Temperature normalized structure

Aeronautics and astronautics – Aircraft structure

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

244119, 244123, B64C 138, B64D 3734

Patent

active

053059735

ABSTRACT:
Circulation of temperature controlled fluid through cavities in structure stiffening members of hypersonic aerospace vehicles precludes destructive temperature gradients in such members and preserves stress residuals for functional requirements.

REFERENCES:
patent: 3015461 (1962-01-01), Fineblum
patent: 3369782 (1968-02-01), Billig et al.
patent: 4273304 (1981-06-01), Frosch et al.
patent: 4776536 (1988-10-01), Hudson et al.
patent: 4786015 (1988-11-01), Niggemann
patent: 4923146 (1990-05-01), Anthony

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

Temperature normalized structure does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Temperature normalized structure, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Temperature normalized structure will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1707115

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