Aircraft wing

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

244113, B64C 350

Patent

active

040157873

ABSTRACT:
An aircraft wing having a relatively thin airfoil cross section including a main body portion and a plurality of auxiliary airfoil sections disposed at the trailing edge of the wing and movable relative to the main body portion and to one another. In a normal cruise position the auxiliary sections and the main body portion form a complete airfoil having a substantially contiguous and unbroken exterior airfoil surface which preserves the high speed characteristics of the wing. At least two of the auxiliary sections comprising a leading auxiliary section and a trailing auxiliary section are movable about a common hinge member carried by the main body portion, while another auxiliary section also hingedly connected to the main body portion is positioned relative thereto in response to the position of the other auxiliary sections. The movement of these auxiliary sections is programmed and operable by a position regulating mechanism that is contained within the confines of the relatively thin airfoil and is operable to substantially improve the wings lift generating capability by cooperating to provide a highly cambered airfoil when deployed while simultaneously exposing a duct to channel ram air flow in a manner which will accelerate the flow and augment the boundary layer flow over the airfoil and its deployed auxiliary airfoil sections. The auxiliary sections are also capable of being deployed so that they extend significantly into the airstream above and below the exterior surfaces of the main body portion and thereby spoil the air flow and create an aerodynamic brake which is caused by the exposure of the large surfaces to the airstream and the effective trapping of a large volume of air within the confined duct area fromed by deploying the auxiliary sections in this manner.

REFERENCES:
patent: 2772058 (1956-11-01), Grant
patent: 2899152 (1959-08-01), Weiland
patent: 2920844 (1960-01-01), Marshall et al.
patent: 3921942 (1975-11-01), Bracka

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

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

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

Rate now

     

Profile ID: LFUS-PAI-O-2263058

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