Title:
ターボジェットおよびターボプロップ複合エンジン
Document Type and Number:
Japanese Patent JP6836303
Kind Code:
B2
Abstract:
The present disclosure relates to an engine having two modes of operation—air breathing and rocket—that may be used in aerospace applications such as in an aircraft, flying machine, or aerospace vehicle. The engine's efficiency can be maximized by using a precooler arrangement to cool intake air in air breathing mode using cold fuel delivery systems used for the rocket mode. By introducing the precooler and certain other engine cycle components, and arranging and operating them as described, problems such as those associated with higher fuel and weight requirements and frost formation can be alleviated.
Inventors:
Bond Alan
Virville richard
Virville richard
Application Number:
JP2019090907A
Publication Date:
February 24, 2021
Filing Date:
May 13, 2019
Export Citation:
Assignee:
Reaction Engines Limited
International Classes:
F02K9/78; F02C7/143
Domestic Patent References:
| JP1318752A | ||||
| JP62288352A | ||||
| JP4101053A |
Foreign References:
| GB2238080A | ||||
| WO2012032273A1 | ||||
| US5101622 | ||||
| US2713243 | ||||
| US2673445 |
Other References:
F.Jivraj, R.Varvill, A.Bond and G.Paniagua,The Scimitar Precooled Mach 5 Engine,2nd EUROPEAN CONFERENCE FOR AEROSPACE SCIENCES (EUCASS),2007年 7月
Richard Varvill and Alan Bond,The SKYLON Spaceplane,journal of the British Interplanetary Society,英国,2003年10月 9日,vol.57,22-32
Richard Varvill and Alan Bond,The SKYLON Spaceplane,journal of the British Interplanetary Society,英国,2003年10月 9日,vol.57,22-32
Attorney, Agent or Firm:
Kazuko Fujita