CN102865157A - Main component device of micro-emission high-energy-saving multiplied tremendous-power pulse knocking engine - Google Patents
Main component device of micro-emission high-energy-saving multiplied tremendous-power pulse knocking engine Download PDFInfo
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- CN102865157A CN102865157A CN 201110186126 CN201110186126A CN102865157A CN 102865157 A CN102865157 A CN 102865157A CN 201110186126 CN201110186126 CN 201110186126 CN 201110186126 A CN201110186126 A CN 201110186126A CN 102865157 A CN102865157 A CN 102865157A
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Abstract
The invention discloses a main component device of a micro-emission high-energy-saving multiplied tremendous-power pulse knocking engine. The main component device comprises a spark plug, a knocking tube, an oil inlet, a gas inlet, a control valve, a spray pipe and a water cooler, wherein a taper pre-detonation head pulse explosion ignition knocking pipe, a vertical hook type gas inlet channel, a secondary high-temperature air stable-combustion outer cover outer spray pipe and a secondary air stable-combustion outer cover gas inlet channel are arranged on a taper inlet pulse knocking combustion chamber, and a high-pressure fuel inlet pipe front-end fuel supply longevity pulse control shutter valve, a medium-pressure gas transmission pipe front-end gas transmission supply longevity pulse control shutter valve, a high-energy fuel high-pressure pump, a high-pressure fuel inlet pipe front-end fuel supply longevity pulse control shutter valve are arranged outside the taper inlet pulse knocking combustion chamber. a medium-pressure high-temperature gas storage tank is arranged outside the taper inlet pulse knocking combustion chamber, and a high-speed gas inlet preheating pipe, a high-speed fuel inlet preheating pipe and a high-pressure high-temperature mixing pipe high-speed ejector are arranged on the vertical hook type gas inlet channel. The main component device is used on a power machine.
Description
Affiliated technical field
The present invention relates to the super pulse-knocking engine of a kind of high steady combustion low noise, particularly relate to the huge power pulse detonation engine of a kind of little discharging many times of merits of high energy-conservation product main part device.
Background technique
At present, the technology of existing pulse-knocking engine, mostly in experimental stage, the commodity that can form industrialization are seldom found.
Summary of the invention
At present, adopt the high energy-conservation huge power pulse detonation engine of external Effuser device---the technology of the huge power pulse detonation engine of the high many times of merits of energy-conservation product of little discharging main part device, put down in writing lessly in the document, up to the present, the commodity mass production promotion that still finds no this type of technology on the market is used.
The objective of the invention is: the huge power pulse detonation engine of a kind of little discharging many times of merits of high energy-conservation product main part device is provided.
To achieve the above object, technological scheme of the present invention is: at tapering entrance pulse detonation combustor the pre-initiator head pulse explosion of tapering ignition and detonation pipe, lifting-hook shape intake duct, secondary are set and surely fire outer cover outer nozzle, Secondary Air for high warm air and surely fire the outer cover intake duct, set high pressurized fuel supplying tube front end fuel at tapering entrance pulse detonation combustor peripheral hardware and supply with long-lived pulse and control the fast family of power and influence, the gas transmission of middle pressure pneumatic tube front end and supply with long-lived pulse and control the fast family of power and influence, high-energy fuel high-pressure service pump, fuel under high pressure supplying tube front end fuel and supply with long-lived pulse and control the fast family of power and influence.Middle super pressure-high temperature gas holder is set outside tapering entrance pulse detonation combustor, at lifting-hook shape intake duct high speed charge heating pipe is set, fuel is inputted at a high speed economizer bank, high pressure-temperature blending pipe high velocity jet device.The back segment of the pre-initiator head pulse explosion of tapering ignition and detonation pipe is connected with the front portion of tapering entrance pulse detonation combustor, the rear portion of lifting-hook shape intake duct is connected with the front portion of tapering entrance pulse detonation combustor, at tapering entrance pulse detonation combustor, the external secondary that arranges of jet pipe surely fires the outer cover outer nozzle for high warm air, in the front portion that secondary surely fires the outer cover outer nozzle for high warm air Secondary Air is set and surely fires the outer cover intake duct, supply high warm air surely to fire at secondary and settle tapering entrance pulse detonation combustor in the body of outer cover outer nozzle, jet pipe, fuel under high pressure supplying tube front end fuel is supplied with