CN105386875A - Turbine piston hybrid power system - Google Patents
Turbine piston hybrid power system Download PDFInfo
- Publication number
- CN105386875A CN105386875A CN201510957414.8A CN201510957414A CN105386875A CN 105386875 A CN105386875 A CN 105386875A CN 201510957414 A CN201510957414 A CN 201510957414A CN 105386875 A CN105386875 A CN 105386875A
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- China
- Prior art keywords
- firing chamber
- gas
- air outlet
- suction port
- casing
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
- F02C3/30—Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas- turbine plants for special use
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E20/00—Combustion technologies with mitigation potential
- Y02E20/16—Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]
Abstract
The invention provides a turbine piston hybrid power system which comprises an engine, a steam turbine engine and an engine fuel providing device, wherein the engine is provided with an engine gas inlet and an engine gas outlet. The steam turbine engine comprises a gas compressor, a combustion chamber, a turbine motor, a power turbine and a cartridge receiver. According to the turbine piston hybrid power system provided by the invention, high-pressure air from the gas compressor and high-temperature high-pressure fuel gas from the engine are introduced into the combustion chamber for being mixed and combusted, thereby strengthening a combustion process, improving combustion quality and also improving integral thermal cycle efficiency of the engine. Based on a gas exhaustion process of the combustion chamber, the power turbine is expanded to work, and therefore, the temperature of gas exhausted out of the combustion chamber in the process of expanding to work is greatly reduced relative to the temperature of the gas exhausted out of the engine, so that infrared stealth characteristics can be obviously improved.
Description
Technical field
The present invention relates to aviation, navigation, land vehicle equipment technical field, particularly relate to a kind of Turbine piston hybrid power system.
Background technique
Energy-conservation and high power to weight ratio is the important evaluation index of advanced power systems, and for this reason, the combined cycle engine of high power and low oil consumption has become the development trend of following power system.
Turbine piston combined cycle engine a kind ofly takes into account the low and combined moving Force system of good economy performance, combustion turbine power density advantages of higher of conventional pistonic engine fuel consumption, it is the innovative power form that can realize high power density, the low oil consumption of partial power state, critical loops pattern is wherein the combined cycle (bavin-combustion combined cycle) of diesel engine and gas turbine, in this circulation mode, high supercharging pressure level mass flow air after gas compressor compression is shunted, enter gas turbine and diesel engine respectively, gas turbine and diesel engine parallel operation simultaneously.In the prior art (as shown in Figure 4), the combustion gas of discharging after the cylinders consume high-pressure air of diesel engine (i.e. motor 1) directly enters together with the gas of discharging in the turbo machine 23 of gas turbine and with the firing chamber 22 of gas turbine and drives power turbine 24 to do work.
But the combustion gas of discharging after the cylinders consume high-pressure air of diesel engine is high pressure conditions, temperature is higher and be rich in oxygen, can directly introduce in the firing chamber of gas turbine by utilization of again burning.
Summary of the invention
In view of Problems existing in background technique, one object of the present invention is to provide a kind of Turbine piston hybrid power system, its gas compressor can be compressed after high-pressure air and diesel engine high pressure, high temperature, the oxygen rich fuel gas these two kinds that discharge are non-all presses heterogeneous air-flow to introduce in the firing chamber of gas turbine to burn, enhance combustion performance, improve gas turbine heating power cycle efficiency.
Another order of the present invention is to provide a kind of Turbine piston hybrid power system, and it can avoid the high pressure of diesel engine, high temperature, oxygen rich fuel gas directly to discharge, and improves vehicle infrared stealth characteristic.
To achieve these goals, the invention provides a kind of Turbine piston hybrid power system, it comprises: motor, gas turbine and motor fuel generator.
Motor has: engine intake mouth; And motor air outlet.
Gas turbine comprises: gas compressor, firing chamber, turbo machine, power turbine and casing.Gas compressor has: gas compressor suction port, for introducing outside air; And gas compressor air outlet.Firing chamber has: firing chamber suction port; And air outlet, firing chamber, be arranged on the afterbody of firing chamber.Turbo machine has: turbo machine suction port, is communicated in air outlet, firing chamber; And turbo machine air outlet.Power turbine has: power turbine suction port, is communicated in turbo machine air outlet; And power turbine air outlet.Casing parcel firing chamber.
