Method of assembling a rocket engine with a transition zone...

Details Method of assembling a rocket engine with a transition zone... Method of assembling a rocket engine with a transition zone...

2007-11-27

2007-11-27

Bryant, David P. (Department: 3726)

Metal working

Method of mechanical manufacture

Rocket or jet device making

C029S890038, C060S266000, C060S267000

Reexamination Certificate

active

10985273

ABSTRACT:
An improved engine construction, such as a rocket engine construction is provided. The engine construction comprises a combustion chamber, a smooth wall nozzle, and a transition zone between the chamber and the smooth wall nozzle. The transition zone has a coolant system which includes a manifold formed from a non-copper material through which a coolant flows. In a high heat transfer embodiment, the transition zone includes an additional manifold formed from a copper based material.

REFERENCES:
patent: 3224678 (1965-12-01), Rosman
patent: 3349464 (1967-10-01), Becker Jr. et al.
patent: 3630449 (1971-12-01), Butler
patent: 3897316 (1975-07-01), Huang
patent: 3910039 (1975-10-01), Fortini
patent: 4584171 (1986-04-01), Niino et al.
patent: 4703620 (1987-11-01), Niino et al.
patent: 5557928 (1996-09-01), Castro et al.
patent: 5903976 (1999-05-01), Beaurain et al.
patent: 7051513 (2006-05-01), McMullen et al.
patent: 0 720 876 (1996-07-01), None
patent: 63-120842 (1988-05-01), None
patent: 2003-14235 (2003-01-01), None
patent: WO 02/055863 (2002-07-01), None

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