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Class Information
Number: 60/226.1
Name: Power plants > Reaction motor (e.g., motive fluid generator and reaction nozzle, etc.) > Interrelated reaction motors > Air and diverse fluid discharge from separate discharge outlets (e.g., fan jet, etc.)
Description: Apparatus wherein at least one of the motive fluids is air.
Sub-classes under this class:
Patents under this class:
| Patent Number |
Title Of Patent |
Date Issued |
| 6205771 |
Ducted fan gas turbine engine control system |
Mar. 27, 2001 |
| 6195983 |
Leaned and swept fan outlet guide vanes |
Mar. 6, 2001 |
| 6178740 |
Turbo fan engine nacelle exhaust system with concave primary nozzle plug |
Jan. 30, 2001 |
| 6173566 |
Casing construction on a gas turbine jet engine |
Jan. 16, 2001 |
| 6170252 |
Locator for a gearbox mount |
Jan. 9, 2001 |
| 6158210 |
Gear driven booster |
Dec. 12, 2000 |
| 6151882 |
Turbofan engine construction |
Nov. 28, 2000 |
| 6145300 |
Integrated fan / low pressure compressor rotor for gas turbine engine |
Nov. 14, 2000 |
| 6134880 |
Turbine engine with intercooler in bypass air passage |
Oct. 24, 2000 |
| 6127758 |
Ram air turbine system |
Oct. 3, 2000 |
| 6125626 |
Active rotor stage vibration control |
Oct. 3, 2000 |
| 6112514 |
Fan noise reduction from turbofan engines using adaptive Herschel-Quincke tubes |
Sep. 5, 2000 |
| 6109022 |
Turbofan with frangible rotor support |
Aug. 29, 2000 |
| 6102329 |
Flow diverter system for multiple streams for gas turbine engine |
Aug. 15, 2000 |
| 6098399 |
Ducted fan gas turbine engine |
Aug. 8, 2000 |
| 6094907 |
Jet engine and method for reducing jet engine noise by reducing nacelle boundary layer thickness |
Aug. 1, 2000 |
| 6079200 |
Ducted fan gas turbine engine with fan shaft frangible connection |
Jun. 27, 2000 |
| 6079667 |
Auxiliary inlet for a jet engine |
Jun. 27, 2000 |
| 6073439 |
Ducted fan gas turbine engine |
Jun. 13, 2000 |
| 6070407 |
Ducted fan gas turbine engine with variable area fan duct nozzle |
Jun. 6, 2000 |
| 6068213 |
Aircraft engine ducted fan cowling with thrust reverser section and fairings for fan shroud brace members in fan exhaust duct |
May. 30, 2000 |
| 6058696 |
Inlet and outlet module for a heat exchanger for a flowpath for working medium gases |
May. 9, 2000 |
| 6055805 |
Active rotor stage vibration control |
May. 2, 2000 |
| 6041589 |
Asymmetric turboprop booster |
Mar. 28, 2000 |
| 6009701 |
Ducted fan gas turbine engine having a frangible connection |
Jan. 4, 2000 |
| 5998882 |
Apparatus for converting aircraft exhaust into useful energy |
Dec. 7, 1999 |
| 5996336 |
Jet engine having radial turbine blades and flow-directing turbine manifolds |
Dec. 7, 1999 |
| 5947412 |
Jet engine noise suppressor assembly |
Sep. 7, 1999 |
| 5941061 |
Aircraft propulsive power unit assembly having a leading edge lipskin and intake barrel |
Aug. 24, 1999 |
| 5924632 |
Jet nozzle having centerbody for enhanced exit area mixing |
Jul. 20, 1999 |
| 5916127 |
Method of eliminating Mach waves from supersonic jets |
Jun. 29, 1999 |
| 5906097 |
Engine flow control device |
May. 25, 1999 |
| 5894721 |
Noise reducing stator assembly for a gas turbine engine |
Apr. 20, 1999 |
| 5887822 |
Segmented engine flow control device |
Mar. 30, 1999 |
| 5867979 |
Gas turbine engine system |
Feb. 9, 1999 |
| 5867980 |
Turbofan engine with a low pressure turbine driven supercharger in a bypass duct operated by a fuel rich combustor and an afterburner |
Feb. 9, 1999 |
| 5860276 |
Ducted fan gas turbine engine mounting |
Jan. 19, 1999 |
| 5860275 |
Method of combining ducted fan gas turbine engine modules and aircraft structure |
Jan. 19, 1999 |
| 5848526 |
Noise reducing stator assembly for a gas turbine engine |
Dec. 15, 1998 |
| 5822975 |
Bypass engine with means for limiting gas leakage |
Oct. 20, 1998 |
| 5816042 |
Flow diverter system for multiple streams for gas turbine engines |
Oct. 6, 1998 |
| 5809772 |
Turbofan engine with a core driven supercharged bypass duct |
Sep. 22, 1998 |
| 5806302 |
Variable fan exhaust area nozzle for aircraft gas turbine engine with thrust reverser |
Sep. 15, 1998 |
| 5806303 |
Turbofan engine with a core driven supercharged bypass duct and fixed geometry nozzle |
Sep. 15, 1998 |
| 5794432 |
Variable pressure and variable air flow turbofan engines |
Aug. 18, 1998 |
| 5782077 |
Device for bleeding off and cooling hot air in an aircraft engine |
Jul. 21, 1998 |
| 5782082 |
Aircraft engine acoustic liner |
Jul. 21, 1998 |
| 5778659 |
Variable area fan exhaust nozzle having mechanically separate sleeve and thrust reverser actuation systems |
Jul. 14, 1998 |
| 5771681 |
Aircraft turbofan engine mixing apparatus |
Jun. 30, 1998 |
| 5771680 |
Stiffened composite structures and method of making thereof |
Jun. 30, 1998 |
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