INFRARED RADIATION SUPPRESSION DEVICE
Assignee
Filed
Jun 28, 1982
Granted
Jan 16, 1996
Location
Abstract
A gas turbine engine of the type generating a hot gas stream and a fan stream includes a mixer having upstream and downstream portions which define first and second chutes for efficiently mixing the streams prior to discharge through an engine nozzle. Means are provided to selectively communicate the downstream chutes with alternate ones of the upstream chutes to cool the downstream mixer portion and reduce the infrared radiation emissions from the nozzle,
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Jul 25, 1983
Rescinded
May 23, 1994
Duration
10 years, 10 months
Inventor
- 1Unknown Unknown
Record Details
- Patent number
- US 5483793
- Application
- 05078334
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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INFRARED SUPPRESSOR FOR A GAS TURBINE ENGINE
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