Method of making cooled rocket combustion chamber construction

Details Method of making cooled rocket combustion chamber construction Method of making cooled rocket combustion chamber construction

1994-03-14

1995-12-12

Cuda, Irene

Metal working

Method of mechanical manufacture

Rocket or jet device making

2989002, B23P 1500

Patent

active

054738172

ABSTRACT:
A method of producing a rocket combustion chamber
ozzle assembly in which a liner blank is deformed against the forming surface of a die to form a finished cooling liner, a structural jacket is electro-formed about the finished cooling liner, and fluid manifolds are secured to the finished cooling liner and structural jacket assembly.

REFERENCES:
patent: 4942653 (1990-07-01), Hawkinson
patent: 5075966 (1991-12-01), Mantkowski
patent: 5226598 (1993-07-01), Woehrl
patent: 5233755 (1993-08-01), Vandendriessche
patent: 5249357 (1993-10-01), Holmes et al.
patent: 5309636 (1994-05-01), McGovern et al.

Affiliated with

Also associated with

Rating

Method of making cooled rocket combustion chamber construction does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Method of making cooled rocket combustion chamber construction, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method of making cooled rocket combustion chamber construction will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1352962