Variable area fan nozzle thrust reverser
US8844261B2 · kind B2 · utility
0Cited by
9References
10Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Feb 10, 2012 |
| Grant date | Sep 30, 2014 |
| Priority date | — |
| Expiry date | Jan 9, 2033 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF02K1/70
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A nozzle for use in a gas turbine engine includes nozzle doors coupled with a fan nacelle wherein the nozzle doors move in unison between a plurality of positions to influence a bypass airflow through a fan bypass passage. A linkage connects the nozzle doors and an actuator. A louver section coupled with the linkage moves in unison with the nozzle doors between a plurality of louver positions to direct a portion of the bypass airflow in a selected direction.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.