Title:
ガスタービンエンジン推力を発生させるための方法及び装置
Document Type and Number:
Japanese Patent JP5000101
Kind Code:
B2
Abstract:
Methods and apparatus for generating thrust from a gas turbine engine using a pulse detonation system is provided. The gas turbine engine includes a fan assembly, and a bypass duct channeling air to a core engine and the pulse detonation system. The method includes injecting a charge of fuel into a pulse detonation tube that is coupled radially outward from the core engine, and controlling a supply of air from the fan into the pulse detonation tube through an opening in the inlet end of the pulse detonation tube using a rotary valve that is positioned radially outward from the core engine.
Inventors:
John Leslie Henry
Application Number:
JP2005147519A
Publication Date:
August 15, 2012
Filing Date:
May 20, 2005
Export Citation:
Assignee:
GENERAL ELECTRIC COMPANY
International Classes:
F02C5/02; F02C5/12; F02K3/06; F02K3/11
Domestic Patent References:
| JP63014013A |
Foreign References:
| US6477829 | ||||
| US3738290 | ||||
| US3332236 | ||||
| US20030154707 | ||||
| US4175380 |
Attorney, Agent or Firm:
Arakawa Satoshi
Hirokazu Ogura
Nobukazu Ito
Toshihisa Kurokawa
Hirokazu Ogura
Nobukazu Ito
Toshihisa Kurokawa