CN103644042A - Jet rotor engine - Google Patents
Jet rotor engine Download PDFInfo
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- CN103644042A CN103644042A CN201310726889.7A CN201310726889A CN103644042A CN 103644042 A CN103644042 A CN 103644042A CN 201310726889 A CN201310726889 A CN 201310726889A CN 103644042 A CN103644042 A CN 103644042A
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Abstract
The invention relates to the field of thermal energy and power, and particularly discloses a jet rotor engine which comprises a spray pipe, a forward-rotating structural body, a backward-rotating structural body and an auxiliary forward-rotating structural body, wherein the spray pipe is arranged on the forward-rotating structural body, with torque; the backward-rotating structural body is arranged at the outer part of the forward-rotating structural body; the auxiliary forward-rotating structural body is arranged at the outer part of the backward-rotating structural body, and is fixedly connected with the forward-rotating structural body; an impact transmission fluid passage is arranged on the backward-rotating structural body; an impact transmission fluid passage is arranged on the auxiliary forward-rotating structural body; a working medium inlet is communicated with a high-pressure working medium source; the static pressure of a working medium outlet of the spray pipe is less than 0.3 MPa; high-speed air sprayed from the spray pipe impacts and transmits the impact and transmission fluid passage arranged on the backward-rotating structural body and then impacts and the transmits the impact transmission fluid passage arranged on the auxiliary forward-rotating structural body. The jet rotor engine has a simple structure, and is high in power density and high in efficiency.
Description
Technical field
The present invention relates to heat energy and power field, particularly a kind of air injection rotor engine.
Background technique
Piston internal-combustion engine specific power is low, and steam turbine, gas turbine and jet engine specific power are high, but after miniaturization, (MW class or MW class are following) efficiency obviously declines, and therefore need to invent a kind of novel motor.
Summary of the invention
To achieve these goals, the technological scheme that the present invention proposes is as follows:
Scheme 1: a kind of air injection rotor engine, comprise jet pipe, be rotated in the forward structure, counterrotating structure and be rotated in the forward accessory structure body, described jet pipe has square to be rotated in the forward on structure described in being arranged on, described in being arranged on, described counterrotating structure is rotated in the forward the outside of structure, describedly be rotated in the forward the outside that accessory structure body is arranged on described counterrotating structure, described be rotated in the forward accessory structure body with described in be rotated in the forward structure and be connected, on described counterrotating structure, arrange and impact power transmitting fluids passage, described being rotated in the forward on accessory structure body, arranging and impact power transmitting fluids passage, the working medium entrance of described jet pipe is communicated with high-pressure working medium source, the static pressure at the sender property outlet place of described jet pipe is less than 0.3MPa, the high-speed gas of described jet pipe ejection is rotated in the forward the described impact power transmitting fluids passage impact transmission on accessory structure body again after being arranged on the described impact power transmitting fluids passage impact transmission on described counterrotating structure described in being arranged on.
Scheme 2: a kind of air injection rotor engine, comprise jet pipe, be rotated in the forward structure, counterrotating structure and be rotated in the forward accessory structure body, described jet pipe has square to be rotated in the forward on structure described in being arranged on, the vertical plane of the axis of described jet pipe and described in the angle that is rotated in the forward between the vertical plane of axis of structure be less than 90 degree, described be rotated in the forward structure with described in be rotated in the forward accessory structure body on same axis by the axial direction setting that is connected, described counterrotating structure suit be arranged on by described be rotated in the forward structure and described in be rotated in the forward the outside of the rotor that accessory structure body forms, on described counterrotating structure, arrange and impact power transmitting fluids passage, described being rotated in the forward on accessory structure body, arranging and impact power transmitting fluids passage, the working medium entrance of described jet pipe is communicated with high-pressure working medium source, the static pressure at the sender property outlet place of described jet pipe is less than 0.3MPa, the high-speed gas of described jet pipe ejection impacts after transmission the trend axis of being turned back and the more described impact power transmitting fluids passage being rotated in the forward on accessory structure body described in being arranged on is impacted to transmission being arranged on described impact power transmitting fluids passage on described counterrotating structure.
