Invention Grant
- Patent Title: Igniter for gas turbine engine
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Application No.: US16370046Application Date: 2019-03-29
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Publication No.: US11408351B2Publication Date: 2022-08-09
- Inventor: Michel Bousquet , Richard Freer
- Applicant: PRATT & WHITNEY CANADA CORP.
- Applicant Address: CA Longueuil
- Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee: PRATT & WHITNEY CANADA CORP.
- Current Assignee Address: CA Longueuil
- Agency: Norton Rose Fulbright Canada LLP
- Main IPC: F02C7/264
- IPC: F02C7/264 ; F23Q7/00

Abstract:
There is disclosed an igniter for a gas turbine engine including: a base; an inner conductor extending along an axis from the base to an end; a resistive heating element electrically connected to the end of the conductor; an outer conductor being electrically connected to the heating element, the outer conductor surrounding and extending axially along the inner conductor and forming a return electrical path, the outer conductor being radially spaced apart from the inner conductor by a gap, and an electrical insulator in the gap.
Public/Granted literature
- US20200080485A1 IGNITER FOR GAS TURBINE ENGINE Public/Granted day:2020-03-12
Information query
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