long-lived pulse and is controlled the fast family of power and influence's a end and be connected the other end with an end of high pressure special fuel input pulse control system and be connected with an end of high pressure special fuel supplying tube, the gas transmission of middle pressure pneumatic tube front end is supplied with long-lived pulse and is controlled the fast family of power and influence's a end and be connected the other end with an end of middle super pressure-high temperature pneumatic tube and be connected with an end of middle super pressure-high temperature gas holder, one end of high-energy fuel high-pressure service pump is connected the other end and is connected with an end of fuel under high pressure input pulse control system with an end of high energy fuel tank, fuel under high pressure supplying tube front end fuel is supplied with long-lived pulse and controlled the fast family of power and influence's a end and be connected the other end with an end of fuel under high pressure input pulse control system and be connected with an end of fuel under high pressure supplying tube.One end of middle super pressure-high temperature gas holder is connected the other end and the gas transmission of middle pressure pneumatic tube front end and supplies with long-lived pulse and control the fast family of power and influence's a end and be connected with an end of intermediate pressure compressor, in tapering entrance pulse detonation combustor, settle high speed charge heating pipe, in high speed charge heating pipe, settle fuel to input at a high speed economizer bank (36), in the back segment of high speed charge heating pipe, settle high pressure-temperature blending pipe high velocity jet device, settle high pressure-temperature blending pipe high velocity jet device in the front portion of tapering entrance pulse detonation combustor.
The invention has the beneficial effects as follows: 1, simple in structure, 2, stable performance, 3, practicability is stronger, 4, the low emission environmental protection, 5, fractional energy savings is higher, 6, cost is lower, 7, produce the many times of huge power of merit, 8, be convenient to quick penetration and promotion and use.
Description of drawings
The present invention is further illustrated below in conjunction with drawings and Examples.
Fig. 1 is the brief introduction schematic representation of the huge power pulse detonation engine of the little discharging of the present invention many times of merits of high energy-conservation product main part device embodiment's working principle.
Fig. 2 is the brief introduction schematic representation of working principle of the huge power pulse detonation engine of the little discharging of the present invention many times of merits of high energy-conservation product main part device embodiment's starting drive.
Fig. 3 is that the huge power pulse detonation engine of the little discharging of the present invention many times of merits of high energy-conservation product main part device embodiment's power produces and the brief introduction schematic representation of the working principle of extraction apparatus.
Among the figure: 1, high-energy igniter, 2, the pre-initiator head pulse explosion of tapering ignition and detonation pipe, 3, the special fuel bottle detonates, 4, the high pressure fuel input pulse control system of detonating, 5, the high pressure fuel inlet pipe that detonates, 6, the fuel high pressure sparger detonates, 7, the Special Oxidants bottle detonates, 8, the high pressure oxygenant input pulse control system of detonating, 9, the high pressure oxygenant supplying tube that detonates, 10, the oxygenant that detonates high-pressure injector, 11, tapering entrance pulse detonation combustor, 12, high pressure special fuel tank, 13, high pressure special fuel input pulse control system, 14, high pressure special fuel supplying tube, 15, the special fuel high-pressure injector, 16, fuel under high pressure supplying tube front end fuel is supplied with long-lived pulse and is controlled the fast family of power and influence, 17, lifting-hook shape intake duct, 18, jet pipe, 19, secondary surely fires the outer cover outer nozzle for high warm air, 20, Secondary Air surely fires the outer cover intake duct, 21, high-pressure turbine, 22, the taking of power device, 23, middle pressure turbine, 24, intermediate pressure compressor, 25, middle super pressure-high temperature pneumatic tube, 26, middle super pressure-high temperature gas holder, 27, the gas transmission of middle pressure pneumatic tube front end is supplied with long-lived pulse and is controlled the fast family of power and influence, 28, high energy fuel tank, 29, the high-energy fuel high-pressure service pump, 30, fuel under high pressure input pulse control system, 31, the fuel under high pressure supplying tube, 32, high-pressure fuel injectors, 33, fuel under high pressure supplying tube front end fuel is supplied with long-lived pulse and is controlled the fast family of power and influence, 34, middle pressure pneumatic tube, 35, high speed charge heating pipe, 36, fuel is inputted at a high speed economizer bank, 37, high pressure-temperature blending pipe high velocity jet device.
