Invention Grant
- Patent Title: Feathering device for the fan blades of a turboprop engine
- Patent Title (中): 用于涡轮螺旋桨发动机风扇叶片的羽化装置
-
Application No.: US13073139Application Date: 2011-03-28
-
Publication No.: US08696303B2Publication Date: 2014-04-15
- Inventor: Francois Gallet
- Applicant: Francois Gallet
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1052287 20100329
- Main IPC: F01D21/12
- IPC: F01D21/12

Abstract:
A feathering device for the fan blades of a turboprop engine that includes at least one set of fan blades with adjustable orientation is provided. The assembly is attached in rotation to a rotating cowling connected to a turbine rotor. Each blade is coupled, for the adjustment of its orientation, to a control ring that is movable between two extreme positions, one of which corresponds to feathering of the blades. Mechanical parts are able to extend elastically as a result of a rise in their temperature, these mechanical parts being positioned facing the control ring so as to be able to exert a thrust force on the ring in order to put it in a position to feather the blades when they expand. A device to cause a rise in the temperature of the mechanical parts so as to expand them is also provided.
Public/Granted literature
- US20110236212A1 FEATHERING DEVICE FOR THE FAN BLADES OF A TURBOPROP ENGINE Public/Granted day:2011-09-29
Information query