Engine mount system for a gas turbine engine
US12179929B2 · kind B2 · utility
1Cited by
259References
19Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Jun 28, 2023 |
| Grant date | Dec 31, 2024 |
| Priority date | — |
| Expiry date | Jun 28, 2043 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2270/42
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
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.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.