Embodiment
In Fig. 1, in the front portion of tapering entrance pulse detonation combustor (11) the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2) is set, in the front portion of the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2) high-energy igniter (1) is set, in the front portion of tapering entrance pulse detonation combustor (11) lifting-hook shape intake duct (17) is set, at tapering entrance pulse detonation combustor (11), jet pipe (18) external arranges secondary and surely fires outer cover outer nozzle (19) for high warm air, in the front portion that secondary surely fires outer cover outer nozzle (19) for high warm air Secondary Air is set and surely fires outer cover intake duct (20).Front portion at the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2) arranges the fuel high pressure sparger (6) that detonates, the oxygenant that detonates high-pressure injector (10), at the external setting of the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2) the special fuel bottle (3) that detonates, the high pressure fuel input pulse control system (4) of detonating, the high pressure fuel inlet pipe (5) that detonates is at the external setting of the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2) the Special Oxidants bottle (7) that detonates, the high pressure oxygenant input pulse control system (8) of detonating, the high pressure oxygenant supplying tube (9) that detonates.Tapering entrance pulse detonation combustor (11) external high pressure special fuel tank (12), high pressure special fuel input pulse control system (13), fuel under high pressure supplying tube front end fuel being set supplies with long-lived pulse and controls the fast family of power and influence (16), high pressure special fuel supplying tube (14), special fuel high-pressure injector (15).One end of the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2) is connected the other end and is connected with the front portion of tapering entrance pulse detonation combustor (11) with an end of high-energy igniter (1).The rear portion of lifting-hook shape intake duct (17) is connected with the front portion of tapering entrance pulse detonation combustor (11).Supplying high warm air surely to fire at secondary settles tapering entrance pulse detonation combustor (11), jet pipe (18), settles Secondary Air surely to fire outer cover intake duct (20) in the front portion that secondary surely fires outer cover outer nozzle (19) for high warm air in the body of outer cover outer nozzle (19).Front portion at the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2) arranges the fuel high pressure sparger (6) that detonates, the oxygenant that detonates high-pressure injector (10), at the external setting of the fuel high pressure sparger (6) that the detonates special fuel bottle (3) that detonates, the high pressure fuel input pulse control system (4) of detonating, the high pressure fuel inlet pipe (5) that detonates, a detonate end of fuel input pulse control system (4) of high pressure is connected the other end and the high pressure fuel inlet pipe (5) that detonates and is connected with the special fuel bottle (3) that detonates, an end of the fuel high pressure sparger (6) that detonates and the high pressure fuel inlet pipe (5) that detonates is connected the other end and is connected with the front portion of the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2).At the external setting of the oxygenant high-pressure injector (10) that the detonates Special Oxidants bottle (7) that detonates, the high pressure oxygenant input pulse control system (8) of detonating, the high pressure oxygenant supplying tube (9) that detonates, a detonate end of oxygenant input pulse control system (8) of high pressure is connected the other end and the high pressure oxygenant supplying tube (9) that detonates and is connected with the Special Oxidants bottle (7) that detonates, an end of the oxygenant that detonates high-pressure injector (10) and the high pressure oxygenant supplying tube (9) that detonates is connected the other end and is connected with the front portion of the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2).One end of high pressure special fuel input pulse control system (13) is connected the other end and fuel under high pressure supplying tube front end fuel and supplies with long-lived pulse and control the fast family of power and influence (16) and be connected with high pressure special fuel tank (12), one end of high pressure special fuel supplying tube (14) is connected with special fuel high-pressure injector (15), and the other end of special fuel high-pressure injector (15) is connected with tapering entrance pulse detonation combustor (11).At the rear portion of tapering entrance pulse detonation combustor (11) jet pipe (18) is set.
