CN201730699U - Gas piston pulse engine - Google Patents
Gas piston pulse engine Download PDFInfo
- Publication number
- CN201730699U CN201730699U CN2010201470707U CN201020147070U CN201730699U CN 201730699 U CN201730699 U CN 201730699U CN 2010201470707 U CN2010201470707 U CN 2010201470707U CN 201020147070 U CN201020147070 U CN 201020147070U CN 201730699 U CN201730699 U CN 201730699U
- Authority
- CN
- China
- Prior art keywords
- jet pipe
- pressure liquid
- gas
- pressure
- gas piston
- Prior art date
- 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.)
- Expired - Lifetime
Links
Images
Landscapes
- Nozzles (AREA)
Abstract
The utility model discloses a gas piston pulse engine, which comprises a jet pipe (1). At least one combustion chamber (2) is disposed inside the jet pipe (1), at least one high-pressure fluid nozzle (3) jetting toward the jet direction of the jet pipe (1) is disposed inside the jet pipe (1) and/or on the lateral wall of the jet pipe (1), and/or at least one high-pressure fluid nozzle (3) jetting toward a direction opposite to the jet direction of the jet pipe (1) is disposed inside the jet pipe (1) and/or on the lateral wall of the jet pipe (1), and the high-pressure fluid nozzles (3) are communicated with a high-pressure fluid source (4) via high-pressure fluid jet control valves (5). The gas piston pulse engine is few in moving parts and high in compression ratio, solves the lubrication difficulty of a great number of moving parts in case of the great number of moving parts existing in an existing internal combustion engine, and solves the problem that a single ramjet cannot start from stationary state or work at low speed working conditions.
Description
Technical field
The utility model relates to engine art, especially a kind of gas piston pulse engine.
Technical background
In the internal combustion (IC) Engine Design, can reach subsequently the needed High Temperature High Pressure of combustion explosion,, all must compress air inlet simultaneously also in order to improve the thermal efficiency of internal-combustion engine in order to make fuel and AIR MIXTURES.Adopted three kinds of technological schemes to realize calming the anger in the existing internal combustion (IC) Engine Design, promptly piston gas-pressing, turbine are calmed the anger or punching press is calmed the anger.But, no matter be to utilize piston (such as internal-combustion piston engine) or compressor turbine mechanical parts such as (such as gas turbine, jet engines etc.) that air is compressed, still utilize the high-speed motion of internal-combustion engine that air is carried out punching press and come air is compressed (such as pressed engine), all exist fairly obvious drawback; The above two are complex structure, manufacture cost height not only, and need be lubricated the parts of calming the anger such as piston, turbine, thereby bring a series of problem, and the energy that itself is consumed of calming the anger comes from the mechanical work of the preciousness of not at all easy acquisition, reduced the hot merit conversion efficiency of motor; Though the latter has solved the problem of the above two existence to a certain extent, can't work under the low speed operating mode, and can not start under quiescent conditions; In addition, be that turbine is calmed the anger or punching press is calmed the anger all exist the problem of the effect deficiency of calming the anger under the low speed operating mode.These have all greatly restricted the raising of existing internal combustion engine thermal efficiency, the reduction of manufacture cost and the expansion in the field of use.
Therefore, be badly in need of a kind of internal combustion type or mixed combustion engine of invention with novel air pressing mode.
The model utility content
In order to address the above problem, the technological scheme that the utility model proposes is as follows:
A kind of gas piston pulse engine comprises jet pipe, and at least one firing chamber is set in described jet pipe; It serves as to spray the high-pressure liquid nozzle that points to that at least one injection direction with described jet pipe is set in described jet pipe and/or on the sidewall of described jet pipe, and/or the high-pressure liquid nozzle that at least one opposite direction with the injection direction of described jet pipe is the injection sensing is set in described jet pipe and/or on the sidewall of described jet pipe, described high-pressure liquid nozzle is communicated with high-pressure fluid source through the high-pressure liquid injection control valve;
Wherein, injection direction with described jet pipe serves as to spray the described high-pressure liquid nozzle that points to be made as forward high-pressure liquid nozzle, and the described high-pressure liquid injection control valve between described forward high-pressure liquid nozzle and the described high-pressure fluid source is made as forward high-pressure liquid injection control valve; Opposite direction with the injection direction of described jet pipe serves as to spray the described high-pressure liquid nozzle that points to be made as reverse high-pressure liquid nozzle, and the described high-pressure liquid injection control valve between described reverse high-pressure liquid nozzle and the described high-pressure fluid source is made as reverse high-pressure liquid injection control valve.
