Laminar flow wing for transonic cruise

Aeronautics and astronautics – Aircraft structure – Details

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C244S03500A, C244S204000

Reexamination Certificate

active

07000870

ABSTRACT:
In combination, an aircraft wing and fuselage, comprising the wing having camber at or near the wing leading edge which has blunted sharpness and low sweep angle, and the fuselage having indentation along the wing side thereof, and lengthwise of the fuselage.

REFERENCES:
patent: 2709052 (1955-05-01), Berg
patent: D179348 (1956-12-01), Johnson
patent: 5322242 (1994-06-01), Tracy
patent: 5518204 (1996-05-01), Tracy
patent: 5842666 (1998-12-01), Gerhardt et al.
patent: 5897076 (1999-04-01), Tracy
patent: 6149101 (2000-11-01), Tracy

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

Laminar flow wing for transonic cruise does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Laminar flow wing for transonic cruise, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Laminar flow wing for transonic cruise will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-3642626

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