Cooling liner for convergent-divergent exhaust nozzle

Details Cooling liner for convergent-divergent exhaust nozzle Cooling liner for convergent-divergent exhaust nozzle

1981-04-17

1987-02-17

Kashnikow, Andres

Fluid sprinkling, spraying, and diffusing

Processes

Including heating or cooling

60265, 60266, 2391273, B64D 3308

Patent

active

046433562

ABSTRACT:
A gas turbine exhaust nozzle capable of long term, reliable operation is disclosed. Nozzle cooling concepts specifically directed to convergent-divergent exhaust nozzles are developed. The exhaust nozzle disclosed has a cooling liner which is strategically positioned in the nozzle to take advantage of aerodynamic conditions along the axial length of the nozzle.

REFERENCES:
patent: 3046730 (1962-07-01), Petren
patent: 3595023 (1971-07-01), Stockel
patent: 3605412 (1971-09-01), Stockel
patent: 3979065 (1976-09-01), Madden

Affiliated with

Also associated with

Rating

Cooling liner for convergent-divergent exhaust nozzle does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Cooling liner for convergent-divergent exhaust nozzle, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Cooling liner for convergent-divergent exhaust nozzle will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1933116