Described high-pressure liquid nozzle is arranged on the inside cavity of the described jet pipe outside the described firing chamber and/or is arranged on the sidewall of the described jet pipe outside the described firing chamber.
Described jet pipe is made as the local boosting jet pipe with expansion regions.
Described high-pressure liquid nozzle is made as venturi and sprays tube nozzle, and the pressurized gas inlet that described venturi sprays tube nozzle is communicated with described high-pressure fluid source.
The jet pipe inlet end of described jet pipe is established the port sealing shell, and described port sealing shell seals described jet pipe inlet end, establishes at least one gas-entered passageway on described port sealing shell, and described gas-entered passageway is communicated with the body source of calming the anger.
The jet pipe inlet end of described jet pipe is established the port sealing shell, and described port sealing shell seals described jet pipe inlet end, establishes at least one gas-entered passageway on described port sealing shell, the fluid spout connection of described gas-entered passageway and venturi injection pipe; Or the jet pipe inlet end of described jet pipe is established the port sealing shell, described port sealing shell seals described jet pipe inlet end, on described port sealing shell, establish at least one gas-entered passageway, the fluid spout connection of described gas-entered passageway and venturi injection pipe, pressurized gas inlet and low-pressure gas ingress at described venturi injection pipe are established high pressure control valve and low-pressure control valve respectively, control described high pressure control valve and described low-pressure control valve and make described venturi injection pipe intermittent type jet fluid.
In the structure that is provided with described high pressure control valve and described low-pressure control valve, described gas-entered passageway is divided into two groups at least, control described high pressure control valve and the described low-pressure control valve described gas-entered passageway in making not on the same group and replace air inlet, increasing the working pressure in the described jet pipe, or realize the work of described jet pipe continous-stable in the working pressure in increasing described jet pipe.
Also be provided with the normal opened type gas-entered passageway on the described port sealing shell, described gas-entered passageway surrounds a week around described normal opened type gas-entered passageway, and described normal opened type gas-entered passageway is by continuous intake method work.
Along described injection pipe axially on establish at least two described firing chambers, fuel sprayed and/or igniting during difference when each described firing chamber was differed from.
In described jet pipe, establish a described firing chamber and at least two described reverse high-pressure liquid nozzles, to improve the pressure of the gas in the described firing chamber.
Compressor turbine is established in the place ahead in described firing chamber, establishes power turbine at the rear of described firing chamber, described compressor turbine and the coaxial setting of described power turbine;
Perhaps establish power turbine at the rear of described firing chamber, described power turbine is connected with pto.
Described gas piston pulse engine is located at formation gas piston pulse rotary engine on the rotor.
Establish the high-pressure liquid export mouth at described rear combustion chamber, described high-pressure liquid export mouth is communicated with described high-pressure liquid nozzle or is communicated with described high-pressure liquid nozzle behind supercharging device;
Or described rear combustion chamber establishes the high-pressure liquid export mouth, and described high-pressure liquid export mouth is penetrated the high-pressure liquid inlet of annotating pump with threeway and is communicated with, and the fluid output that the notes pump is penetrated in described threeway is communicated with described high-pressure liquid nozzle;
Or establish the high-pressure liquid export mouth at described rear combustion chamber, and described high-pressure liquid export mouth is penetrated the high-pressure liquid inlet of annotating pump through described supercharging device and described threeway and is communicated with, and the fluid output that the notes pump is penetrated in described threeway is communicated with described high-pressure liquid nozzle.
On the sidewall of described jet pipe, establish the cooling spray orifice, described cooling spray orifice is communicated with the inner chamber and the described high-pressure fluid source of described jet pipe, realize high-pressure liquid in the described high-pressure fluid source through described cooling spray orifice to the cooling of the sidewall of described jet pipe and realize to the isolation between the sidewall of flame in the described firing chamber and described jet pipe.