Motor fuel generator is communicated in motor, provides power fuel to motor.
Wherein, casing is passed from the gas compressor pressurized gas that air outlet is discharged, enter in firing chamber via firing chamber suction port, casing is passed from the motor high-temperature high-pressure fuel gas that air outlet is discharged, enter in firing chamber via firing chamber suction port, thus enter into pressurized gas and the high-temperature high-pressure fuel gas mixed combustion in a combustion chamber of firing chamber, the waste gas forming High Temperature High Pressure in firing chamber after mixed combustion passes casing via air outlet, firing chamber and enters turbo machine via turbo machine suction port, turbine drives gas compressor and make gas compressor compress the air be incorporated into via gas compressor suction port in gas compressor, air after compression becomes pressurized gas and discharges via gas compressor air outlet, the pressurized gas shunting of discharging and make a part of pressurized gas through casing and enter firing chamber via firing chamber suction port and another part pressurized gas enter motor via engine intake mouth, power fuel is in motor combustion, form high-temperature high-pressure fuel gas and discharge via motor air outlet, the high-temperature high-pressure fuel gas of discharging passes casing and enters in firing chamber via firing chamber suction port, periodic duty and so forth.
Beneficial effect of the present invention is as follows:
In Turbine piston hybrid power system according to the present invention, by the high-temperature high-pressure fuel gas mixed combustion from motor that gas compressor air outlet and casing are incorporated into the high-pressure air from gas compressor in firing chamber and are incorporated into by motor air outlet and casing in firing chamber, enhance combustion process, improve combustion quality.Meanwhile, based on being communicated with of firing chamber and motor, the complementary energy in motor can be made full use of, thus improve the mean temperature of the combustion gas of discharging via air outlet, firing chamber, and improve overall engine efficiency of thermal cycle.In addition, in Turbine piston hybrid power system of the present invention, motor is without the need to directly to outer exhaust, but first the high-temperature high-pressure fuel gas that motor is discharged is incorporated in firing chamber, then be outwards vented by firing chamber, exhaust process based on firing chamber need be expanded by power turbine and do manual work, therefore in expansion workmanship process the gas that firing chamber is discharged temperature opposite engine in the gas temperature of discharging can greatly reduce, thus can obviously promote infrared stealth characteristic.
Accompanying drawing explanation
Fig. 1 is the system connection diagram (arrow only represents gas flow, does not represent concrete pipeline) of the embodiment according to Turbine piston hybrid power system of the present invention, and wherein casing only has a first bleed hole and a second bleed hole;
Fig. 2 is the system connection diagram (arrow only represents gas flow, does not represent concrete pipeline) of another embodiment according to Turbine piston hybrid power system of the present invention, and wherein casing has multiple first bleed hole and multiple second bleed hole;
Fig. 3 is the system connection diagram (arrow only represents gas flow, does not represent concrete pipeline) of another embodiment according to Turbine piston hybrid power system of the present invention;
Fig. 4 is the system connection diagram of Turbine piston hybrid power system of the prior art.
Wherein, description of reference numerals is as follows:
1 motor 231 turbo machine suction port
11 engine intake mouth 232 turbo machine air outlets
12 motors air outlet 24 power turbine
2 gas turbine 241 power turbine suction ports
21 gas compressor 242 power turbine air outlets
211 gas compressors suction port 25 casing
212 gas compressors bleed hole, air outlet 251 first
22 bleed hole, firing chambers 252 second
221 firing chambers suction port 253 conduit box
222 air outlet, firing chamber 254 pipelines portal
23 turbo machine 3 motor fuel generators
Embodiment
Describe in detail with reference to the accompanying drawings according to Turbine piston hybrid power system of the present invention.
Referring to figs. 1 through Fig. 3, Turbine piston hybrid power system according to the present invention comprises: motor 1, gas turbine 2 and motor fuel generator 3.
Motor 1 has: engine intake mouth 11; And motor air outlet 12.
