High temperature compressible support and gasket material

Fluid sprinkling – spraying – and diffusing – Reaction motor discharge nozzle – With means controlling amount – shape or direction of...

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60200A, 428308, B64C 1506

Patent

active

041802110

ABSTRACT:
A high-temperature compressible material especially useful in rocket motors to support nozzle ring inserts, the material including a binder which when pyrolyzed leaves a char having substantial strength, and fillers including carbonaceous fillers such as carbon fibers, wools, powders, etc., plus a special filler comprising hollow carbon microspheres which can crush to provide a compressibility to the material when it is confined in a volume-limiting environment, plus other fillers which may be added to obtain special yield characteristics.

REFERENCES:
patent: 3112614 (1963-12-01), Ellenburg et al.
patent: 3133411 (1964-05-01), McCorkle
patent: 3142960 (1964-08-01), Bluck
patent: 3285519 (1966-11-01), McKague, Jr.
patent: 3524794 (1970-08-01), Jonnes 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

High temperature compressible support and gasket material does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with High temperature compressible support and gasket material, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and High temperature compressible support and gasket material will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-2067922

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