As everyone knows, the fluid of high-speed motion can form an interface between the gas in himself and its place ahead, and this interface gas towards the place ahead under the promotion of this high-velocity fluid advances fast, just just as the gas piston of a high-speed motion, thereby can play the effect of compression to the gas in its place ahead; Especially when the gas in the fluid of high-speed motion and the place ahead thereof is positioned at same pipe interior, the calm the anger effect of phenomenon of this kind high-velocity fluid interface will be more obvious.Gas piston be the formed inertia of fluid motion at all.Rocket for example if explain the motion of rocket from the rocket spout, is because the reaction force that the high velocity jet fluid obtains promotes rocket motion.But, if analyze the motion of rocket from the peripheral interface of the gas of rocket ejection, the gas piston that to can be understood as a stroke be endless.
Therefore be not difficult to imagine, when towards a gassy, such as air or fuel-air mixture, jet pipe in when spraying high-velocity fluid, this high-velocity fluid must produce compression to air in the jet pipe or fuel-air mixture, its pressure, temperature are sharply raise, thereby reach combustion in IC engine blast conditions needed.
In the utility model, both the high-pressure liquid nozzle that sprays to the firing chamber can be set simultaneously in the jet pipe of both sides, firing chamber, thereby form the interface of two mutual convergences of high speed in the both sides of firing chamber, piston just as two mutual convergences of high speed, thereby air between it, that be positioned at the firing chamber or fuel-air mixture are sharply compressed, make it reach the combustion in IC engine needed High Temperature High Pressure of exploding; Also the high-pressure liquid nozzle that sprays to the firing chamber can only be set in the jet pipe of firing chamber one side, while is provided with baffle plate or sealing or regulates the firing chamber and the shape of the jet pipe of front and back, firing chamber in the jet pipe of the opposite side of firing chamber, utilize high-pressure liquid to form, high speed is towards the interface of the direction propelling of firing chamber, just as the piston of a high speed towards the direction propelling of firing chamber, sharply compress the air or the fuel-air mixture in the place ahead, can make air or fuel-air mixture in the firing chamber reach the needed High Temperature High Pressure of combustion in IC engine explosion time too.
In the utility model, the setting of reverse high-pressure liquid nozzle is equivalent to form the fluid wall one after the firing chamber, make the high-speed air flow of coming be decelerated supercharging from intake duct, just sharply compressed, the pressure of air improves rapidly, thereby increased the effect of calming the anger, made that air or the fuel-air mixture in the motor reaches the required temperature and pressure of burning.When taking fire in the firing chamber, reverse high-pressure liquid nozzle is closed, thereby the disappearance of fluid wall does not influence the orientation movement of combustion gas.
In the utility model, when two facing to the high-pressure liquid nozzle of firing chamber during simultaneously towards the direction high velocity jet of firing chamber, be equivalent to form the gas piston of two mutual convergence motions at the two ends of firing chamber, thereby make and to enter the firing chamber and near air is sharply compressed, pressure improves rapidly, thereby play the effect of calming the anger, thereby can replace machineries such as piston or the compressor turbine parts of calming the anger calms the anger, make the simple in structure of motor, can also replace or alleviate pressed engine to a certain extent to rely on high speed stamping to come air is compressed, even thereby make pressed engine under lower speed or even static state, also can be so that air in the firing chamber and fuel mixture reach the required temperature, pressure of burning, and make that pressed engine can proper functioning.And when taking fire in the firing chamber, reverse high-pressure liquid nozzle is closed, thereby the disappearance of the gas piston after the firing chamber does not influence the orientation movement of combustion gas.
In the utility model, when multistage nozzle is set, before and after nozzles at different levels, can form the pressure reduction of one-level level, these pressure reduction mutual superposition, thereby make along the pressure of nozzle spray direction can be step by step raising, higher pressure after will obtaining to superpose in the therefore previous stage makes wherein compressed air or fuel-air mixture can obtain higher pressure and temperature.Especially when a plurality of nozzles when same direction is sprayed, this effect will be more obvious---promptly before and after each nozzle, form level, the equidirectional pressure reduction of one-level, thereby make along the pressure of nozzle spray direction can be step by step increase, will obtain higher pressure in the therefore previous stage.
High-pressure fluid source in the utility model can be to compress good air or other pressurized gass in advance, also can be highly pressurised liquid, liquid gas, can be the fuel and the fuel mixture of high pressure equally, can also be by the exhaust of the high compressed steam that waste heat produced of motor self or motor self or work done working medium etc.
Hydrodynamic pressure in the so-called high-pressure fluid source of the utility model, greater than satisfying gas piston pulse engine proper functioning of the present utility model, the needed pressure of blast that takes fire of the fuel mixture in the firing chamber.