Gas turbine 2 comprises: gas compressor 21, firing chamber 22, turbo machine 23, power turbine 24 and casing 25.Gas compressor 21 has: gas compressor suction port 211, for introducing outside air; And gas compressor air outlet 212.Firing chamber 22 has: firing chamber suction port 221; And air outlet 222, firing chamber, be arranged on the afterbody of firing chamber 22.Turbo machine 23 has: turbo machine suction port 231, is communicated in air outlet, firing chamber 222; And turbo machine air outlet 232.Power turbine 24 has: power turbine suction port 241, is communicated in turbo machine air outlet 232; And power turbine air outlet 242.Casing 25 wraps up firing chamber 22.
Motor fuel generator 3 is communicated in motor 1, provides power fuel to motor 1.
Wherein, casing 25 is passed from the gas compressor pressurized gas that air outlet 212 is discharged, enter in firing chamber 22 via firing chamber suction port 221, casing 25 is passed from the motor high-temperature high-pressure fuel gas that air outlet 12 is discharged, enter in firing chamber 22 via firing chamber suction port 221, thus enter into the pressurized gas of firing chamber 22 and high-temperature high-pressure fuel gas in firing chamber 22 mixed combustion, the waste gas forming High Temperature High Pressure in firing chamber 22 after mixed combustion passes casing 25 via air outlet, firing chamber 222 and enters turbo machine 23 via turbo machine suction port 231, turbo machine 23 drives gas compressor 21 and gas compressor 21 is compressed to be incorporated into via gas compressor suction port 211 air in gas compressor 21, air after compression becomes pressurized gas and discharges via gas compressor air outlet 212, the pressurized gas shunting of discharging and make a part of pressurized gas through casing 25 and enter firing chamber 22 via firing chamber suction port 221 and another part pressurized gas enter motor 1 via engine intake mouth 11, power fuel is in motor 1 combustion, form high-temperature high-pressure fuel gas and discharge via motor air outlet 12, the high-temperature high-pressure fuel gas of discharging passes casing 25 and enters in firing chamber 22 via firing chamber suction port 221, periodic duty and so forth.
In Turbine piston hybrid power system according to the present invention, by the high-temperature high-pressure fuel gas mixed combustion from motor 1 that gas compressor air outlet 212 and casing 25 are incorporated into the high-pressure air from gas compressor 21 in firing chamber 22 and are incorporated into by motor air outlet 12 and casing 25 in firing chamber 22, enhance combustion process, improve combustion quality.Meanwhile, based on being communicated with of firing chamber 22 and motor 1, the complementary energy in motor 1 can be made full use of, thus improve the mean temperature of the combustion gas of discharging via air outlet, firing chamber 222, and improve the overall efficiency of thermal cycle of motor 1.In addition, in Turbine piston hybrid power system of the present invention, motor 1 is without the need to directly to outer exhaust, but first the high-temperature high-pressure fuel gas that motor 1 is discharged is incorporated in firing chamber 22, then be outwards vented by firing chamber 22, exhaust process based on firing chamber 22 need be expanded by power turbine 24 and do manual work, therefore in expansion workmanship process the gas that firing chamber 22 is discharged temperature opposite engine 1 in the gas temperature of discharging can greatly reduce, thus can obviously promote infrared stealth characteristic.According to Turbine piston hybrid power system of the present invention, in one embodiment, see figures.1.and.2, casing 25 has: the first bleed hole 251, is directly communicated with gas compressor air outlet 212; And the second bleed hole 252, be directly communicated with motor air outlet 12.The outer wall that firing chamber suction port 221 is arranged on firing chamber 22 is communicated in the first bleed hole 251 of casing 25 and the second bleed hole 252 of casing 25 simultaneously.The pressurized gas of discharging from gas compressor air outlet 212 enter firing chamber suction port 221 via the first bleed hole 251 of casing 25, firing chamber 22 is entered into again via firing chamber suction port 221, the high-temperature high-pressure fuel gas of discharging from