Co-generator utilizing micro gas turbine engine

Claim 2

A turbo heater for providing heated air comprising: a gas turbine engine including: an engine housing; a shaft assembly rotatably supported within said engine housing on a first bearing assembly and a second bearing assembly; a compressor operably disposed on a first end of said shaft assembly for drawing air into said gas turbine engine and generating compressed air; a combustor in fluid communication with said compressor such that said compressed air is directed from said compressor into said combustor; a fuel system for mixing a combustion fuel with said compressed air to form an air-fuel mixture, and for injecting said air-fuel mixture into said combustor such that said air-fuel mixture is ignited and burned in said combustor to generate an exhaust gas; and a turbine operably disposed on a second end of said shaft assembly for concurrent rotation with said compressor, said combustor being in fluid communication with said turbine such that said exhaust gas are expanded in said turbine, thereby drivingly rotating said shaft assembly; a heat exchanger assembly including: a heat exchanger housing; and a fan operably coupled to said shaft assembly for propelling an ambient air into said heat exchanger housing such that said exhaust gas interacts with said ambient air to generate a heated ambient air which is discharged from said heat exchanger housing.

Claim 3

The turbo heater of claim 1 wherein said heat exchanger assembly further comprises a tube bundle disposed in said heat exchanger housing to define a fresh air volume in fluid communication with said fan for propelling said ambient air therethrough, and an exhaust gas volume in fluid communication with said gas turbine engine for passing said exhaust gas therethrough, whereby said tube bundle transfers heat from said exhaust gas to said ambient air for generating said heated ambient air.

Claim 4

The turbo heater of claim 2 wherein said heat exchanger assembly further comprises a liquid coil disposed within said heat exchanger housing to define a liquid volume in fluid communication with a liquid pump for pumping a liquid therethrough and an exhaust gas volume in fluid communication with said gas turbine engine for passing said exhaust gas therethrough, whereby said liquid coil transfers heat from said exhaust gas to said liquid for generating a heated liquid.

Claim 5

The turbo heater of claim 1 wherein said heat exchanger assembly further comprises a liquid coil disposed within said heat exchanger housing to define a liquid volume in fluid communication with a liquid pump for pumping a liquid therethrough and an exhaust gas volume in fluid communication with said gas turbine engine for passing said exhaust gas therethrough, whereby said liquid coil transfers heat from said exhaust gas to said liquid for generating a heated liquid.

Claim 6

The turbo heater of claim 1 wherein said heat exchanger assembly further comprises a catalytic convertor disposed within said heat exchanger housing and in fluid communication with said gas turbine engine for passing said exhaust gas therethrough to generate a catalytically-treated exhaust gas which is exhausted into said heat exchanger housing for mixing with said ambient air.

Claim 7

The turbo heater of claim 1 wherein said combustor is an annular combustor concentrically disposed about said shaft assembly between said compressor and said turbine.

Claim 8

The turbo heater of claim 6 wherein said tube bundle is generally annularly configured such that said gas turbine engine is at least partially disposed within said annular tube bundle.

Claim 9

The turbo heater of claim 1 further comprising a gear reduction assembly having an input shaft operably coupled to said shaft assembly and an output shaft operably coupled to said fan, and a gear set operably coupled between said input shaft and said output shaft to provide a gear ratio therebetween.

Claim 10

The turbo heater of claim 8 wherein said gear reduction assembly further comprises a pinion gear disposed on an end of said shaft assembly and a pair of counter-rotating reduction gear sets operably coupled between said pinion gear and said output shaft.

Claim 11

The turbo heater of claim 9 wherein said first bearing assembly rotatably supports said pinion gear and is elastically supported within said engine housing to provide load sharing between said pair of counter-rotating reduction gear sets.

Claim 12

The turbo heater of claim 8 further comprising an electrical generator operably coupled to said output shaft of said gear reduction assembly.

Claim 13

The turbo heater of claim 11 wherein said electrical generator comprises a first electrical generator for producing electrical power for said turbo heater and a second electrical generator for producing surplus electrical power.

Claim 14

The turbo heater of claim 8 further comprising a starter motor operably coupled to said output shaft of said gear reduction assembly for initiating rotation of said shaft assembly for starting said gas turbine engine.

Claim 15

The turbo heater of claim 13 further comprising a one-way over-running clutch interdisposed between said output shaft and said starter motor.

Claim 16

The turbo heater of claim 13 further comprising a battery electrically connected to said starter motor by a soft start circuit, said soft start circuit including a first circuit having a resistance element interdisposed between said battery and said starter motor for limiting the current drawn from the battery, a second circuit directly connecting said battery to said starter motor, and a controller for selectively switching between said first circuit and said second circuit.

Claim 17

The turbo heater of claim 15 wherein said resistance element is disposed in a housing and wherein said combustion fuel is delivered to said housing for heating said combustion fuel prior to injection into said combustor.

Claim 18

The turbo heater of claim 1 wherein said fuel system modulates a fuel flow rate to maintain a substantially constant pressure in said combustor, thereby controlling the heat generated by said gas turbine engine.