The utility model is so-called when poor, is meant that life period at interval between two actions.
Gas piston pulse engine of the present utility model both can be by the ejection acting working medium at a high speed backward of the jet exhaust on the jet pipe, utilizes the recoil force of its acquisition to promote gas piston pulse engine and advance; Also can be connected to come outputting power with pto, thereby also gas piston pulse engine can be arranged on external outputting rotary power on the solid of rotation by power turbine is set.
Gas piston pulse engine in the utility model can be the adjustment that air inflow realizes power by the control fuel injection amount.Gas piston pulse engine in the utility model also can a plurality of work in combination, formation is similar to the mode of operation of multicylinder engine, can be by controlling each gas piston pulse engine work in this combined engine or intermittently realizing load responding to reach combined engine under the prerequisite that guarantees the high efficiency low emission.
The so-called body source of calming the anger of the utility model includes but not limited to the air outlet in general expression punching press chamber, the air outlet in jet-type punching press chamber, the air outlet in venturi type jet-type punching press chamber, fluid spout or other body source of calming the anger of venturi nozzle.It is the patent of invention of CN201010124191.4 and CN201010124192.9 that so-called jet-type punching press chamber sees also the application number of submitting to State Patent Office in person.So-called venturi type jet-type punching press chamber is meant that the jet nozzle in jet-type punching press chamber is a venturi nozzle.
The utility model is so-called to serve as to spray to point to the injection direction of jet pipe and/or the opposite direction of injection direction, both comprised that with the injection direction of jet pipe and/or the opposite direction of injection direction be accurate fully situation of spraying sensing, though comprise that also the drift angle that exists to a certain extent serves as to spray situation about pointing to the injection direction of jet pipe and/or the opposite direction of injection direction still substantially.
The so-called local boosting jet pipe with expansion regions of the utility model is compressed the structural design that heats supercharging thereby punching press chamber that includes but not limited to pressed engine etc. can make high velocity air slow down therein.
The utility model the place ahead, so-called firing chamber and rear combustion chamber, be meant the flow direction of the High Temperature High Pressure working medium discharge motor that generates according to the blast of the fuel combustion in firing chamber back, flow to an opposite side with this working medium in the both sides of firing chamber and be the place ahead, flow to an identical side with this working medium and be the rear.
The so-called gas piston pulse engine of the utility model can be that internal-combustion engine also can be a mixed combustion engine; The product that so-called mixed combustion engine is meant burning is as acting working medium the time, and the heated fluid in the motor is also as acting working medium; So-called heated fluid is meant the fluid in the engine-cooling system and makes the fluid of the exhaust cooling of motor (mixed combustion engine is the patent of invention of CN201010118601.4 with reference to me to the patent No. of State Patent Office's submission further please).
The so-called gas piston pulse engine of the utility model can be used for aeroengine, jet engine, gas turbine, pressed engine etc.
The so-called gas piston pulse engine of the utility model can be arranged on the rotor, and the axle that forms with rotor is the rotor motor of pto.
The beneficial effects of the utility model are as follows:
1, the utility model movement parts is few, the compression ratio height, both solved the lubricated difficult problem of a large amount of movement parts under the situation that there are a large amount of movement parts in existing internal-combustion engine, also solved the problem that simple pressed engine self can't start, can't work under the state of rest under the low speed operating mode.
2, the utility model anti-knock performance is good, and the feature of environmental protection is good, thermal efficiency height.
Description of drawings
Shown in Figure 1 is the utility model embodiment 1 structural representation;
Shown in Figure 2 is the utility model embodiment 2 structural representation;
Shown in Figure 3 is the utility model embodiment 3 structural representation;
Shown in Figure 4 is the utility model embodiment 4 structural representation;
Shown in Figure 5 is the utility model embodiment 5 structural representation;
Shown in Figure 6 is the utility model embodiment 6 structural representation;
Fig. 7, Fig. 8 and shown in Figure 9 be the utility model embodiment 7 structural representation;
Shown in Figure 10 is the utility model embodiment 8 structural representation;
Shown in Figure 11 is the utility model embodiment 9 structural representation;
Shown in Figure 12 is the utility model embodiment 10 structural representation;
Shown in Figure 13 is the utility model embodiment 11 structural representation;
Shown in Figure 14 is the utility model embodiment 12 structural representation;
Shown in Figure 15 is the utility model embodiment 13 structural representation;
Shown in Figure 16 is the utility model embodiment 14 structural representation.
