Invention Grant
- Patent Title: Inner diffuser case for a gas turbine engine
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Application No.: US15029474Application Date: 2014-10-31
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Publication No.: US10533437B2Publication Date: 2020-01-14
- Inventor: Timothy Dale , Swati G. Bhanderi
- 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: O'Shea Getz P.C.
- International Application: PCT/US2014/063427 WO 20141031
- International Announcement: WO2015/066473 WO 20150507
- Main IPC: F01D9/02
- IPC: F01D9/02 ; F01D25/30 ; F01D25/24 ; F23R3/04 ; F23R3/50 ; F23R3/10
Abstract:
A combustor section of a gas turbine engine has a diffuser case with a structural cone having variable wall thicknesses strategically located for reducing localized stress in the cone.
Public/Granted literature
- US20160265371A1 INNER DIFFUSER CASE FOR A GAS TURBINE ENGINE Public/Granted day:2016-09-15
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