Invention Grant
- Patent Title: Variable vane for gas turbine engine
- Patent Title (中): 燃气轮机发动机变叶片
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Application No.: US13340983Application Date: 2011-12-30
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Publication No.: US09309778B2Publication Date: 2016-04-12
- Inventor: Robert A. Ress, Jr.
- Applicant: Robert A. Ress, Jr.
- Applicant Address: US IN Indianapolis
- Assignee: Rolls-Royce North American Technologies, Inc.
- Current Assignee: Rolls-Royce North American Technologies, Inc.
- Current Assignee Address: US IN Indianapolis
- Agency: McCracken & Gillen LLC
- Main IPC: F04D29/56
- IPC: F04D29/56 ; F01D17/16

Abstract:
A turbomachine includes a variably positioned vane, an outer spindle integral with a vane outer button, where the vane is coupled to the vane outer button, an annular sleeve defining the spindle, where the annular sleeve contacts the vane outer button at a radially inward extent and contacts a turbine casing at a radially outward extent. The annular sleeve includes a wall portion having an aperture and the spindle extends through the aperture. A nut engages spindle threads, where the nut applies force to the wall portion toward the radially inward extent. An end of the spindle extends through the turbine casing, and a cantilever rotation actuator is coupled to the end of the spindle. A first bearing and second bearing engage the annular sleeve. A vane inner button is coupled to the vane, and a third bearing engages the vane inner button.
Public/Granted literature
- US20120263571A1 VARIABLE VANE FOR GAS TURBINE ENGINE Public/Granted day:2012-10-18
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