Invention Grant
US09580183B2 Actuation mechanism for a convertible gas turbine propulsion system
有权
可转换燃气轮机推进系统的启动机制
- Patent Title: Actuation mechanism for a convertible gas turbine propulsion system
- Patent Title (中): 可转换燃气轮机推进系统的启动机制
-
Application No.: US13271196Application Date: 2011-10-11
-
Publication No.: US09580183B2Publication Date: 2017-02-28
- Inventor: Rajendra K. Agrawal , Gregory E. Reinhardt
- Applicant: Rajendra K. Agrawal , Gregory E. Reinhardt
- Applicant Address: US CT Stanford
- Assignee: Sikorsky Aircraft Corporation
- Current Assignee: Sikorsky Aircraft Corporation
- Current Assignee Address: US CT Stanford
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F02C1/00
- IPC: F02C1/00 ; B64D35/02 ; B64C27/22 ; B64D33/04 ; F02C3/10 ; F02C6/08 ; F02C6/20 ; F02C7/36 ; F02K3/02
Abstract:
A method of powering a rotary-wing aircraft includes selectively coupling and uncoupling a first power turbine to change a power distribution between the rotor system and the secondary propulsion system.
Public/Granted literature
- US20120034080A1 ACTUATION MECHANISM FOR A CONVERTIBLE GAS TURBINE PROPULSION SYSTEM Public/Granted day:2012-02-09
Information query