motor air outlet 12 enters firing chamber suction port 221 via the second bleed hole 252 of casing 25, firing chamber 22 is entered into again via firing chamber suction port 221, thus enter into the pressurized gas of firing chamber 22 and high-temperature high-pressure fuel gas in firing chamber 22 mixed combustion, the waste gas forming High Temperature High Pressure in firing chamber 22 after mixed combustion passes casing 25 via air outlet, firing chamber 222 and enters turbo machine 23 via turbo machine suction port 231, turbo machine 23 drives gas compressor 21 and gas compressor 21 is compressed to be incorporated into via gas compressor suction port 211 air in gas compressor 21, air after compression becomes pressurized gas and discharges via gas compressor air outlet 212, the pressurized gas shunting of discharging and make that a part of pressurized gas enter firing chamber 22 via the first air entraining jet and firing chamber suction port 221 and another part pressurized gas enter motor 1 via engine intake mouth 11, motor 1 uses fuel in motor 1 combustion, form high-temperature high-pressure fuel gas and discharge via motor air outlet 12, the high-temperature high-pressure fuel gas of discharging enters in firing chamber 22 via the second air entraining jet and firing chamber suction port 221, periodic duty and so forth.Here remark additionally, in this embodiment, first the pressurized gas from gas compressor 21 enter in the inner chamber of casing 25 via the first bleed hole 251 of casing 25, are then flowed freely in firing chamber 22 by firing chamber suction port 221.In like manner, first the high-temperature high-pressure fuel gas from motor 1 enters in the inner chamber of casing 25 via the second bleed hole 252 of casing 25, then flows freely in firing chamber 22 via firing chamber suction port 221.
In one embodiment, see figures.1.and.2, the first bleed hole 251 of casing 25 is one or more.
In one embodiment, see figures.1.and.2, the second bleed hole 252 of casing 25 is one or more.
In one embodiment, the first bleed hole 251 of casing 25 and the second bleed hole 252 of casing 25 can be same.In this case, described same also can be one or more.When described same be only one time, can be described as single port bleed, single port bleed equally can realize gas compressor 21 to exit being vented with motor 1 and be incorporated in firing chamber 22.Further, the first bleed hole 251 (or second bleed hole 252) of casing 25 directly can be communicated with motor air outlet 12 with gas compressor air outlet 212 via three-way pipe.
In one embodiment, with reference to Fig. 3, the firing chamber suction port 221 of firing chamber 22 is arranged on the head of firing chamber 22.Casing 25 has: hand-hole 253, is arranged on the head of casing 25, passes casing 25 and is communicated with firing chamber suction port 221 for being communicated with gas compressor air outlet 212, to feed gas directly in firing chamber 22 with the pipeline of motor air outlet 12; And portal 254, be arranged on the afterbody of casing 25 and be communicated in air outlet, firing chamber 222, the waste gas of the High Temperature High Pressure in firing chamber 22 via air outlet, firing chamber 222, portal 254 and turbo machine suction port 231 enter in turbo machine 23.What here remark additionally is, in this embodiment, gas compressor air outlet 212 is all directly communicated with firing chamber suction port 221 with motor air outlet 12, thus make the high-temperature high-pressure fuel gas in the high-pressure air in gas compressor 21 and motor 1 directly not enter in firing chamber 22 by the inner chamber of casing 25, casing 25 is same with this structural design of firing chamber 22 can be realized the exhaust of the venting of gas compressor 21 and motor 1 to be incorporated in firing chamber 22 simultaneously, and simple and reliable for structure.
In one embodiment, with reference to Fig. 3, firing chamber suction port 221 is one, and firing chamber suction port 221 directly can be communicated with motor air outlet 12 with gas compressor air outlet 212 via three-way pipe.
In one embodiment, motor 1 can be diesel engine.
In one embodiment, firing chamber 22 can be connular combustor or annular combustion chamber, but not only for so, also according to concrete actual demand, firing chamber 22 can be designed to other shape.
