flight in memory. The method also includes the steps of determining aircraft altitude and determining aircraft airspeed. The method further includes the steps of computing an engine thrust value that complies with the sound exposure level limit based on the altitude, airspeed and the sound exposure levels, and outputting the computed engine thrust value for use in controlling the aircraft during departure.
Public/Granted literature
- US20090132107A1 Method of Generating Variable Thrust Cutback During Aircraft Departure Public/Granted day:2009-05-21
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