Embodiment
Gas piston pulse engine as shown in Figure 1 comprises jet pipe 1, and firing chamber 2 is set in jet pipe 1; It serves as to spray the high-pressure liquid nozzle 3 that points to that at least one injection direction with jet pipe 1 is set in jet pipe 1, with at least one opposite direction with the injection direction of jet pipe 1 serves as to spray the high-pressure liquid nozzle 3 that points to, and high-pressure liquid nozzle 3 is communicated with high-pressure fluid source 4 through high-pressure liquid injection control valve 5; Wherein, serve as to spray the high-pressure liquid nozzle 3 that points to be made as forward high-pressure liquid nozzle 301 with the injection direction of jet pipe 1, forward the high-pressure liquid injection control valve 5 between high-pressure liquid nozzle 301 and the high-pressure fluid source 4 is made as forward high-pressure liquid injection control valve 501; Opposite direction with the injection direction of jet pipe 1 serves as to spray the high-pressure liquid nozzle 3 that points to be made as reverse high-pressure liquid nozzle 302, and the high-pressure liquid injection control valve 5 between reverse high-pressure liquid nozzle 302 and the high-pressure fluid source 4 is made as reverse high-pressure liquid injection control valve 502.Specifically, the injection direction that is provided with in jet pipe 1 with jet pipe 1 serves as to spray the forward high-pressure liquid nozzle 301 that points to, forward high-pressure liquid nozzle 301 is arranged on the inside cavity of the jet pipe 1 of 2 both sides, firing chamber, and forward high-pressure liquid nozzle 301 is communicated with high-pressure fluid source 4 through high-pressure liquid injection control valve 501 forward; The opposite direction that while is provided with in jet pipe 1 with the injection direction of jet pipe 1 serves as to spray the reverse high-pressure liquid nozzle 302 that points to, and reverse high-pressure liquid nozzle 302 is arranged on the inside cavity of the jet pipe 1 of 2 both sides, firing chamber.Reverse high-pressure liquid nozzle 302 is communicated with high-pressure fluid source 4 through reverse high-pressure liquid injection control valve 502.
Gas piston pulse engine as shown in Figure 2, itself and embodiment's 1 difference is: the opposite direction that only is provided with in jet pipe 1 with the injection direction of jet pipe 1 serves as to spray the reverse high-pressure liquid nozzle 302 that points to, and reverse high-pressure liquid nozzle 302 is communicated with high-pressure fluid source 4 through reverse high-pressure liquid injection control valve 502.High-pressure liquid nozzle 3 is arranged on the sidewall of the jet pipe 1 of 2 both sides, firing chamber.Jet pipe 1 is made as the local boosting jet pipe 100 with expansion regions.
Gas piston pulse engine as shown in Figure 3, itself and embodiment's 1 difference is: forward high-pressure liquid nozzle 301 and reverse high-pressure liquid nozzle 302 all are made as venturi and spray tube nozzle 30, and the pressurized gas inlet that venturi sprays tube nozzle 30 is communicated with high-pressure fluid source 4.
Gas piston pulse engine as shown in Figure 4, itself and embodiment's 1 difference is: the jet pipe inlet end 101 of jet pipe 1 is established port sealing shell 102, port sealing shell 102 is with 101 sealings of jet pipe inlet end, establish at least one gas-entered passageway 103 on port sealing shell 102, gas-entered passageway 103 is communicated with the body source 6 of calming the anger.
Gas piston pulse engine as shown in Figure 5, itself and embodiment's 1 difference is: the jet pipe inlet end 101 of jet pipe 1 is established port sealing shell 102, port sealing shell 102 is with 101 sealings of jet pipe inlet end, on port sealing shell 102, establish at least one gas-entered passageway 103, the fluid spout connection of gas-entered passageway 103 and venturi injection pipe 50, pressurized gas inlet and low-pressure gas ingress at venturi injection pipe 50 are established high pressure control valve 503 and low-pressure control valve 504 respectively, and control high pressure control valve 503 and low-pressure control valve 504 make venturi injection pipe 50 intermittent type jet fluids.
Gas piston pulse engine as shown in Figure 6, itself and embodiment's 5 difference is: gas-entered passageway 103 has two, be divided into and be two groups of A, B, gas-entered passageway 103 alternately air inlets during control high pressure control valve 503 and low-pressure control valve 504 make not on the same group, increasing the working pressure in the described jet pipe 1, or realize described jet pipe 1 continous-stable work in the working pressure in increasing described jet pipe 1.