Scheme 3: a kind of air injection rotor engine, comprise jet pipe, be rotated in the forward structure, counterrotating structure and be rotated in the forward accessory structure body, described jet pipe has square to be rotated in the forward on structure described in being arranged on, the vertical plane of the axis of described jet pipe and described in the angle that is rotated in the forward between the vertical plane of axis of structure be less than 90 degree, the described structure that is rotated in the forward, described counterrotating structure and described in be rotated in the forward accessory structure body and by axial direction, set gradually on same axis, on described counterrotating structure, arrange and impact power transmitting fluids passage, described being rotated in the forward on accessory structure body, arranging and impact power transmitting fluids passage, the working medium entrance of described jet pipe is communicated with high-pressure working medium source, the static pressure at the sender property outlet place of described jet pipe is less than 0.3MPa, the high-speed gas of described jet pipe ejection is rotated in the forward the described impact power transmitting fluids passage impact transmission on accessory structure body again after being arranged on the described impact power transmitting fluids passage impact transmission on described counterrotating structure described in being arranged on.
Scheme 4: a kind of air injection rotor engine, comprise jet pipe, be rotated in the forward structure, counterrotating structure and be rotated in the forward accessory structure body, described jet pipe has square to be rotated in the forward on structure described in being arranged on, described in being arranged on, described counterrotating structure suit is rotated in the forward the outside of structure, the described accessory structure body that is rotated in the forward is set with the outside that is arranged on described counterrotating structure, described be rotated in the forward accessory structure body with described in be rotated in the forward structure and be connected, on described counterrotating structure, arrange and impact power transmitting fluids passage, described being rotated in the forward on accessory structure body, arranging and impact power transmitting fluids passage, the working medium entrance of described jet pipe is communicated with high-pressure working medium source, the static pressure at the sender property outlet place of described jet pipe is less than 0.3MPa, the high-speed gas of described jet pipe ejection is rotated in the forward the described impact power transmitting fluids passage impact transmission on accessory structure body again after being arranged on the described impact power transmitting fluids passage impact transmission on described counterrotating structure described in being arranged on.
Scheme 5: a kind of air injection rotor engine, comprise jet pipe, be rotated in the forward structure, counterrotating structure and be rotated in the forward accessory structure body, described jet pipe has square to be rotated in the forward on structure described in being arranged on, described in being arranged on, described counterrotating structure suit is rotated in the forward the inside of structure, the described accessory structure body that is rotated in the forward is set with the inside that is arranged on described counterrotating structure, described be rotated in the forward accessory structure body with described in be rotated in the forward structure and be connected, on described counterrotating structure, arrange and impact power transmitting fluids passage, described being rotated in the forward on accessory structure body, arranging and impact power transmitting fluids passage, the working medium entrance of described jet pipe is communicated with high-pressure working medium source, the static pressure at the sender property outlet place of described jet pipe is less than 0.3MPa, the high-speed gas of described jet pipe ejection is rotated in the forward the described impact power transmitting fluids passage impact transmission on accessory structure body again after being arranged on the described impact power transmitting fluids passage impact transmission on described counterrotating structure described in being arranged on.
Scheme 6: a kind of air injection rotor engine, comprise jet pipe, be rotated in the forward structure, counterrotating structure and be rotated in the forward accessory structure body, described jet pipe has square to be rotated in the forward on structure described in being arranged on, the vertical plane of the axis of described jet pipe and described in the angle that is rotated in the forward between the vertical plane of axis of structure be less than 90 degree, described be rotated in the forward structure with described in be rotated in the forward accessory structure body on same axis by the axial direction setting that is connected, described counterrotating structure suit be arranged on by described be rotated in the forward structure and described in be rotated in the forward the inside of the rotor that accessory structure body forms, on described counterrotating structure, arrange and impact power transmitting fluids passage, described being rotated in the forward on accessory structure body, arranging and impact power transmitting fluids passage, the working medium entrance of described jet pipe is communicated with high-pressure working medium source, the static pressure at the sender property outlet place of described jet pipe is less than 0.3MPa, the high-speed gas of described jet pipe ejection impacts after transmission to be turned back and the more described impact power transmitting fluids passage being rotated in the forward on accessory structure body described in being arranged on is impacted to transmission away from axis being arranged on described impact power transmitting fluids passage on described counterrotating structure.
