Title:
INTEGRATED PROPULSION SYSTEM WITH BYPASS TURBOJET ENGINE
Document Type and Number:
Japanese Patent JP2008114836
Kind Code:
A
Abstract:
To provide a propulsion system capable of easily, effectively, and economically avoiding the defects of a conventional technique and facilitating maintenance operations applied to an engine at regular intervals.
This integrated propulsion turbojet engine system comprises a downstream side cylindrical nacelle structure formed of two parts. One 26 of the two parts is fixed and has a beam 20 for securing a mounting means for mounting it on aircraft. The other 40 of them can be moved between the use position and the opened position at which the maintenance operations can be easily performed.
Inventors:
GUIBERT THIBAUD JEAN-BAPTISTE
LEFORT GUILLAUME
TESNIERE MARC PATRICK
LEFORT GUILLAUME
TESNIERE MARC PATRICK
Application Number:
JP2007241953A
Publication Date:
May 22, 2008
Filing Date:
September 19, 2007
Export Citation:
Assignee:
SNECMA
International Classes:
B64D29/06; F01D25/28; F02C7/00; F02C7/20; F02K1/78
Domestic Patent References:
| JPH06510724A | 1994-12-01 | |||
| JPS6432450U | 1989-03-01 | |||
| JPS4324151B1 | ||||
| JPH08510193A | 1996-10-29 | |||
| JPH06510724A | 1994-12-01 | |||
| JPS6432450U | 1989-03-01 | |||
| JPS4324151B1 | ||||
| JPH01202598A | 1989-08-15 |
Attorney, Agent or Firm:
Yoshio Kawaguchi
Makoto Ono
Chihiro Watanabe
Kenkyo Kanayama
Katsuma Osaki
Mitsuaki Tsubokura
Makoto Ono
Chihiro Watanabe
Kenkyo Kanayama
Katsuma Osaki
Mitsuaki Tsubokura