Laminar-flow airfoil

Aeronautics and astronautics – Composite aircraft – Trains

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C244S03500A, C244S216000, C244S211000

Reexamination Certificate

active

06905092

ABSTRACT:
An airfoil having a fore airfoil element, an aft airfoil element, and a slot region in between them. These elements induce laminar flow over substantially all of the fore airfoil element and also provide for laminar flow in at least a portion of the slot region. The method of the invention is one for inducing natural laminar flow over an airfoil. In the method, a fore airfoil element, having a leading and trailing edge, and an aft airfoil element define a slot region. Natural laminar flow is induced over substantially all of the fore airfoil element, by inducing the pressures on both surfaces of the fore airfoil element to decrease to a location proximate the trailing edge of the fore airfoil element using pressures created by the aft airfoil element.

REFERENCES:
patent: 1433030 (1922-10-01), Page
patent: 1589780 (1926-06-01), Wragg
patent: 1770575 (1930-07-01), Ksoll
patent: 1895140 (1933-01-01), Stage
patent: 2041786 (1936-05-01), Stalker
patent: 2111274 (1938-03-01), Bellanca
patent: 2241521 (1941-05-01), Richard
patent: 2306015 (1942-12-01), Dornier
patent: 2507611 (1950-05-01), Pappas et al.
patent: 2576294 (1951-11-01), Geraci
patent: 3298636 (1967-01-01), Arnholdt
patent: 4146197 (1979-03-01), Grotz
patent: 4191349 (1980-03-01), Pravaz
patent: 4498646 (1985-02-01), Proksch et al.
patent: 4575030 (1986-03-01), Gratzer
patent: 4614320 (1986-09-01), Rutan
patent: 4813631 (1989-03-01), Gratzer
patent: 4856735 (1989-08-01), Lotz et al.
patent: 4976349 (1990-12-01), Adkins
patent: 5294080 (1994-03-01), Ross
patent: 5342004 (1994-08-01), Bobbitt
patent: 5788190 (1998-08-01), Siers
patent: 6293497 (2001-09-01), Kelley-Wickemeyer et al.
patent: 6328265 (2001-12-01), Dizdarevic
patent: 6435458 (2002-08-01), Bliesner
patent: 6464171 (2002-10-01), Ruffin
patent: 6607164 (2003-08-01), Somers
Whitcomb, Richard T. and Clark, Larry R., “An Airfoil Shape for Efficient Flight at Supercritical Mach Numbers.” NASA TM X-1109, 1965, pp. 1-57 (Springfield, VA).
Steen, Gregory G., “A Two Element Laminar Flow Airfoil Optimized for Cruise,” AIAA Paper 95-0014, Jan. 9-12, 1995, pp. 1-11 (Washington, D.C.).
R.W. Barnwell et al., “Natural Laminar Flow and Laminar Flow Control”, 1992, Space Systems Division, NASA Langley Research Center, pp. 1-71.

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 airfoil 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 airfoil, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Laminar-flow airfoil will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-3474087

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