Invention Grant
- Patent Title: Blade clearance control for gas turbine engine
- Patent Title (中): 燃气轮机发动机叶片间隙控制
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Application No.: US14143567Application Date: 2013-12-30
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Publication No.: US09587507B2Publication Date: 2017-03-07
- Inventor: Nathan W. Ottow
- Applicant: Rolls-Royce North American Technologies, Inc.
- 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: Barnes & Thornburg LLP
- Main IPC: F01D11/22
- IPC: F01D11/22 ; F04D29/42 ; F04D29/62 ; F01D5/04

Abstract:
An apparatus and method for controlling a clearance between the blades of a turbomachinery component and flow forming surface are disclosed herein, and includes controlling the clearance by moving the surface axially relative to the turbomachinery component. In one embodiment the apparatus includes an impeller rotatable about a first axis, a shroud encircling the impeller, and a first ring encircling the first axis. An actuator is operably engaged with the first ring to pivot the first ring about the first axis. The apparatus also includes at least one cam engaged with the first ring and at least one cam follower engaged with the shroud. Pivoting movement of the first ring about the first axis results in the at least one cam urging the at least one cam follower and the shroud along the first axis to vary a distance between the plurality of blades and the shroud.
Public/Granted literature
- US20150016946A1 BLADE CLEARANCE CONTROL FOR GAS TURBINE ENGINE Public/Granted day:2015-01-15
Information query
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