Rocket engine with integral combustion chamber step structure an

Details Rocket engine with integral combustion chamber step structure an Rocket engine with integral combustion chamber step structure an

1998-05-11

2000-10-31

Thorpe, Timothy S.

Power plants

Reaction motor

Liquid oxidizer

F02K 960

Patent

active

06138450&

ABSTRACT:
A rocket engine is prepared by fabricating a combustion chamber having an annular wall as a single piece of material. The wall has a first axial region with a first inner diameter, a second axial region with a second inner diameter greater than the first inner diameter, and an inner wall step transition between the first axial region and the second axial region. The combustion chamber is attached to an injector by bonding an annular metallic deposit to the first axial region of the combustion chamber, providing an annular adaptor ring, first welding the adaptor ring to the metallic deposit, and second welding the adaptor ring to the injector.

REFERENCES:
patent: 3085393 (1963-04-01), Hamlin, Jr.
patent: 4841724 (1989-06-01), Hall et al.
patent: 4917968 (1990-04-01), Tuffias et al.
patent: 5572865 (1996-11-01), Sackheim et al.
patent: 5613299 (1997-03-01), Ring et al.
patent: 5893266 (1999-04-01), Smith et al.

Affiliated with

Also associated with

Rating

Rocket engine with integral combustion chamber step structure an does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Rocket engine with integral combustion chamber step structure an, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Rocket engine with integral combustion chamber step structure an will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-2039622