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Class Information
Number: 60/228
Name: Power plants > Reaction motor (e.g., motive fluid generator and reaction nozzle, etc.) > With thrust direction modifying means
Description: Apparatus having means which may so direct all or a portion of the motive fluid that the direction of thrust produced by the motor is altered.
Sub-classes under this class:
Patents under this class:
| Patent Number |
Title Of Patent |
Date Issued |
| 7599768 |
Method for computer-assisted determination of an optimum-fuel control of nozzles |
Oct. 6, 2009 |
| 7581381 |
Ducted air power plant |
Sep. 1, 2009 |
| 7578472 |
Aircraft ejection seat system |
Aug. 25, 2009 |
| 7559507 |
Thrust reversers including locking assemblies for inhibiting deflection |
Jul. 14, 2009 |
| 7555894 |
Swivelling exhaust nozzle for an aircraft engine |
Jul. 7, 2009 |
| 7555893 |
Aircraft propulsion system |
Jul. 7, 2009 |
| 7509797 |
Thrust vectoring missile turbojet |
Mar. 31, 2009 |
| 7481038 |
Yaw vectoring for exhaust nozzle |
Jan. 27, 2009 |
| 7406821 |
Adapter device for a rocket engine nozzle having a movable diverging portion |
Aug. 5, 2008 |
| 7313910 |
Jet vane thrust vector control system |
Jan. 1, 2008 |
| 7174718 |
Device for controlling propulsive jet mixing for aircraft jet engines |
Feb. 13, 2007 |
| 7134271 |
Thrust vectoring aft FLADE engine |
Nov. 14, 2006 |
| 6948307 |
Rocket engine nozzle that is steerable by means of a moving diverging portion on a cardan mount |
Sep. 27, 2005 |
| 6745570 |
Methods and apparatus for sealing gas turbine engine nozzles using a flap system |
Jun. 8, 2004 |
| 6681560 |
Nozzle throat area control apparatus and method |
Jan. 27, 2004 |
| 6631314 |
Propellant utilization system |
Oct. 7, 2003 |
| 6598385 |
Two stage gas pilot valve controlling gas flow to a reaction jet nozzle |
Jul. 29, 2003 |
| 6532730 |
Slip joint duct system for a rocket fuel duct |
Mar. 18, 2003 |
| 6520450 |
V/STOL aircraft |
Feb. 18, 2003 |
| 6315239 |
Variable coupling arrangement for an integrated missile steering system |
Nov. 13, 2001 |
| 6192671 |
Cross bar centering mechanism for slave petals in covergent divergent nozzles with variable geometry |
Feb. 27, 2001 |
| 6170253 |
Cascade structure arrangement for a gas turbine engine |
Jan. 9, 2001 |
| 6134873 |
Method of operating a combustion turbine power plant at full power at high ambient temperature or at low air density using supplemental compressed air |
Oct. 24, 2000 |
| 6105901 |
Thrust vectoring system |
Aug. 22, 2000 |
| 6105364 |
Vstovl engines |
Aug. 22, 2000 |
| 6102329 |
Flow diverter system for multiple streams for gas turbine engine |
Aug. 15, 2000 |
| 6042053 |
Automatic restow system for aircraft thrust reverser |
Mar. 28, 2000 |
| 5903432 |
Computer package with a polygonal shaped motherboard |
May. 11, 1999 |
| 5752381 |
Method and apparatus for vectoring thrust employing electrodes generating voltages greater than the dielectric breakdown voltage |
May. 19, 1998 |
| 5598701 |
Frangible connection for a thrust reverser for a ducted fan gas turbine |
Feb. 4, 1997 |
| 5485959 |
Axisymmetric vectoring exhaust nozzle thermal shield |
Jan. 23, 1996 |
| 5383332 |
Gas turbine engines |
Jan. 24, 1995 |
| 5329763 |
Thrust vectoring variable geometry exhaust nozzle for gas turbines |
Jul. 19, 1994 |
| 5245823 |
External flap vectoring mechanism |
Sep. 21, 1993 |
| 5239815 |
Sync-ring assembly for a gas turbine engine exhaust nozzle |
Aug. 31, 1993 |
| 5205512 |
Fluid control apparatus |
Apr. 27, 1993 |
| 5174502 |
Support for a translating nozzle vectoring ring |
Dec. 29, 1992 |
| 5154050 |
Thrust vector control using internal airfoils |
Oct. 13, 1992 |
| 5142862 |
Thrust reversing system for high bypass fan engines |
Sep. 1, 1992 |
| 5120005 |
Exhaust flap speedbrake |
Jun. 9, 1992 |
| 5103634 |
Thrust reversing system and method |
Apr. 14, 1992 |
| 5082209 |
Thrust reverser assembly |
Jan. 21, 1992 |
| 5079912 |
Convergent side disk cooling system for a two-dimensional nozzle |
Jan. 14, 1992 |
| 5054285 |
Thrust reverser for turbofan engine |
Oct. 8, 1991 |
| 5039014 |
Axisymmetric vectoring exhaust nozzle seal |
Aug. 13, 1991 |
| 4994660 |
Axisymmetric vectoring exhaust nozzle |
Feb. 19, 1991 |
| 4991393 |
Spacecraft guidance and control system |
Feb. 12, 1991 |
| 4878617 |
Triple axis thrust vectoring exhaust nozzle |
Nov. 7, 1989 |
| 4830519 |
Annular seal assembly |
May. 16, 1989 |
| 4787201 |
Method and apparatus for controlling multiple engine aircraft |
Nov. 29, 1988 |
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