Title:
特定の飛行状態を支援するために航空機の複数のエンジンによって生成される推力を制御するための方法及びシステム
Document Type and Number:
Japanese Patent JP7246192
Kind Code:
B2
Abstract:
In an example, method of controlling thrust produced by a plurality of engines on an aircraft for assisting with nose-down recovery of the aircraft is described. The method includes selecting a maximum value of an aircraft parameter, measuring a value of the aircraft parameter while the aircraft is in flight, based on a comparison of the maximum value and the measured value determining that the measured value exceeds the maximum value, and reducing a thrust produced by each of the engines of the plurality of engines to bring the measured value of the aircraft parameter below the maximum value of the aircraft parameter.
Inventors:
Mills, Nikos
eggold, david
Hogeburg, Heidi
Wilson, Douglas
Inderhaze, Leonard
Belland, Stephen
Karnofsky, Kent
Hodges, Christopher
eggold, david
Hogeburg, Heidi
Wilson, Douglas
Inderhaze, Leonard
Belland, Stephen
Karnofsky, Kent
Hodges, Christopher
Application Number:
JP2019008554A
Publication Date:
March 27, 2023
Filing Date:
January 22, 2019
Export Citation:
Assignee:
The Boeing Company
International Classes:
B64C15/02
Domestic Patent References:
| JP2014000951A | ||||
| JP2017165395A |
Foreign References:
| US20160274739 | ||||
| US20160041561 | ||||
| US20180022469 |
Attorney, Agent or Firm:
Sonoda & Kobayashi Patent Attorneys Corporation
Previous Patent: Coffee beverage containing milk solids and fruit flavor
Next Patent: MRI NOISE CONTROL SYSTEM
Next Patent: MRI NOISE CONTROL SYSTEM