Claims (10)
1. a Turbine piston hybrid power system, comprising:
Motor (1), has:
Engine intake mouth (11); And
Motor is with air outlet (12);
Gas turbine (2), comprising:
Gas compressor (21), has:
Gas compressor with suction port (211), for introducing outside air; And
Gas compressor is with air outlet (212);
Firing chamber (22), has:
Firing chamber is with suction port (221); And
Firing chamber, with air outlet (222), is arranged on the afterbody of firing chamber (22);
Turbo machine (23), has:
Turbo machine, with suction port (231), is communicated in air outlet, firing chamber (222); And
Turbo machine is with air outlet (232);
Power turbine (24), has:
Power turbine, with suction port (241), is communicated in turbo machine air outlet (232); And
Power turbine is with air outlet (242); And
Casing (25), parcel firing chamber (22);
Motor fuel generator (3), is communicated in motor (1), provides power fuel to motor (1);
It is characterized in that,
The pressurized gas of discharging from gas compressor air outlet (212) pass casing (25), enter in firing chamber (22) via firing chamber suction port (221), the high-temperature high-pressure fuel gas of discharging from motor air outlet (12) passes casing (25), enter in firing chamber (22) via firing chamber suction port (221), thus enter into the pressurized gas of firing chamber (22) and high-temperature high-pressure fuel gas in firing chamber (22) mixed combustion, the waste gas that forms High Temperature High Pressure in firing chamber (22) after mixed combustion enters turbo machine (23) through casing (25) via turbo machine suction port (231) via air outlet, firing chamber (222), turbo machine (23) drives gas compressor (21) and makes gas compressor (21) compress the air be incorporated into via gas compressor suction port (211) in gas compressor (21), air after compression becomes pressurized gas and discharges via gas compressor air outlet (212), the pressurized gas shunting of discharging and make a part of pressurized gas through casing (25) and enter firing chamber (22) via firing chamber suction port (221) and another part pressurized gas enter motor (1) via engine intake mouth (11), power fuel is in motor (1) combustion, form high-temperature high-pressure fuel gas and discharge with air outlet (12) via motor, the high-temperature high-pressure fuel gas of discharging passes casing (25) and enters in firing chamber (22) via firing chamber suction port (221), periodic duty and so forth.
2. Turbine piston hybrid power system according to claim 1, is characterized in that,
Casing (25) has:
First bleed hole (251), is directly communicated with gas compressor air outlet (212); And
Second bleed hole (252), is directly communicated with motor air outlet (12);
The outer wall that firing chamber suction port (221) is arranged on firing chamber (22) is communicated in the first bleed hole (251) of casing (25) and the second bleed hole (252) of casing (25) simultaneously;
The pressurized gas of discharging from gas compressor air outlet (212) enter firing chamber suction port (221) via the first bleed hole (251) of casing (25), firing chamber (22) is entered into again via firing chamber suction port (221), the high-temperature high-pressure fuel gas of discharging from motor air outlet (12) enters firing chamber suction port (221) via the second bleed hole (252) of casing (25), firing chamber (22) is entered into again via firing chamber suction port (221), thus enter into the pressurized gas of firing chamber (22) and high-temperature high-pressure fuel gas in firing chamber (22) mixed combustion, the waste gas that forms High Temperature High Pressure in firing chamber (22) after mixed combustion enters turbo machine (23) through casing (25) via turbo machine suction port (231) via air outlet, firing chamber (222), turbo machine (23) drives gas compressor (21) and makes gas compressor (21) compress the air be incorporated into via gas compressor suction port (211) in gas compressor (21), air after compression becomes pressurized gas and discharges via gas compressor air outlet (212), the pressurized gas shunting of discharging and make that a part of pressurized gas enter firing chamber (22) via the first air entraining jet and firing chamber suction port (221) and another part pressurized gas enter motor (1) via engine intake mouth (11), motor (1) uses fuel in motor (1) combustion, form high-temperature high-pressure fuel gas and discharge with air outlet (12) via motor, the high-temperature high-pressure fuel gas of discharging enters in firing chamber (22) via the second air entraining jet and firing chamber suction port (221), periodic duty and so forth.
3. Turbine piston hybrid power system according to claim 2, is characterized in that, the first bleed hole (251) of casing (25) is for one or more.
4. Turbine piston hybrid power system according to claim 2, is characterized in that, the second bleed hole (252) of casing (25) is for one or more.
5. the Turbine piston hybrid power system according to any one of claim 2-4, it is characterized in that, the first bleed hole (251) of casing (25) and the second bleed hole (252) of casing (25) are for same.
6. Turbine piston hybrid power system according to claim 5, it is characterized in that, the first bleed hole (251) of casing (25) is directly communicated with motor air outlet (12) with gas compressor air outlet (212) via three-way pipe.