In Fig. 2, Fig. 2 is identical with Fig. 1 major part.In the front portion of tapering entrance pulse detonation combustor (11) the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2) is set, in the front portion of the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2) high-energy igniter (1) is set, in the front portion of tapering entrance pulse detonation combustor (11) lifting-hook shape intake duct (17) is set, at the rear portion of tapering entrance pulse detonation combustor (11) jet pipe (18) is set, tapering entrance pulse detonation combustor (11) external secondary is set and surely fires outer cover outer nozzle (19) for high warm air, in the front portion that secondary surely fires outer cover outer nozzle (19) for high warm air Secondary Air is set and surely fires outer cover intake duct (20).At the rear portion of lifting-hook shape intake duct (17) high speed charge heating pipe (35) is set, material is set in high speed charge heating pipe (35) inputs at a high speed economizer bank (36), at the carry-out part of lifting-hook shape intake duct (17) high pressure-temperature blending pipe high velocity jet device (37) is set.Front portion at the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2) arranges the fuel high pressure sparger (6) that detonates, the oxygenant that detonates high-pressure injector (10), at the external setting of the fuel high pressure sparger (6) that the detonates special fuel bottle (3) that detonates, the high pressure fuel input pulse control system (4) of detonating, the high pressure fuel inlet pipe (5) that detonates, a detonate end of fuel input pulse control system (4) of high pressure is connected the other end and the high pressure fuel inlet pipe (5) that detonates and is connected with the special fuel bottle (3) that detonates, an end of the fuel high pressure sparger (6) that detonates and the high pressure fuel inlet pipe (5) that detonates is connected the other end and is connected with the front portion of the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2).At the external setting of the oxygenant high-pressure injector (10) that the detonates Special Oxidants bottle (7) that detonates, the high pressure oxygenant input pulse control system (8) of detonating, the high pressure oxygenant supplying tube (9) that detonates, a detonate end of oxygenant input pulse control system (8) of high pressure is connected the other end and the high pressure oxygenant supplying tube (9) that detonates and is connected with the Special Oxidants bottle (7) that detonates, an end of the oxygenant that detonates high-pressure injector (10) and the high pressure oxygenant supplying tube (9) that detonates is connected the other end and is connected with the front portion of the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2).High speed charge heating pipe (35) is set in tapering entrance pulse detonation combustor (11), high pressure-temperature blending pipe high velocity jet device (37), set high pressurized fuel sparger (32) at tapering entrance pulse detonation combustor (11) peripheral hardware, at the external high energy fuel tank (28) that arranges of high-pressure fuel injectors (32), high-energy fuel high-pressure service pump (29), fuel under high pressure input pulse control system (30), fuel under high pressure supplying tube front end fuel is supplied with long-lived pulse and is controlled the fast family of power and influence (33), fuel under high pressure supplying tube (31).One end of high-energy fuel high-pressure service pump (29) is connected the other end and is connected with fuel under high pressure input pulse control system (30) with high energy fuel tank (28), fuel under high pressure supplying tube front end fuel is supplied with long-lived pulse and is controlled the fast family of power and influence's (33) a end and be connected the other end with fuel under high pressure input pulse control system (30) and be connected with fuel under high pressure supplying tube (31), and an end of high-pressure fuel injectors (32) is connected the other end and is connected with tapering entrance pulse detonation combustor (11) with fuel under high pressure supplying tube (31).
In Fig. 3, Fig. 3 and Fig. 2, Fig. 1 major part are identical.In the front portion of tapering entrance pulse detonation combustor (11) the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2) is set, in the front portion of the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2) high-energy igniter (1) is set, at the rear portion of tapering entrance pulse detonation combustor (11) jet pipe (18) is set, supply high warm air surely to fire in the body of outer cover outer nozzle (19) at secondary tapering entrance pulse detonation combustor (11) is set, jet pipe (18) arranges Secondary Air in the front portion that secondary surely fires outer cover outer nozzle (19) for high warm air and surely fires outer cover intake duct (20).Front portion at the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2) arranges the fuel high pressure sparger (6) that detonates, the oxygenant that detonates high-pressure injector (10), at the external setting of the fuel high pressure sparger (6) that the detonates special fuel bottle (3) that detonates, the high pressure fuel input pulse control system (4) of detonating, the high pressure fuel inlet pipe (5) that detonates, a detonate end of fuel input pulse control system (4) of high pressure is connected the other end and the high pressure fuel inlet pipe (5) that detonates and is connected with the special fuel bottle (3) that detonates, an end of the fuel high pressure sparger (6) that detonates and the high pressure fuel inlet pipe (5) that detonates is connected the other end and is connected with the front portion of the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2).At the external setting of the oxygenant high-pressure injector (10) that the detonates