Invention Grant
- Patent Title: Flange fastening assembly in a gas turbine engine
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Application No.: US15299022Application Date: 2016-10-20
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Publication No.: US10247038B2Publication Date: 2019-04-02
- Inventor: Matthew J. Kappes , Erin M. Romanowski , Dennes K. Burney
- Applicant: Rolls-Royce Corporation
- Applicant Address: US IN Indianapolis
- Assignee: Rolls-Royce Corporation
- Current Assignee: Rolls-Royce Corporation
- Current Assignee Address: US IN Indianapolis
- Agency: McCracken & Gillen LLC
- Main IPC: F01D25/24
- IPC: F01D25/24 ; F01D25/00 ; F01D21/04

Abstract:
According to one aspect, a flange fastening assembly for a gas turbine engine includes a first flange having a first hole therein, a second flange having a second hole disposed adjacent to the first flange, and a shoulder bolt disposed through the first hole and the second hole. The shoulder bolt has a head portion, a stem portion, and a thread portion, and the stem portion and the thread portion define a shoulder. A bolt nut is disposed on the thread portion and a first spacer is disposed between the bolt nut and the first flange such that the first spacer overhangs the shoulder.
Public/Granted literature
- US20180112557A1 FLANGE FASTENING ASSEMBLY IN A GAS TURBINE ENGINE Public/Granted day:2018-04-26
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