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4174610 |
Power cruise diverter valve
An air control valve for use in the exhaust emission control system of an internal combustion engine as used for example, in a vehicle, the air control valve, which is adapted to perform three...
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4167097 |
Gas turbine engines with improved compressor-combustor interfaces
Gas turbine engines with interfaces between a compressor and a combustor which minimize disturbances in the pattern of air flowing from the compressor to the combustor. Provision is also made for...
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4154056 |
Fuel nozzle assembly for a gas turbine engine
A fuel nozzle assembly having a nozzle tip disposed in one end of a fuel delivery tube supported in a mounting flange. An air delivery tube, also secured to said support flange, encloses the fuel...
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4075562 |
Speed sensor mounting for a gas turbine
A speed sensor mounting assembly for a gas turbine speed sensor insures a magnetic speed sensing device is positioned a predetermined distance from a toothed wheel mounted on the output shaft of...
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4037404 |
Coupling device for gas turbine engine
A gas turbine engine of the type comprising a compressor and an expansion rbine of which the respective rotors are mutually joined together in rotation and in axial traction by a main coupling...
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4028888 |
Fuel distribution manifold to an annular combustion chamber
A fuel distribution system for a gas turbine-compressor includes means permitting ready replacement and maintenance of individual fuel nozzles without disassembly of the entire fuel nozzle system....
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4016718 |
Gas turbine engine having an improved transition duct support
An axial flow gas turbine engine is provided with a plurality of combustion chambers distributed circumferentially about the engine axis and a plurality of transition ducts which carry propulsive...
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4009568 |
Turbine support structure
A gas turbine engine has a turbine shroud and back seal plate to define a gas flow passage across turbine rotor blades. A conically shaped turbine support plate for the shroud and back seal plate...
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4008568 |
Combustor support
A combustor assembly includes a porous, laminated metal dome and an elongated tubular body portion disposed vertically within an air supply plenum. The dome and body portion are joined by a...
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3977183 |
Adjusting mechanism and method for fuel control
The indexing of the power lever of a fuel control for a turbine type of power and the mechanism necessary to effectuate the same is simplified so as to facilitate the installation of the fuel...
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3959966 |
Gas turbine engine
The disclosure of this invention pertains to a gas turbine engine having an annular combustion chamber having an outlet duct to turbine entry vanes, an extension of the combustion chamber...
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3927521 |
Multicone exhaust diffuser system for a gas turbine
An exhaust system for hot motive fluid gases expelled from a gas turbine wherein the hot gases pass into an annular chamber, thereafter the gases are directed through a circumferential array of...
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3924403 |
Combustion liner spring support used for hot wire igniter circuit
A combustion liner for a gas turbine combustion apparatus is composed of a series of ceramic wall rings coaxially aligned from the upstream to the downstream end of the liner. The ceramic rings are...
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3911672 |
Combustor with ceramic liner
A combustor for a gas turbine engine embodies a ceramic liner the upstream or dome end of which has a central opening. The liner is supported from the combustion chamber housing by an annular...
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3910381 |
Lubricating oil system integral with structural steel turbine foundation
A support foundation for a turbogenerator power plant having an oil lubricating system integral with the structural steel of the foundation. An oil reservoir with associated pumping and conduit...
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3902314 |
Gas turbine engine frame structure
A gas turbine engine has an integral cast aft frame which includes an aft bearing housing interconnected by means of struts with sections defining the hot gas flow path through the frame. The frame...
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3860359 |
MOUNTING SYSTEM FOR GAS TURBINE POWER UNIT
A mounting system for a gas turbine power unit in which the stator housing is supported by an annular mounting ring having a radial spline connection to the stator housing, the mounting ring and...
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3845619 |
COMPOSITE HEAT-CONDUCTING MEANS
In a gas turbine engine the housing for the power turbine shaft is hollow and contains compacted copper powder.
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3800530 |
AIR COOLED AUGMENTER IGNITER ASSEMBLY
An augmenter igniter assembly for a mixed flow augmenter gas turbine engine is shown to include an airfoil-shaped, hollow housing which surrounds an electrical discharge-type igniter and provides a...
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3798899 |
GAS TURBINE ENGINE
A gas turbine engine including a compressor, a burner and a turbine. The turbine includes a stator, a rotor and a shroud about the periphery of the rotor. Means are provided for supporting the...
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3797236 |
ANNULAR COMBUSTION CHAMBER WITH CERAMIC ANNULAR RING
An annular combustion chamber for a gas turbine engine in which an annular wall part is made of a ring of ceramic material which is located in the chamber by compression between a frusto-conical...
