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Class Information
Number: 244/214
Name: Aeronautics > Aircraft sustentation > Sustaining airfoils > With lift modification > Variable > By flap and/or spoiler > At leading edge
Description: A flap located at the leading edge of the airfoil.


Patents under this class:
1 2 3

Patent Number Title Of Patent Date Issued
7448578 Aircraft with forward opening inlay spoilers for yaw control Nov. 11, 2008
7437955 Device for determining the rotation angle of a shaft in an aircraft Oct. 21, 2008
7357358 Aircraft leading edge device systems and corresponding sizing methods Apr. 15, 2008
7322547 Aerospace vehicle leading edge slat devices and corresponding methods Jan. 29, 2008
7270305 Aircraft leading edge apparatuses and corresponding methods Sep. 18, 2007
7264206 Leading edge flap apparatuses and associated methods Sep. 4, 2007
7249735 Translating conduit apparatus for an airplane or equipment Jul. 31, 2007
7216835 Aircraft with extendable leading edge of fuselage and wings May. 15, 2007
7101297 Compact actuator Sep. 5, 2006
7051982 Fairing arrangements for aircraft May. 30, 2006
6978971 Methods and apparatuses for controlling airflow proximate to engine/airfoil systems Dec. 27, 2005
6974112 Deployment system for a moveable wing surface Dec. 13, 2005
6796534 Method and apparatus for controlling airflow with a leading edge device having a flexible flow surface Sep. 28, 2004
6789769 Flexible airflow separator to reduce aerodynamic noise generated by a leading edge slat of an aircraft wing Sep. 14, 2004
6682023 Contiguous variable camber device Jan. 27, 2004
6536714 Pressure control system for a pressure-expandable displacement element Mar. 25, 2003
6530544 Device and mechanism for transmission of radial forces between the central and end regions of this device Mar. 11, 2003
6513754 Transonic flow shockwave position stabilizer Feb. 4, 2003
6464167 Vehicle with vertical wings and a stabilizing torque system of jets to use fluid energy for forward motion Oct. 15, 2002
6457680 Auxiliary airfoil for aircraft main wings Oct. 1, 2002
6454219 Aircraft wing and method for reducing airframe-generated noise Sep. 24, 2002
6435458 Tailored wing assembly for an aircraft moveable slat system Aug. 20, 2002
6394396 Aerodynamic noise reducing structure for aircraft wing slats May. 28, 2002
6375126 Variable camber leading edge for an airfoil Apr. 23, 2002
6371415 Aerodynamic component with a leading edge flap Apr. 16, 2002
6364254 Aircraft airfoil with close-mounted engine and leading edge high lift system Apr. 2, 2002
6328265 Slot forming segments and slot changing spoilers Dec. 11, 2001
6318677 Method and apparatus for generating a stable leading-edge lifting-vortex controller Nov. 20, 2001
6286790 Aerofoil having a slat with flexible data link Sep. 11, 2001
6231012 No-back/offset gear box May. 15, 2001
6213433 Leading edge for an aircraft Apr. 10, 2001
6152404 Apparatus for influencing a wing root airflow in an aircraft Nov. 28, 2000
6149105 Deployment mechanisms for aircraft auxiliary airfoils Nov. 21, 2000
6138954 Aircraft funnel slat system Oct. 31, 2000
6135395 Aircraft wing leading edge high lift device with suction Oct. 24, 2000
6123297 Segmented flap with variable camber for aircraft wing Sep. 26, 2000
6076776 Profile edge of an aerodynamic profile Jun. 20, 2000
6073889 Wing flap seal bump Jun. 13, 2000
6015117 Variable camber wing mechanism Jan. 18, 2000
5947422 Tail for an aircraft Sep. 7, 1999
5931422 Active reinforced elastomer system Aug. 3, 1999
5927656 Wing leading edge flap and method therefor Jul. 27, 1999
5921506 Extendible leading edge flap Jul. 13, 1999
5897076 High-efficiency, supersonic aircraft Apr. 27, 1999
5842666 Laminar supersonic transport aircraft Dec. 1, 1998
5839699 Leading edge slat/wing combination Nov. 24, 1998
5839698 Control surface continuous seal Nov. 24, 1998
5836550 Mechanism for streamwise fowler deployment of the wing trailing or leading edge Nov. 17, 1998
5740991 Method and apparatus for optimizing the aerodynamic effect of an airfoil Apr. 21, 1998
5711496 STOL aircraft and wing slat actuating mechanism for same Jan. 27, 1998

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