Special Oxidants bottle (7) that detonates, the high pressure oxygenant input pulse control system (8) of detonating, the high pressure oxygenant supplying tube (9) that detonates, a detonate end of oxygenant input pulse control system (8) of high pressure is connected the other end and the high pressure oxygenant supplying tube (9) that detonates and is connected with the Special Oxidants bottle (7) that detonates, an end of the oxygenant that detonates high-pressure injector (10) and the high pressure oxygenant supplying tube (9) that detonates is connected the other end and is connected with the front portion of the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2).At tapering entrance pulse detonation combustor (11) high-pressure fuel injectors (32) is set, high-pressure fuel injectors (32) external high energy fuel tank (28), high-energy fuel high-pressure service pump (29), fuel under high pressure input pulse control system (30), fuel under high pressure supplying tube front end fuel is set and supplies with long-lived pulse and control the fast family of power and influence (33), fuel under high pressure supplying tube (31).One end of high-energy fuel high-pressure service pump (29) is connected the other end and is connected with fuel under high pressure input pulse control system (30) with high energy fuel tank (28), fuel under high pressure supplying tube front end fuel is supplied with long-lived pulse and is controlled the fast family of power and influence's (33) a end and be connected the other end with fuel under high pressure input pulse control system (30) and be connected with fuel under high pressure supplying tube (31), and an end of high-pressure fuel injectors (32) is connected the other end and is connected with tapering entrance pulse detonation combustor (11) with fuel under high pressure supplying tube (31).The afterbody that surely fires outer cover outer nozzle (19) for high warm air at secondary arranges high-pressure turbine (21), at high-pressure turbine (21) taking of power device (22) is set, at high-pressure turbine (21) middle pressure pneumatic tube (34) is set, at middle pressure pneumatic tube (34) middle pressure turbine (23) is set, at middle pressure turbine (23) intermediate pressure compressor (24) is set, at intermediate pressure compressor (24) middle super pressure-high temperature gas holder (26) is set, at middle super pressure-high temperature gas holder (26) gas transmission of middle pressure pneumatic tube front end being set supplies with long-lived pulse and controls the fast family of power and influence (27), supply with long-lived pulse in the gas transmission of middle pressure pneumatic tube front end and control the fast family of power and influence (27) middle super pressure-high temperature pneumatic tube (25) is set, in the front portion of lifting-hook shape intake duct (17) middle super pressure-high temperature pneumatic tube (25) is set.One end of middle super pressure-high temperature pneumatic tube (25) is connected the other end and the gas transmission of middle pressure pneumatic tube front end to be supplied with long-lived pulse and controls the fast family of power and influence (27) and be connected with lifting-hook shape intake duct (17), and an end of middle super pressure-high temperature gas holder (26) and the gas transmission of middle pressure pneumatic tube front end are supplied with long-lived pulse and controlled the fast family of power and influence (27) and be connected the other end and be connected with intermediate pressure compressor (24).The coaxial middle pressure turbine (23) that arranges at intermediate pressure compressor (24), one end of middle pressure pneumatic tube (34) is connected the other end and is connected with high-pressure turbine (21) with middle pressure turbine (23), one end of taking of power device (22) is connected with high-pressure turbine (21), and an end of high-pressure turbine (21) is connected with the afterbody that secondary surely fires outer cover outer nozzle (19) for high warm air.One end of high-pressure fuel injectors (32) is connected with lifting-hook shape intake duct (17), and an end of lifting-hook shape intake duct (17) is connected with tapering entrance pulse detonation combustor (11).
Claims (4)
1. the huge power pulse detonation engine of little discharging many times of merits of high energy-conservation product main part device, comprise spark plug, detonation tube, oil-feed, air inlet, control valve, jet pipe, water-cooled, it is characterized in that: at tapering entrance pulse detonation combustor (11) the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2) is set, lifting-hook shape intake duct (17), secondary surely fires outer cover outer nozzle (19) for high warm air, Secondary Air surely fires outer cover intake duct (20), sets high pressurized fuel supplying tube front end fuel at tapering entrance pulse detonation combustor (11) peripheral hardware and supplies with long-lived pulse and control the fast family of power and influence (16), the gas transmission of middle pressure pneumatic tube front end is supplied with long-lived pulse and is controlled the fast family of power and influence (27), high-energy fuel high-pressure service pump (29), fuel under high pressure supplying tube front end fuel is supplied with long-lived pulse and is controlled the fast family of power and influence (33).
2. the huge power pulse detonation engine of little discharging according to claim 1 many times of merits of high energy-conservation product main part device, it is characterized in that: middle super pressure-high temperature gas holder (26) is set outside tapering entrance pulse detonation combustor (11), at lifting-hook shape intake duct (17) high speed charge heating pipe (35) is set, fuel is inputted at a high speed economizer bank (36), high pressure-temperature blending pipe high velocity jet device (37).
