Title:
性能強化型のジェットエンジン装着支柱
Document Type and Number:
Japanese Patent JP6920054
Kind Code:
B2
Abstract:
In one example embodiment, a strut (14) for mounting a jet engine (10) to a wing (12) of an aircraft includes a plurality of engine mounts (312, 316) and a space frame truss (600) supported from the wing (12) and comprising front and aft portions, the front portion (602) being coupled to and supporting the engine mounts (312, 316), the aft portion (604) extending upwardly and rearwardly from an aft end of the front portion (602). By removing the aft end of the strut (14) from the core exhaust zone (20) of the engine (10), substantial reductions in the weight and drag of the strut (14), and a corresponding increase in the specific fuel consumption of the associated aircraft may be achieved.
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| WO/2014/174222 | STRUCTURE FOR SUSPENDING A TWIN PROP-FAN ENGINE FROM A STRUCTURAL ELEMENT OF AN AIRCRAFT |
| WO/2023/167130 | AIRCRAFT |
| WO/2015/028747 | ISOSTATIC SUSPENSION OF A TURBOJET BY REAR DOUBLE SUPPORT |
Inventors:
Nak Javani, Omid Bee.
Willie, Robert H.
Park, Paul S.
Hey Dali, Mohammad Ali
Eberle, Leonard J.
Stefanovic, Milan
Perminda, sing
Halpar, Namish Kumar Bee.
Na, Andrew Wye.
Willie, Robert H.
Park, Paul S.
Hey Dali, Mohammad Ali
Eberle, Leonard J.
Stefanovic, Milan
Perminda, sing
Halpar, Namish Kumar Bee.
Na, Andrew Wye.
Application Number:
JP2016247351A
Publication Date:
August 18, 2021
Filing Date:
December 21, 2016
Export Citation:
Assignee:
The Boeing Company
International Classes:
B64D27/26; B64D27/18; F01D25/28; F02C7/00; F02C7/20; F02K3/06
Domestic Patent References:
| JP2014522338A |
Foreign References:
| WO2015134234A1 | ||||
| US20120080582 | ||||
| US20130140281 | ||||
| EP1852346A1 | ||||
| US20100147996 | ||||
| US20120056033 |
Attorney, Agent or Firm:
Sonoda/Kobayashi Patent Business Corporation