Invention Grant
- Patent Title: Cam isolation system for gas turbine engine compressor section
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Application No.: US16038344Application Date: 2018-07-18
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Publication No.: US10830086B2Publication Date: 2020-11-10
- Inventor: William S. Pratt , Paul W. Duesler
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Cantor Colburn LLP
- Main IPC: F01D17/16
- IPC: F01D17/16 ; F01D25/28

Abstract:
A cam isolation system for a gas turbine engine compressor actuator includes a torque tube. The system also includes a cam bracket operatively coupled to an engine case structure, the cam bracket defining a slot. The system further includes an actuator bracket operatively coupled to the torque tube at a first end of the actuator bracket, the actuator bracket having a pin disposed within the slot of the cam bracket.
Public/Granted literature
- US20200025023A1 CAM ISOLATION SYSTEM FOR GAS TURBINE ENGINE COMPRESSOR SECTION Public/Granted day:2020-01-23
Information query
IPC分类: