Title:
安全性向上航空機
Document Type and Number:
Japanese Patent JP7180957
Kind Code:
B2
Abstract:
An airplane has main propulsion engines and a first fuel supply for the main propulsion engines. The airplane further has an auxiliary propulsion engine and a second fuel supply for the auxiliary propulsion engine, this second fuel supply being separate from the first fuel supply. The auxiliary propulsion engine can be switched on independently from the main propulsion engines. Such airplane has increased safety, since it will be possible to maintain flight, particularly when at high altitude, even if all main propulsion engines have failed.
Inventors:
Low, Stephen
Application Number:
JP2020506220A
Publication Date:
November 30, 2022
Filing Date:
April 01, 2019
Export Citation:
Assignee:
Low, Stephen
International Classes:
B64D45/00; B64D33/00; B64D37/00; B64D41/00
Domestic Patent References:
| JP8192796A | ||||
| JP2267327A | ||||
| JP2016508466A |
Foreign References:
| CA2507280A1 | ||||
| US8528312 | ||||
| US3529793 |
Attorney, Agent or Firm:
Atsushi Nakajima
Kato Kazuho
Kato Kazuho