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Class Information
Number: 244/130
Name: Aeronautics > Aircraft structure > Details > Aerodynamic resistance reducing
Description: Devices and structural arrangements for reducing the resistance of aircraft or aircraft elements to motion through the air.
Patents under this class:
| Patent Number |
Title Of Patent |
Date Issued |
| 7607607 |
De-rotation system suitable for use with a shaft fairing system |
Oct. 27, 2009 |
| 7604201 |
Nacelle drag reduction device for a turbofan gas turbine engine |
Oct. 20, 2009 |
| 7562845 |
Rudder unit connection to a fuselage without a bolt-fairing structure |
Jul. 21, 2009 |
| 7510144 |
Elastic pre-deformed fairings for aircrafts |
Mar. 31, 2009 |
| 7478781 |
Joint cover in aircraft |
Jan. 20, 2009 |
| 7475853 |
Method and system for regulating external fluid flow over an object's surface, and particularly a wing and diffuser |
Jan. 13, 2009 |
| 7413262 |
Hub for wheel of human powered vehicle |
Aug. 19, 2008 |
| 7410133 |
Miniature trailing edge effector for aerodynamic control |
Aug. 12, 2008 |
| 7407135 |
Aircraft provided with a belly fairing, and corresponding belly fairing |
Aug. 5, 2008 |
| 7392963 |
Supersonic flight vehicle |
Jul. 1, 2008 |
| 7380756 |
Single dielectric barrier aerodynamic plasma actuation |
Jun. 3, 2008 |
| 7357351 |
Linear shock wave absorber |
Apr. 15, 2008 |
| 7334760 |
Flow control device and method of controlling flow |
Feb. 26, 2008 |
| 7331752 |
Method of conversion of continuous medium flow energy and device for conversion of continuous medium flow energy |
Feb. 19, 2008 |
| 7311287 |
Methods for incorporating area ruled surfaces in a supersonic aircraft |
Dec. 25, 2007 |
| 7309046 |
Method for determination of fuselage shape of supersonic aircraft, and fuselage front section shape |
Dec. 18, 2007 |
| 7278609 |
Movable nose cap and control strut assembly for supersonic aircraft |
Oct. 9, 2007 |
| 7278825 |
Method and system for regulating fluid over an airfoil or a hydrofoil |
Oct. 9, 2007 |
| 7270520 |
Fairing for the rotor of a rotorscraft |
Sep. 18, 2007 |
| 7252263 |
Design methods and configurations for supersonic aircraft |
Aug. 7, 2007 |
| 7216922 |
Fairing panel retainer apparatus |
May. 15, 2007 |
| 7150434 |
Vehicle wake vortex modifier |
Dec. 19, 2006 |
| 7150435 |
Type aircraft |
Dec. 19, 2006 |
| 7121511 |
Shock wave modification method and system |
Oct. 17, 2006 |
| 7118072 |
Method for reducing resistance of flying object using expandable nose cone |
Oct. 10, 2006 |
| 7118071 |
Methods and systems for controlling lower surface shocks |
Oct. 10, 2006 |
| 7114785 |
Aerodynamic surfaced bicycle wheel |
Oct. 3, 2006 |
| 7108225 |
More aerodynamic wheel fairings for small airplanes |
Sep. 19, 2006 |
| 7100867 |
Lifting foil |
Sep. 5, 2006 |
| 7070146 |
Aircraft thickness/camber control device for low sonic boom |
Jul. 4, 2006 |
| 7070850 |
Drag reduction article and method of use |
Jul. 4, 2006 |
| 7063289 |
Helicopter tail section |
Jun. 20, 2006 |
| 7048230 |
Laminar flow nacelle for an aircraft engine |
May. 23, 2006 |
| 7048505 |
Method and system for regulating fluid flow over an airfoil or a hydrofoil |
May. 23, 2006 |
| 7041363 |
Solid body with microstructured surface |
May. 9, 2006 |
| 7000870 |
Laminar flow wing for transonic cruise |
Feb. 21, 2006 |
| 6986484 |
VTOL aircraft external load drag reduction system |
Jan. 17, 2006 |
| 6978971 |
Methods and apparatuses for controlling airflow proximate to engine/airfoil systems |
Dec. 27, 2005 |
| 6969029 |
Methods and systems for removing material from aircraft flight surfaces |
Nov. 29, 2005 |
| 6964397 |
Nacelle chine installation for drag reduction |
Nov. 15, 2005 |
| 6957792 |
Lifting arrangement for aircraft fuselages |
Oct. 25, 2005 |
| 6908063 |
Vortex shedding and drag force reduction |
Jun. 21, 2005 |
| 6899302 |
Method and device for altering the separation characteristics of flow over an aerodynamic surface via hybrid intermittent blowing and suction |
May. 31, 2005 |
| 6892989 |
Method for reducing the drag of blunt-based vehicles by adaptively increasing forebody roughness |
May. 17, 2005 |
| 6869045 |
Helicopter tail section and retrofit method |
Mar. 22, 2005 |
| 6863245 |
Aerodynamic profile with an adjustable flap |
Mar. 8, 2005 |
| 6857604 |
Shock wave absorber |
Feb. 22, 2005 |
| 6857598 |
Integrated high-speed aircraft and associated methods of manufacture |
Feb. 22, 2005 |
| 6854687 |
Nacelle integration with reflexed wing for sonic boom reduction |
Feb. 15, 2005 |
| 6824092 |
Aircraft tail configuration for sonic boom reduction |
Nov. 30, 2004 |
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