Compact infrared suppressors with ring vanes for gas turbine engines
US12421914B2 · kind B2 · utility
0Cited by
14References
14Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Dec 6, 2024 |
| Grant date | Sep 23, 2025 |
| Priority date | — |
| Expiry date | Dec 6, 2044 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF02K1/825
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
An infrared suppressor adapted for use with a gas turbine engine includes a first ring arranged circumferentially around a axis, a second ring arranged circumferentially around the axis, and a strut that extends radially between and interconnects the first ring and the second ring. A portion of the second ring extends radially toward the first ring such that the portion of the second ring cooperates with the first ring to block line-of-sight into the infrared suppressor.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.