7. Turbine piston hybrid power system according to claim 1, is characterized in that,
The firing chamber suction port (221) of firing chamber (22) is arranged on the head of firing chamber (22);
Casing (25) has:
Hand-hole (253), be arranged on the head of casing (25), pass casing (25) with the pipeline of motor air outlet (12) and be communicated with firing chamber suction port (221) for being communicated with gas compressor air outlet (212), to feed gas directly in firing chamber (22);
Portal (254), be arranged on the afterbody of casing (25) and be communicated in air outlet, firing chamber (222), the waste gas of the High Temperature High Pressure in firing chamber (22) via air outlet, firing chamber (222), to portal (254) and turbo machine suction port (231) enters in turbo machine (23).
8. Turbine piston hybrid power system according to claim 7, it is characterized in that, firing chamber suction port (221) is one, and firing chamber suction port (221) is directly communicated with motor air outlet (12) with gas compressor air outlet (212) via three-way pipe.
9. Turbine piston hybrid power system according to claim 1, is characterized in that, motor (1) is diesel engine.
10. Turbine piston hybrid power system according to claim 1, is characterized in that, firing chamber (22) are connular combustor or annular combustion chamber.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510957414.8A CN105386875B (en) | 2015-12-18 | 2015-12-18 | turbine piston hybrid power system |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510957414.8A CN105386875B (en) | 2015-12-18 | 2015-12-18 | turbine piston hybrid power system |
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| CN105386875A true CN105386875A (en) | 2016-03-09 |
| CN105386875B CN105386875B (en) | 2017-03-29 |
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| CN201510957414.8A Active CN105386875B (en) | 2015-12-18 | 2015-12-18 | turbine piston hybrid power system |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105650678A (en) * | 2016-01-11 | 2016-06-08 | 清华大学 | Combustion chamber air inlet structure of turbine piston hybrid power system |
| CN105698218A (en) * | 2016-01-11 | 2016-06-22 | 清华大学 | Combustion chamber gas introducing mechanism of turbine piston hybrid power system |
| CN107299868A (en) * | 2017-06-26 | 2017-10-27 | 李宏江 | The method that motor exhaust circulation oxygenation burning eliminates pollutant emission |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3131573B1 (en) * | 2022-01-06 | 2024-03-29 | Safran Helicopter Engines | Hybrid propulsion system for aircraft |
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| US4815294A (en) * | 1987-08-14 | 1989-03-28 | David Constant V | Gas turbine with external free-piston combustor |
| CN1831312A (en) * | 2004-08-19 | 2006-09-13 | 余正 | Combined electromechanical engine |
| CN101117915A (en) * | 2007-08-28 | 2008-02-06 | 余正 | Subsequent technology of combined dynamoelectric engine |
| CN103754103A (en) * | 2014-01-22 | 2014-04-30 | 清华大学 | Turbine piston hybrid power system and vehicle |
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2015
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US4815294A (en) * | 1987-08-14 | 1989-03-28 | David Constant V | Gas turbine with external free-piston combustor |
| CN1831312A (en) * | 2004-08-19 | 2006-09-13 | 余正 | Combined electromechanical engine |
| CN101117915A (en) * | 2007-08-28 | 2008-02-06 | 余正 | Subsequent technology of combined dynamoelectric engine |
| CN103754103A (en) * | 2014-01-22 | 2014-04-30 | 清华大学 | Turbine piston hybrid power system and vehicle |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105650678A (en) * | 2016-01-11 | 2016-06-08 | 清华大学 | Combustion chamber air inlet structure of turbine piston hybrid power system |
| CN105698218A (en) * | 2016-01-11 | 2016-06-22 | 清华大学 | Combustion chamber gas introducing mechanism of turbine piston hybrid power system |
| CN105698218B (en) * | 2016-01-11 | 2018-07-24 | 清华大学 | The combustion chamber bleed mechanism of Turbine piston hybrid power system |
| CN107299868A (en) * | 2017-06-26 | 2017-10-27 | 李宏江 | The method that motor exhaust circulation oxygenation burning eliminates pollutant emission |
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|---|---|
| CN105386875B (en) | 2017-03-29 |
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