Invention Grant
- Patent Title: High response turbine tip clearance control system
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Application No.: US15359066Application Date: 2016-11-22
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Publication No.: US10316686B2Publication Date: 2019-06-11
- Inventor: Eric A. Hudson , Stephen K. Kramer
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Snell & Wilmer, L.L.P.
- Main IPC: F01D11/22
- IPC: F01D11/22 ; F01D25/24

Abstract:
An actuation system according to various embodiments can include an actuation ring having a first end and a second end separated by a gap, the actuation ring being configured to be coupled to a blade outer air seal (BOAS). The actuation system can also include an actuator coupled to at least one of the first end or the second end and configured to adjust a size of the gap such that a tip clearance between the BOAS and a blade tip is reduced in response to the size of the gap being reduced.
Public/Granted literature
- US20170159483A1 HIGH RESPONSE TURBINE TIP CLEARANCE CONTROL SYSTEM Public/Granted day:2017-06-08
Information query
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