Claim 19

A turbo heater for providing heated air comprising: an engine housing; a turbine nozzle assembly disposed within said engine housing and supporting a nozzle hub; a shaft assembly disposed within said nozzle hub and defining an annulus therebetween; a rear bearing assembly disposed within said annulus and rotatably supporting said shaft assembly in said nozzle hub, the rear bearing assembly including an inner race formed on the shaft assembly, an outer race supported within a bearing holder, a plurality of bearings interdisposed between said inner and outer races for rotatably supporting said shaft assembly about a center of rotation, and a bearing cage interdisposed between said inner and outer races and retaining said plurality of bearings, said bearing cage having a plurality of radial holes formed therethrough for providing fluid communication between said inner race and said outer race; a front bearing assembly disposed within said engine housing and rotatably supporting said shaft assembly; a compressor operably disposed on a first end of said shaft assembly for drawing air into said engine housing and generating compressed air; an annular combustor concentrically disposed about the shaft assembly adjacent said compressor; a fuel delivery system including a fuel feed tube for delivering a fuel to said annulus through a first fuel passageway formed in said nozzle hub and a second fuel passageway formed in said bearing holder, a scavenger blower assembly disposed within said annulus, and a fuel slinger coupled to said shaft assembly for rotation therewith, said nozzle hub having a compressed air passageway formed therethrough, wherein said scavenger blower assembly is operable to direct compressed air from said compressor past said second fuel passageway for mixing said fuel with said compressed air to form an air-fuel mixture, said air-fuel mixture passing through said bearing cage holes for centering said bearing cage about said center of rotation, through said bearing assembly for cooling and lubricating said bearing assembly and into said fuel slinger such that said air-fuel mixture is injected into said annular combustor and combusted to form a combusted gas; a turbine operably disposed on a second end of said shaft assembly for concurrent rotation with said compressor, said combusted gas being expanded in said turbine, thereby drivingly rotating said shaft assembly; a gear reduction assembly including an input shaft operably coupled to said shaft assembly, an output shaft, and a gear set operably coupled between said input shaft and said output shaft; an electrical generator operably coupled to said output shaft of said gear reduction assembly; a starter assembly having a starter motor operably coupled to said output shaft of said gear reduction assembly through a clutch member to initiate rotation of said shaft assembly for starting said gas turbine engine; a heat exchanger assembly including a housing and a heat exchanger element in fluid communication with said gas turbine engine; and a fan operably coupled to said output shaft for propelling an ambient air into said heat exchanger housing such that said exhaust gas interacts with said ambient air to generate a heated ambient air which is discharged from said heat exchanger housing.

Claim 20

A turbo heater for providing heated air comprising: an engine housing; a turbine nozzle assembly disposed within said engine housing and supporting a nozzle hub; a shaft assembly disposed within said nozzle hub and defining an annulus therebetween; a rear bearing assembly disposed within said annulus and rotatably supporting said shaft assembly in said nozzle hub, the rear bearing assembly including an inner race formed on the shaft assembly, an outer race supported within a bearing holder, a plurality of bearings interdisposed between said inner and outer races for rotatably supporting said shaft assembly about a center of rotation, and a bearing cage interdisposed between said inner and outer races and retaining said plurality of bearings, said bearing cage having a plurality of radial holes formed therethrough for providing fluid communication between said inner race and said outer race; a front bearing assembly disposed within said engine housing and rotatably supporting said shaft assembly; a compressor operably disposed on a first end of said shaft assembly for drawing air into said engine housing and generating compressed air; an annular combustor concentrically disposed about the shaft assembly adjacent said compressor; a fuel delivery system including a fuel feed tube for delivering a fuel to said annulus through a first fuel passageway formed in said nozzle hub and a second fuel passageway formed in said bearing holder, a scavenger blower assembly disposed within said annulus, and a fuel slinger coupled to said shaft assembly for rotation therewith, said nozzle hub having a compressed air passageway formed therethrough, wherein said scavenger blower assembly is operable to direct compressed air from said compressor past said second fuel passageway for mixing said fuel with said compressed air to form an air-fuel mixture, said air-fuel mixture passing through said bearing cage holes for centering said bearing cage about said center of rotation, through said bearing assembly for cooling and lubricating said bearing assembly and into said fuel slinger such that said air-fuel mixture is injected into said annular combustor and combusted to form a combusted gas; a turbine operably disposed on a second end of said shaft assembly for concurrent rotation with said compressor, said combusted gas being expanded in said turbine, thereby drivingly rotating said shaft assembly; a gear reduction assembly including an input shaft operably coupled to said shaft assembly, an output shaft, and a gear set operably coupled between said input shaft and said output shaft; an electrical generator operably coupled to said output shaft of said gear reduction assembly; a starter assembly having a starter motor operably coupled to said output shaft of said gear reduction assembly through a clutch member to initiate rotation of said shaft assembly for starting said gas turbine engine; a heat exchanger assembly including a housing and a heat exchanger element in fluid communication with said gas turbine engine; and a fan operably coupled to said output shaft for propelling an ambient air into said heat exchanger housing such that said exhaust gas interacts with said ambient air to generate a heated ambient air which is discharged from said heat exchanger housing.

Claim 21

The turbo heater of claim 18 wherein said heat exchanger assembly further comprises a tube bundle disposed in said heat exchanger housing to define a fresh air volume in fluid communication with said fan for propelling said ambient air therethrough, and an exhaust gas volume in fluid communication with said gas turbine engine for passing said exhaust gas therethrough, whereby said tube bundle transfers heat from said exhaust gas to said ambient air for generating said heated ambient air.

Claim 22

The turbo heater of claim 18 wherein said heat exchanger assembly further comprises a liquid coil disposed within said heat exchanger housing to define a liquid volume in fluid communication with a liquid pump for pumping a liquid therethrough and an exhaust gas volume in fluid communication with said gas turbine engine for passing said exhaust gas therethrough, whereby said liquid coil transfers heat from said exhaust gas to said liquid for generating a heated liquid.

Claim 23

The turbo heater of claim 18 wherein said heat exchanger assembly further comprises a catalytic convertor disposed within said heat exchanger housing and in fluid communication with said gas turbine engine for passing said exhaust gas therethrough to generate a catalytically-treated exhaust gas which is exhausted into said heat exchanger housing for mixing with said ambient air.