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Class Information
Number: 244/117A
Name: Aeronautics > Aircraft structure > Skin cooling
Description:
Patents under this class:
| Patent Number |
Title Of Patent |
Date Issued |
| 7401682 |
Architecture for an acoustic liner |
Jul. 22, 2008 |
| 7325772 |
Aircraft heat sink and electronics enclosure |
Feb. 5, 2008 |
| 7311175 |
Acoustic liner with bypass cooling |
Dec. 25, 2007 |
| 7232093 |
Cooled insulation surface temperature control system |
Jun. 19, 2007 |
| 7121512 |
Drain particularly for engine support strut |
Oct. 17, 2006 |
| 6857602 |
Environmental control system and method of using the same |
Feb. 22, 2005 |
| 6612523 |
Aircraft structures having improved through-thickness thermal conductivity |
Sep. 2, 2003 |
| 6578491 |
Externally accessible thermal ground plane for tactical missiles |
Jun. 17, 2003 |
| 6435454 |
Heat pipe cooling of aircraft skins for infrared radiation matching |
Aug. 20, 2002 |
| 6241184 |
Vehicle having a ceramic radome joined thereto by an actively brazed compliant metallic transition element |
Jun. 5, 2001 |
| 6178865 |
Thermally massive radar decoy |
Jan. 30, 2001 |
| 6027072 |
Payload chamber cooling system |
Feb. 22, 2000 |
| 5979831 |
System and method for attaching a structural component to an aerospace vehicle |
Nov. 9, 1999 |
| 5897076 |
High-efficiency, supersonic aircraft |
Apr. 27, 1999 |
| 5882765 |
Element made of a reinforced low density heat protective material and method to obtain said element |
Mar. 16, 1999 |
| 5806793 |
Cooling device for a turboshaft engine on an aircraft |
Sep. 15, 1998 |
| 5803159 |
Integrated fin-heat pipe |
Sep. 8, 1998 |
| 5794888 |
System for removing incident heat from aircraft during flight |
Aug. 18, 1998 |
| 5785113 |
Cooling system for optical port |
Jul. 28, 1998 |
| 5758845 |
Vehicle having a ceramic radome with a compliant, disengageable attachment |
Jun. 2, 1998 |
| 5702073 |
Modular liquid skin heat exchanger |
Dec. 30, 1997 |
| 5667168 |
Modular liquid skin heat exchanger |
Sep. 16, 1997 |
| 5649488 |
Non-explosive target directed reentry projectile |
Jul. 22, 1997 |
| 5598989 |
Spacecraft protective blanket |
Feb. 4, 1997 |
| 5593112 |
Nacelle air pump for vector nozzles for aircraft |
Jan. 14, 1997 |
| 5560569 |
Aircraft thermal protection system |
Oct. 1, 1996 |
| 5484122 |
Turbine exhaust gas anti-ice system |
Jan. 16, 1996 |
| 5452866 |
Transpiration cooling for a vehicle with low radius leading edge |
Sep. 26, 1995 |
| 5423498 |
Modular liquid skin heat exchanger |
Jun. 13, 1995 |
| 5372333 |
Seeker head assembly in a guided missile |
Dec. 13, 1994 |
| 5351917 |
Transpiration cooling for a vehicle with low radius leading edges |
Oct. 4, 1994 |
| 5340058 |
Projectile with cooled nose cone |
Aug. 23, 1994 |
| 5330124 |
Thermal protection device using the vaporization and superheating of a rechargeable liquid |
Jul. 19, 1994 |
| 5312693 |
Nonsacrificial laser hardening |
May. 17, 1994 |
| 5305973 |
Temperature normalized structure |
Apr. 26, 1994 |
| 5299762 |
Injection-cooled hypersonic leading edge construction and method |
Apr. 5, 1994 |
| 5291830 |
Dual-mode semi-passive nosetip for a hypersonic weapon |
Mar. 8, 1994 |
| 5284095 |
Compartment for electric circuits |
Feb. 8, 1994 |
| 5257757 |
Advanced hypersonic nosecap |
Nov. 2, 1993 |
| 5236151 |
Thermal barrier structure |
Aug. 17, 1993 |
| 5236152 |
Cooling/fuel system for hypersonic flight |
Aug. 17, 1993 |
| 5178922 |
Fringed thermal protection device |
Jan. 12, 1993 |
| 5174524 |
Cooling system for high speed aircraft |
Dec. 29, 1992 |
| 5173350 |
Thermal protection coating comprising a fiber reinforced main layer and an insulative sublayer |
Dec. 22, 1992 |
| 5154373 |
Integral structure and thermal protection system |
Oct. 13, 1992 |
| 5151171 |
Method of cooling with an endothermic fuel |
Sep. 29, 1992 |
| 5149018 |
Cooling system for a hypersonic aircraft |
Sep. 22, 1992 |
| 5135184 |
Propellant utilization system |
Aug. 4, 1992 |
| 5112008 |
Fin stabilized projectile having heat resistant fins |
May. 12, 1992 |
| 5079912 |
Convergent side disk cooling system for a two-dimensional nozzle |
Jan. 14, 1992 |
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