Method for manufacturing outlet nozzles for rocket engines

Metal working – Method of mechanical manufacture – Rocket or jet device making

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C029S557000, C219S121630, C060S267000, C060S770000

Reexamination Certificate

active

06907662

ABSTRACT:
Methods for manufacturing outlet nozzles for use in rocket motors are disclosed. The methods include providing an inner wall, positioning an outer wall around the inner wall, positioning spacers in the space between the inner and outer walls, and laser welding between the spacers and at least one of the inner and outer walls in order to form cooling ducts between the spacers and to provide T-shaped joints between the spacers and at least one of the inner and outer walls, the T-shaped joints including a rounded shape within the cooling ducts.

REFERENCES:
patent: 3235947 (1966-02-01), Schlemann
patent: 3832290 (1974-08-01), Fortini
patent: 5221045 (1993-06-01), McAninch et al.
patent: 5233755 (1993-08-01), Vandendriessche
patent: 5501011 (1996-03-01), Pellet
patent: 5588268 (1996-12-01), Sterflinger et al.
patent: 5645127 (1997-07-01), Enderle et al.
patent: 5822853 (1998-10-01), Ritter et al.
patent: 5874015 (1999-02-01), Mittendorf et al.
patent: 6107596 (2000-08-01), Semenov et al.
patent: 6134782 (2000-10-01), Wright
patent: 6205661 (2001-03-01), Ring
patent: 6240640 (2001-06-01), Matsuoka et al.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Method for manufacturing outlet nozzles for rocket engines 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 for manufacturing outlet nozzles for rocket engines, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Method for manufacturing outlet nozzles for rocket engines will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-3482747

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.