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3791682 |
TURBINE DRIVEN ELECTRICAL GENERATOR
A turbine driven electrical driven generator set having one or more turbines positioned above the generator to provide a power source at locations where there is a minimum available floor space. An...
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3791142 |
FLUID-POWERED ENGINE
The engine, in one embodiment thereof, comprises an impulse velocity, staged turbine operative under the influence of energized fluid to provide thrust, or rotary torque, or both. Ancillary fluid...
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3768251 |
FIXING OF FUEL INJECTION MANIFOLDS INTO COMBUSTION CHAMBERS
A device for securing within a combustion chamber an injection manifold wh is connected to the wall of the said chamber by a pipe section preferably curved into a "swan-neck," said device...
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3742704 |
COMBUSTION CHAMBER SUPPORT STRUCTURE
A support structure for the upstream portion of a combustion chamber. The combustion chamber includes a conically shaped collar portion having a circumferential groove on its inner diameter...
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3740164 |
DEFLECTION CONTROL MEANS FOR MACHINE HOUSINGS
The housing is divided at an intermediate point and a ring having two mating annular parts is positioned between the divided housing parts. The mating parts of the ring are rotatable about a common...
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3738105 |
GAS TURBINE ENGINE STRUCTURE
The disclosure illustrates a gas turbine engine structure in which a turbine housing is structurally connected to a compressor housing by three equally spaced straight-lined struts. These struts...
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3722214 |
GEARBOX FOR CONTROLLING THE MECHANISMS OF A GAS TURBINE ENGINE HAVING ROTARY HEAT EXCHANGERS
A gearbox for driving the various accessories of a gas turbine provided with rotating heat exchangers. The gearbox has a triangular shape and fits on the front of the turbine. An electric starter...
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3710568 |
INTEGRAL TUBING AND/OR ELECTRICAL LEAD SUPPORT AND MOUNTING PAD FOR GAS TURBINE ENGINE CONTROLS AND ACCESSORIES
A new tubing (or electrical lead) support is combined with a new gas turbine engine control and accessory mounting pad, which also serves to communicate fluids/electrical signals to such controls...
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3702058 |
DOUBLE WALL COMBUSTION CHAMBER
A combustion chamber for a gas turbine power plant of the step-liner type including a plurality of annular double wall step-liner portions. The portions are of various sizes and are arranged...
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3685294 |
HOT GAS PUMPS AND THRUSTERS
This is a hot gas dredger or pump in which compressed air is mixed with fuel and ignited in a combustor near the end of a tube into which hot gases from the ignited fuel and air are directed in a...
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3670497 |
COMBUSTION CHAMBER SUPPORT
An annular combustion chamber having an inner and outer wall has its rear, downstream, end mounted to permit radial growth and meter cooling air to control the temperature at that location at...
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3657883 |
COMBUSTION CHAMBER CLUSTERING STRUCTURE
A gas turbine power plant having a combustion section defined by a casing structure divided into upper and lower semi-cylindrical casing halves along a horizontal plane. The casing halves encompass...
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3643439 |
COMPOUND REACTION PROPULSION MEANS WITH MULTIPLE THRUST
This power propulsion system involves compound reaction thrust for propulsion, and including supplementary air propulsion by supplementary propelled airstream impulse, and including pressurized...
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3612598 |
POWER PLANT HAVING COMPRESSOR-POWERED ASPIRATING SYSTEM
An enclosure for a gas turbine power plant in which the noise of the ventilating and the fuel air is at a minimum will be provided by the structure of the invention wherein the entering and...
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3576101 |
COMBINED DIESEL AND GAS TURBINE POWER UNIT
A vertically mounted turbine engine includes air inlet means surrounding, at least in part, an upwardly extending exhaust duct to cause substantial heat transfer between the hot exhaust gases and...
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3531937 |
FUEL VAPORIZER FOR GAS TURBINE ENGINES
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3498063 |
MULTIPLE-COMBUSTOR PULSE JET ENGINE STRUCTURE
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3462949 |
NOISE REDUCING ENCLOSURE FOR A GAS TURBINE ENGINE
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3398529 |
Arrangement of nozzle bodies of hooklike fuel injection nozzles at the combustion chamber of gas-turbine drive units
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3371482 |
Jet propulsion casings having fuel drainage means
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3367108 |
Articulated connections for ducts
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3327473 |
Engine support structure
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3303645 |
Ultra-high temperature burners
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3276204 |
Apparatus for supplying heated gases
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3269116 |
Centrally supported flameholder
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3269118 |
Accessory case mounting
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3238718 |
Gas turbine engine
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3232054 |
Liquid fuel combustion apparatus, for jet-propulsion engines, gas turbines, or other prime movers
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3214908 |
Combined fuel governor and electric generator drive for a gas turbine
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