Invention Grant
- Patent Title: Gas turbine engine with paired distributed fan sets
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Application No.: US14600101Application Date: 2015-01-20
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Publication No.: US10287991B2Publication Date: 2019-05-14
- Inventor: Gabriel L. Suciu , Jesse M. Chandler
- 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: Carlson, Gaskey & Olds, P.C.
- Main IPC: F02C7/36
- IPC: F02C7/36 ; F02C3/10
Abstract:
A gas turbine engine comprises a gas generator rotating along a first axis of rotation, with at least one compressor rotor, at least one gas generator turbine rotor and a combustion section. A fan drive turbine rotates along a second axis of rotation, downstream of at least one gas generator turbine rotor. The fan drive turbine drives a pair of shaft portions extending in opposed directions beyond the axis of rotation of the gas generator.
Public/Granted literature
- US20150361900A1 GAS TURBINE ENGINE WITH PAIRED DISTRIBUTED FAN SETS Public/Granted day:2015-12-17
Information query
IPC分类:
