Invention Publication
- Patent Title: ENGINE MOUNT SYSTEM FOR A GAS TURBINE ENGINE
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Application No.: US18215394Application Date: 2023-06-28
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Publication No.: US20240076050A1Publication Date: 2024-03-07
- Inventor: Gabriel L. Suciu , Brian D. Merry , Christopher M. Dye , Steven B. Johnson , Frederick M. Schwarz
- Applicant: RAYTHEON TECHNOLOGIES CORPORATION
- Applicant Address: US CT Farmington
- Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Main IPC: B64D27/26
- IPC: B64D27/26 ; F01D5/06 ; F01D9/02 ; F01D15/12 ; F01D25/24 ; F01D25/28 ; F02C3/107 ; F02C7/20 ; F02C7/36 ; F02C9/18 ; F02C9/20 ; F02K1/15 ; F02K3/06
Abstract:
A gas turbine engine includes, among other things, a propulsor section including a rotor and blades, a gear train, a compressor section and a turbine section. A static structure includes a first case and a second case. The first case includes a first engine mount location. The second case includes a second engine mount location. The first engine mount location is axially near the gear train.
Public/Granted literature
- US12179929B2 Engine mount system for a gas turbine engine Public/Granted day:2024-12-31
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