As Fig. 7, Fig. 8 and gas piston pulse engine shown in Figure 9, itself and embodiment's 6 difference is: port sealing shell 102 also is provided with normal opened type gas-entered passageway 11, gas-entered passageway 103 surrounds a week around normal opened type gas-entered passageway 11, and normal opened type gas-entered passageway 11 is by continuous intake method work.
Gas piston pulse engine as shown in figure 10, itself and embodiment's 1 difference is: along injection pipe 1 axially on establish three firing chambers 2, fuel sprayed or igniting during difference when each firing chamber 2 was differed from.
Gas piston pulse engine as shown in figure 11, itself and embodiment's 1 difference is: establish a firing chamber 2 and at least two reverse high-pressure liquid nozzles 302 in jet pipe 1, to improve the pressure of the gas in the firing chamber 2.
Embodiment 10
Gas piston pulse engine as shown in figure 12, itself and embodiment's 1 difference is: compressor turbine 7 is established in the place ahead of 2 in the firing chamber, and power turbine 8 is established at 2 rear in the firing chamber, compressor turbine 7 and power turbine 8 coaxial settings.
Gas piston pulse engine as shown in figure 13, itself and embodiment's 1 difference is: power turbine 8 is established at 2 rear in the firing chamber, and power turbine 8 is connected with pto 801.
Gas piston pulse engine as shown in figure 14, itself and embodiment's 1 difference is: gas piston pulse engine is located at constitutes the gas piston pulse rotary engine on the rotor 9.
Embodiment 13
Gas piston pulse engine as shown in figure 15, itself and embodiment's 1 difference is: establish high-pressure liquid export mouth 330 at 2 rears, described firing chamber, described high-pressure liquid export mouth 330 is penetrated the high-pressure liquid inlet 33101 of annotating pump 331 through described supercharging device 332 and described threeway and is communicated with, and described threeway is penetrated the fluid output 33103 of annotating pump 331 and is communicated with described high-pressure liquid nozzle 3.
Embodiment 14
Gas piston pulse engine as shown in figure 16, itself and embodiment's 1 difference is: establish cooling spray orifice 12 on the sidewall of jet pipe 1, cooling spray orifice 12 is communicated with the inner chamber and the high-pressure fluid source 4 of jet pipes 1, realizes that high-pressure liquid in the high-pressure fluid source 4 is through the sidewall cooling of 12 pairs of jet pipes 1 of supercooling spray orifice and realize the isolation between the sidewall of flame in the firing chamber 2 and jet pipe 1.
Claims (14)
1. a gas piston pulse engine comprises jet pipe (1), it is characterized in that: at least one firing chamber (2) is set in described jet pipe (1); It serves as to spray the high-pressure liquid nozzle (3) that points to that at least one injection direction with described jet pipe (1) is set in described jet pipe (1) and/or on the sidewall of described jet pipe (1), and/or the high-pressure liquid nozzle (3) that at least one opposite direction with the injection direction of described jet pipe (1) is the injection sensing is set in described jet pipe (1) and/or on the sidewall of described jet pipe (1), described high-pressure liquid nozzle (3) is communicated with high-pressure fluid source (4) through high-pressure liquid injection control valve (5);
Wherein, injection direction with described jet pipe (1) serves as to spray the described high-pressure liquid nozzle (3) that points to be made as forward high-pressure liquid nozzle (301), and the described high-pressure liquid injection control valve (5) between described forward high-pressure liquid nozzle (301) and the described high-pressure fluid source (4) is made as forward high-pressure liquid injection control valve (501); Opposite direction with the injection direction of described jet pipe (1) serves as to spray the described high-pressure liquid nozzle (3) that points to be made as reverse high-pressure liquid nozzle (302), and the described high-pressure liquid injection control valve (5) between described reverse high-pressure liquid nozzle (302) and the described high-pressure fluid source (4) is made as reverse high-pressure liquid injection control valve (502).
2. gas piston pulse engine according to claim 1 is characterized in that: described high-pressure liquid nozzle (3) is arranged on the inside cavity of the described jet pipe (1) outside the described firing chamber (2) and/or is arranged on the sidewall of the described jet pipe (1) outside the described firing chamber (2).
