Invention Grant
- Patent Title: Airplane having engines partially encased in the fuselage
- Patent Title (中): 发动机部分装在机身内的飞机
-
Application No.: US13061634Application Date: 2009-10-28
-
Publication No.: US08684302B2Publication Date: 2014-04-01
- Inventor: Philippe Gerard Chanez , Jean-Loic Herve Lecordix , Stephane Jacques Francois Thomas
- Applicant: Philippe Gerard Chanez , Jean-Loic Herve Lecordix , Stephane Jacques Francois Thomas
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR0806052 20081030
- International Application: PCT/FR2009/001256 WO 20091028
- International Announcement: WO2010/049610 WO 20100506
- Main IPC: B64D27/20
- IPC: B64D27/20
Abstract:
An airplane provided with dual-flow turbojet engines having nacelles at least partially encased in the fuselage, wherein the air intake of each engine is connected to the fuselage by two boundary layer guiding walls, the walls extending towards the upstream side of the air intake and being spaced apart towards the upstream side.
Public/Granted literature
- US20110163207A1 AIRPLANE HAVING ENGINES PARTIALLY ENCASED IN THE FUSELAGE Public/Granted day:2011-07-07
Information query
