Invention Grant
- Patent Title: Cooling systems for gas turbine engine components
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Application No.: US14708825Application Date: 2015-05-11
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Publication No.: US09920869B2Publication Date: 2018-03-20
- Inventor: Timothy M Davis , Jeremy Drake
- 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: Cantor Colburn LLP
- Main IPC: F16L37/00
- IPC: F16L37/00 ; F16L37/086 ; F16L21/02 ; F01D9/06 ; F01D25/24
Abstract:
A transfer tube includes a conduit with an inlet and an opposed outlet. The transfer tube also includes a retention tab extending from the inlet and a locking spring tab extending from the outlet. The locking spring tab includes a claw portion extending radially from the locking spring tab of the transfer tube.
Public/Granted literature
- US20150338005A1 COOLING SYSTEMS FOR GAS TURBINE ENGINE COMPONENTS Public/Granted day:2015-11-26
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