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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:
| 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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