3. the huge power pulse detonation engine of little discharging according to claim 1 many times of merits of high energy-conservation product main part device, it is characterized in that: the back segment of the pre-initiator head pulse explosion of tapering ignition and detonation pipe (2) is connected with the front portion of tapering entrance pulse detonation combustor (11), the rear portion of lifting-hook shape intake duct (17) is connected with the front portion of tapering entrance pulse detonation combustor (11), at tapering entrance pulse detonation combustor (11), the external secondary that arranges of jet pipe (18) surely fires outer cover outer nozzle (19) for high warm air, in the front portion that secondary surely fires outer cover outer nozzle (19) for high warm air Secondary Air is set and surely fires outer cover intake duct (20), supply high warm air surely to fire at secondary and settle tapering entrance pulse detonation combustor (11) in the body of outer cover outer nozzle (19), jet pipe (18), fuel under high pressure supplying tube front end fuel is supplied with long-lived pulse and is controlled the fast family of power and influence's (16) a end and be connected the other end with an end of high pressure special fuel input pulse control system (13) and be connected with an end of high pressure special fuel supplying tube (14), the gas transmission of middle pressure pneumatic tube front end is supplied with long-lived pulse and is controlled the fast family of power and influence's (27) a end and be connected the other end with an end of middle super pressure-high temperature pneumatic tube (25) and be connected with an end of middle super pressure-high temperature gas holder (26), one end of high-energy fuel high-pressure service pump (29) is connected the other end and is connected with an end of fuel under high pressure input pulse control system (30) with an end of high energy fuel tank (28), fuel under high pressure supplying tube front end fuel is supplied with long-lived pulse and controlled the fast family of power and influence's (33) a end and be connected the other end with an end of fuel under high pressure input pulse control system (30) and be connected with an end of fuel under high pressure supplying tube (31).
4. the huge power pulse detonation engine of little discharging according to claim 1 and 2 many times of merits of high energy-conservation product main part device, it is characterized in that: an end of middle super pressure-high temperature gas holder (26) is connected the other end and the gas transmission of middle pressure pneumatic tube front end and supplies with long-lived pulse and control the fast family of power and influence's (27) a end and be connected with an end of intermediate pressure compressor (24), in tapering entrance pulse detonation combustor (11), settle high speed charge heating pipe (35), in high speed charge heating pipe (35), settle fuel to input at a high speed economizer bank (36), in the back segment of high speed charge heating pipe (35), settle high pressure-temperature blending pipe high velocity jet device (37), settle high pressure-temperature blending pipe high velocity jet device (37) in the front portion of tapering entrance pulse detonation combustor (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201110186126 CN102865157A (en) | 2011-07-05 | 2011-07-05 | Main component device of micro-emission high-energy-saving multiplied tremendous-power pulse knocking engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201110186126 CN102865157A (en) | 2011-07-05 | 2011-07-05 | Main component device of micro-emission high-energy-saving multiplied tremendous-power pulse knocking engine |
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|---|---|
| CN102865157A true CN102865157A (en) | 2013-01-09 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201110186126 Pending CN102865157A (en) | 2011-07-05 | 2011-07-05 | Main component device of micro-emission high-energy-saving multiplied tremendous-power pulse knocking engine |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106939868A (en) * | 2017-03-21 | 2017-07-11 | 中国人民解放军国防科学技术大学 | Heater and its igniter are studied in detonating combustion |
| CN114542326A (en) * | 2022-02-28 | 2022-05-27 | 湖北华海节龙燃油设备科技有限公司 | Compressed air deflagration engine and power generation method |
-
2011
- 2011-07-05 CN CN 201110186126 patent/CN102865157A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106939868A (en) * | 2017-03-21 | 2017-07-11 | 中国人民解放军国防科学技术大学 | Heater and its igniter are studied in detonating combustion |
| CN106939868B (en) * | 2017-03-21 | 2019-01-08 | 中国人民解放军国防科学技术大学 | A kind of heater and its igniter for detonating combustion research |
| CN114542326A (en) * | 2022-02-28 | 2022-05-27 | 湖北华海节龙燃油设备科技有限公司 | Compressed air deflagration engine and power generation method |
| CN114542326B (en) * | 2022-02-28 | 2024-05-28 | 湖北华海节龙燃油设备科技有限公司 | Compressed air deflagration engine and power generation method |
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Application publication date: 20130109 |