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Variable airfoil assembly

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64C-003/48    B64C-009/32   
미국특허분류(USC) 244/219 ; 244/113 ; 244/218
출원번호 US-0914673 (1978-06-09)
발명자 / 주소
인용정보 피인용 횟수 : 8  인용 특허 : 1
초록
▼

The present variable airfoil assembly has an adjustable airfoil member pivotally mounted in the top of a fixed airfoil member for adjustment between a fully lowered position (for minimum wind resistance) and different raised positions in which it projects up above the top surface of the fixed airfoil member to control the lift and drag. A minimum clearance between the fixed and adjustable airfoil members is provided at the front end of the adjustable airfoil member over a range of its pivotal adjustments. The variable airfoil assembly is capable of incre...

대표
청구항
▼

In a variable airfoil assembly having: a fixed airfoil member with a bottom wall, a convex nose extending upward and curving rearward from the front end of said bottom wall to a top wall segment which terminates in a transverse edge at the front of a recess in the top of the fixed airfoil member above said bottom wall; and an adjustable airfoil member in said recess pivotally mounted away from its front end for adjustment between a fully lowered position fitting in said recess and raised positions in which its front end extends up from the top of said fi...

이 특허에 인용된 특허 (1)

  1. Reynolds ; III Collins J. (1615 Krameria St. Denver CO 80220). Upwardly extendible wing flap system. USP1977024007896.

이 특허를 인용한 특허 피인용횟수: 8

  1. Clark,Walter Dennis. Aircraft with forward opening inlay spoilers for yaw control. USP2008117448578.
  2. Nahas, Roger A.. Auxiliary wing and flap assembly for an aircraft. USP2010067740205.
  3. Weber, Carsten; Fischer, Markus; Grote, Arne; Radespiel, Rolf; Dreyer, Martin. Device and method for increasing the aerodynamic lift of an aircraft. USP2015119193444.
  4. Kastner, Mark A.. Gas-discharge lamp having brightness control. USP2003056570347.
  5. Rao Dhanvada M. (Hampton VA). Leading edge flap system for aircraft control augmentation. USP1984124485992.
  6. Motosko, III, Stephen. Variable air foil and spoiler. USP2012028113470.
  7. Muscatell Ralph P. (2007 NE. 20th Ave. Fort Lauderdale FL 33305). Variable airfoil assembly. USP1984024432516.
  8. Dorsett, Kenneth M.. Vortex generation. USP2016119505485.

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