3. gas piston pulse engine according to claim 1 is characterized in that: described jet pipe (1) is made as the local boosting jet pipe (100) with expansion regions.
4. gas piston pulse engine according to claim 1, it is characterized in that: described high-pressure liquid nozzle (3) is made as venturi and sprays tube nozzle (30), and the pressurized gas inlet that described venturi sprays tube nozzle (30) is communicated with described high-pressure fluid source (4).
5. gas piston pulse engine according to claim 1, it is characterized in that: the jet pipe inlet end (101) of described jet pipe (1) is established port sealing shell (102), described port sealing shell (102) seals described jet pipe inlet end (101), establish at least one gas-entered passageway (103) on described port sealing shell (102), described gas-entered passageway (103) is communicated with the body source of calming the anger (6).
6. gas piston pulse engine according to claim 1, it is characterized in that: the jet pipe inlet end (101) of described jet pipe (1) is established port sealing shell (102), described port sealing shell (102) seals described jet pipe inlet end (101), on described port sealing shell (102), establish at least one gas-entered passageway (103), the fluid spout connection of described gas-entered passageway (103) and venturi injection pipe (50); Or the jet pipe inlet end (101) of described jet pipe (1) is established port sealing shell (102), described port sealing shell (102) seals described jet pipe inlet end (101), on described port sealing shell (102), establish at least one gas-entered passageway (103), the fluid spout connection of described gas-entered passageway (103) and venturi injection pipe (50) is established high pressure control valve (503) and low-pressure control valve (504) respectively in the pressurized gas inlet and the low-pressure gas ingress of described venturi injection pipe (50).
7. gas piston pulse engine according to claim 6 is characterized in that: in the structure that is provided with described high pressure control valve (503) and described low-pressure control valve (504), described gas-entered passageway (103) is divided into two groups at least.
8. gas piston pulse engine according to claim 7 is characterized in that: also be provided with normal opened type gas-entered passageway (11) on the described port sealing shell (102), described gas-entered passageway (103) surrounds a week around described normal opened type gas-entered passageway (11).
9. gas piston pulse engine according to claim 1 is characterized in that: along described injection pipe (1) axially on establish at least two described firing chambers (2).
10. gas piston pulse engine according to claim 1 is characterized in that: establish a described firing chamber (2) and at least two described reverse high-pressure liquid nozzles (302) in described jet pipe (1).
11. according to one of any described gas piston pulse engine of claim 1 to 10, it is characterized in that: establish compressor turbine (7) in the place ahead of described firing chamber (2), establish power turbine (8) at the rear of described firing chamber (2), described compressor turbine (7) and the coaxial setting of described power turbine (8);
Perhaps establish power turbine (8) at the rear of described firing chamber (2), described power turbine (8) is connected with pto (801).
12., it is characterized in that: described gas piston pulse engine is located at rotor (9) goes up and constitute the gas piston pulse rotary engine according to one of any described gas piston pulse engine of claim 1 to 10.
13. according to one of any described gas piston pulse engine of claim 1 to 10, it is characterized in that: establish high-pressure liquid export mouth (330) at rear, described firing chamber (2), described high-pressure liquid export mouth (330) is communicated with described high-pressure liquid nozzle (3) or is communicated with described high-pressure liquid nozzle (3) behind supercharging device (332);
Or high-pressure liquid export mouth (330) is established at rear, described firing chamber (2), described high-pressure liquid export mouth (330) is penetrated the high-pressure liquid inlet (33101) of annotating pump (331) with threeway and is communicated with, and described threeway is penetrated the fluid output (33103) of annotating pump (331) and is communicated with described high-pressure liquid nozzle (3);
Or establish high-pressure liquid export mouth (330) at rear, described firing chamber (2), described high-pressure liquid export mouth (330) is penetrated the high-pressure liquid inlet (33101) of annotating pump (331) through described supercharging device (332) and described threeway and is communicated with, and described threeway is penetrated the fluid output (33103) of annotating pump (331) and is communicated with described high-pressure liquid nozzle (3).
