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Class Information
Number: 244/35R
Name: Aeronautics > Aircraft sustentation > Sustaining airfoils
Description:
Sub-classes under this class:
Patents under this class:
| Patent Number |
Title Of Patent |
Date Issued |
| 7475848 |
Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance |
Jan. 13, 2009 |
| 7467762 |
Advanced unmanned aerial vehicle system |
Dec. 23, 2008 |
| 7422051 |
System and method for using a flexible composite surface for pressure-drop free heat transfer enhancement and flow drag reduction |
Sep. 9, 2008 |
| 7410133 |
Miniature trailing edge effector for aerodynamic control |
Aug. 12, 2008 |
| 7185851 |
Inflatable aerodynamic wing and method |
Mar. 6, 2007 |
| 7093792 |
Laminar-flow airfoil |
Aug. 22, 2006 |
| 7065957 |
Segmented mixing device for jet engines and aircraft |
Jun. 27, 2006 |
| 7048228 |
Slotted aircraft wing |
May. 23, 2006 |
| 7032864 |
Wing with inflatable struts |
Apr. 25, 2006 |
| 7007889 |
Flexible airfoils and method |
Mar. 7, 2006 |
| 7004428 |
Lift and twist control using trailing edge control surfaces on supersonic laminar flow wings |
Feb. 28, 2006 |
| 6905092 |
Laminar-flow airfoil |
Jun. 14, 2005 |
| 6834830 |
Main wing structure |
Dec. 28, 2004 |
| 6802474 |
Advanced high turning compressor airfoils |
Oct. 12, 2004 |
| 6688553 |
Inflatable airfoils, and elevated and propulsion driven vehicles |
Feb. 10, 2004 |
| 6659403 |
Inflatable airfoils, and elevated and propulsion driven vehicles |
Dec. 9, 2003 |
| 6651927 |
Airfoil trailing edge |
Nov. 25, 2003 |
| 6626397 |
Autonomous flying wing |
Sep. 30, 2003 |
| 6607164 |
Wing airfoil |
Aug. 19, 2003 |
| 6592072 |
Spanwise tailoring of divergent trailing edge wings |
Jul. 15, 2003 |
| 6588703 |
Passive aerodynamic sonic boom suppression for supersonic aircraft |
Jul. 8, 2003 |
| 6587762 |
Automatic guidance unit for aerial delivery unit |
Jul. 1, 2003 |
| 6578798 |
Airlifting surface division |
Jun. 17, 2003 |
| 6508436 |
Inflatable airfoils, and elevated and propulsion driven vehicles |
Jan. 21, 2003 |
| 6485590 |
Method of forming a multilayer ceramic coating |
Nov. 26, 2002 |
| 6478251 |
Flier structure |
Nov. 12, 2002 |
| 6419189 |
Hot ruddervator apparatus and method for an aerospacecraft |
Jul. 16, 2002 |
| 6419187 |
Profile |
Jul. 16, 2002 |
| 6398160 |
Inflatable airfoils, and elevated and propulsion driven vehicles |
Jun. 4, 2002 |
| 6386481 |
Arrangement for fastening stringers to aircraft wing ribs |
May. 14, 2002 |
| 6382561 |
Trailing edge wedge for an aircraft wing |
May. 7, 2002 |
| 6378802 |
Enhance aerodynamic profile |
Apr. 30, 2002 |
| 6367740 |
Air foil having a hybrid leading edge construction |
Apr. 9, 2002 |
| 6361279 |
Blade profile for aircraft rotor and rotor comprising same |
Mar. 26, 2002 |
| 6341247 |
Adaptive method to control and optimize aircraft performance |
Jan. 22, 2002 |
| 6267331 |
Airfoil with dynamic stall control by oscillatory forcing |
Jul. 31, 2001 |
| 6260798 |
High-G compact folding wing |
Jul. 17, 2001 |
| 6237873 |
Composite material wing structure |
May. 29, 2001 |
| 6199796 |
Adaptive pneumatic wing for fixed wing aircraft |
Mar. 13, 2001 |
| 6179248 |
Aircraft |
Jan. 30, 2001 |
| 6165600 |
Gas turbine engine component having a thermal-insulating multilayer ceramic coating |
Dec. 26, 2000 |
| 6152405 |
Lift body having a variable camber |
Nov. 28, 2000 |
| 6149101 |
Aircraft wing and fuselage contours |
Nov. 21, 2000 |
| 6138957 |
Swept-back wings with airflow channeling |
Oct. 31, 2000 |
| 6119978 |
Leading edge structure of aircraft airfoil and method of fabricating the same |
Sep. 19, 2000 |
| 6116539 |
Aeroelastically stable forward swept wing |
Sep. 12, 2000 |
| 6098927 |
Multi-purpose aircraft |
Aug. 8, 2000 |
| 6098923 |
Aircraft structure to improve directional stability |
Aug. 8, 2000 |
| 6095457 |
Airfoil and wing configuration |
Aug. 1, 2000 |
| 6089502 |
Blunt-leading-edge raked wingtips |
Jul. 18, 2000 |
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