Title:
ガスタービンエンジンの取り付け装置
Document Type and Number:
Japanese Patent JP3612335
Kind Code:
B2
Abstract:
A linkage arrangement (20) joins a nacelle (12) enclosing a gas turbine engine (10) and a pylon (18) suspended from an aircraft wing. The linkage arrangement (20) counteracts the deflections of the nacelle (12) with respect to the free air stream due to the aerodynamic load. The linkage arrangement (20) includes a plurality of links (22, 24, 32, 34) that substantially duplicate the motion of a four bar linkage mechanism.
Inventors:
Duesler, Paul W..
Application Number:
JP52044996A
Publication Date:
January 19, 2005
Filing Date:
November 20, 1995
Export Citation:
Assignee:
UNITED TECHNOLOGIES CORPORATION
International Classes:
B64D29/02; B64D27/18; B64D27/26; F02C7/00; F02K3/06; (IPC1-7): B64D29/02; F02C7/00; F02K3/06
Domestic Patent References:
| JP6008890A |
Foreign References:
| US4717094 | ||||
| US5078342 | ||||
| US5181675 | ||||
| US3327965 |
Attorney, Agent or Firm:
Tsuyoshi Hashimoto