14. according to one of any described gas piston pulse engine of claim 1 to 10, it is characterized in that: on the sidewall of described jet pipe (1), establish cooling spray orifice (12), described cooling spray orifice (12) is communicated with the inner chamber and the described high-pressure fluid source (4) of described jet pipe (1), realize high-pressure liquid in the described high-pressure fluid source (4) through described cooling spray orifice (12) to the cooling of the sidewall of described jet pipe (1) and realize to the isolation between the sidewall of flame in described firing chamber (2) and described jet pipe (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010201470707U CN201730699U (en) | 2010-03-15 | 2010-04-01 | Gas piston pulse engine |
Applications Claiming Priority (9)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201020130970 | 2010-03-15 | ||
| CN201020130970.0 | 2010-03-15 | ||
| CN201020130971.5 | 2010-03-15 | ||
| CN201020130971 | 2010-03-15 | ||
| CN201010132206.1 | 2010-03-25 | ||
| CN201010132206 | 2010-03-25 | ||
| CN201010133080.X | 2010-03-26 | ||
| CN201010133080 | 2010-03-26 | ||
| CN2010201470707U CN201730699U (en) | 2010-03-15 | 2010-04-01 | Gas piston pulse engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201730699U true CN201730699U (en) | 2011-02-02 |
Family
ID=43521856
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010201470707U Expired - Lifetime CN201730699U (en) | 2010-03-15 | 2010-04-01 | Gas piston pulse engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201730699U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101825041A (en) * | 2010-03-15 | 2010-09-08 | 靳北彪 | Gas piston pulse engine |
| WO2011113306A1 (en) * | 2010-03-15 | 2011-09-22 | Jin Beibiao | Gas piston pulse engine |
| CN108413443A (en) * | 2018-02-26 | 2018-08-17 | 中国科学院力学研究所 | The starting method of active cooling scramjet engine and starting device |
| CN109779786A (en) * | 2019-02-22 | 2019-05-21 | 龙世朗 | Egg type pulsed motor |
-
2010
- 2010-04-01 CN CN2010201470707U patent/CN201730699U/en not_active Expired - Lifetime
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101825041A (en) * | 2010-03-15 | 2010-09-08 | 靳北彪 | Gas piston pulse engine |
| WO2011113306A1 (en) * | 2010-03-15 | 2011-09-22 | Jin Beibiao | Gas piston pulse engine |
| CN101825041B (en) * | 2010-03-15 | 2013-06-05 | 靳北彪 | Gas piston pulse engine |
| CN108413443A (en) * | 2018-02-26 | 2018-08-17 | 中国科学院力学研究所 | The starting method of active cooling scramjet engine and starting device |
| CN108413443B (en) * | 2018-02-26 | 2019-09-17 | 中国科学院力学研究所 | The starting method of active cooling scramjet engine and starting device |
| CN109779786A (en) * | 2019-02-22 | 2019-05-21 | 龙世朗 | Egg type pulsed motor |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN101825041B (en) | Gas piston pulse engine | |
| CN201730699U (en) | Gas piston pulse engine | |
| CN202745952U (en) | Low-entropy mixed-combustion gas liquid injection air-powered engine | |
| CN109322760A (en) | The gas-turbine unit and its fuel combustion method of pulse-combustion mode | |
| CN206205999U (en) | Continuous rotation pinking generator | |
| CN102146858A (en) | Stamping engine for pneumatic turbine | |
| CN102562292A (en) | Gas compressor with three valves | |
| CN102374069A (en) | Hot-stamping engine | |
| CN102619642A (en) | Efficient turbojet engine | |
| CN104234867A (en) | Scramjet engine | |
| CN202001139U (en) | Stamping engine with pneumatic turbine | |
| CN208138060U (en) | Three rows mouthful turbojet | |
| CN102979612A (en) | Fan two-stroke engine | |
| CN205064133U (en) | Air preheater of internal -combustion engine | |
| CN102536442A (en) | High-efficiency thermal power system | |
| CN1973119A (en) | Rotary engine | |
| CN201047326Y (en) | Double flow nipple engines | |
| CN202228175U (en) | Low-temperature air inlet engine | |
| CN202091057U (en) | Turbine jet engine with high efficiency | |
| CN1197159A (en) | Dual rotors reversly-acting rotary I. C. engine | |
| CN202690215U (en) | Efficient thermo-power system | |
| CN201103494Y (en) | Air injection rotor engine | |
| WO2011113306A1 (en) | Gas piston pulse engine | |
| CN104632465A (en) | Stamping impinging stream engine | |
| CN201884128U (en) | Hydrogen-mixed gas fuel power machine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20110202 Effective date of abandoning: 20130605 |
|
| RGAV | Abandon patent right to avoid regrant |