Scheme 7: on the basis of arbitrary scheme, further selectable in above-mentioned all schemes, described high-pressure working medium source is made as internal combustion firing chamber, internal combustion evaporation device, external combustion vaporizer or is made as compressed gas source.
In the present invention, so-called " described jet pipe has square to be rotated in the forward on structure described in being arranged on " refer to described jet pipe spray suffered reaction force with described in to be rotated in the forward the spin axis of structure non-intersect, be that described jet pipe forms moment of torsion by spraying gained reaction force for the described spin axis that is rotated in the forward structure, the injection direction of the nozzle of described jet pipe can be the direction that is rotated in the forward the axis of structure away from described, spray from inside to outside, the injection direction of the nozzle of described jet pipe can be also the direction that is rotated in the forward the axis of structure described in convergence, be that ecto-entad sprays.
In the present invention, the injection direction that so-called " vertical plane of the axis of described jet pipe and described in the angle that is rotated in the forward between the vertical plane of axis of structure be less than 90 degree " refers to described jet pipe not with the perpendicular plane of the described axis that is rotated in the forward structure in.
In the present invention, the vertical plane of the axis of described jet pipe and described in the angle that is rotated in the forward between the vertical plane of axis of structure be less than in the structure of 90 degree, should determine the position on the axis that is rotated in the forward structure described in described counterrotating construction according to known technology.
In the present invention, so-called " rotational structure body " refers to the parts with a fixed structure that can rotate, for example, be fixed on the roulette wheel on running shaft.
In the present invention, so-called " forward " and " oppositely " are in order to distinguish the difference of sense of rotation, when forward is when taking advantage of a situation pin, are reversed counterclockwise, when forward is while being counterclockwise, are reversed clockwise.
In the present invention, so-called " impacting power transmitting fluids passage " refers to when accepting high-speed gas impact, the fluid passage that can produce moment.
In the present invention, so-called " high-pressure working medium source " refers to that pressure is greater than 0.5MPa, 0.6MPa, 0.7MPa, 0.8MPa, 0.9MPa, 1.0MPa, 1.1MPa, 1.2MPa, 1.3MPa, 1.4MPa, 1.5MPa, 1.6MPa, 1.7MPa, 1.8 MPa, 1.9MPa or is greater than the gas source of 2.0MPa.
In the present invention, the static pressure at the sender property outlet place of described jet pipe is less than 0.3MPa, 0.25MPa, 0.2MPa, 0.15MPa, 0.10MPa, 0.05MPa, 0.04MPa, 0.03MPa, 0.02MPa, 0.01MPa, 0.009MPa, 0.008MPa, 0.007MPa, 0.006MPa or is less than 0.005MPa.
In the present invention, described in be rotated in the forward structure, described counterrotating structure and described in be rotated in the forward accessory structure body can be individually or simultaneously external outputting power.
In the present invention, when described high-pressure working medium source is made as to described compressed gas source, as suitable in its pressure and temperature value, can formation temperature after acting lower than the gas of ambient temperature, form refrigerating function.
In the present invention, the pressure and temperature of the gas working medium in described high-pressure working medium source meets the adiabatic relation of class.
In the present invention, the adiabatic relation of so-called class comprises following three kinds of situations: 1. at the adiabatic relation curve of the working medium working medium thermal insulation relation curve of standard state point (through) above, the status parameter point of gas working medium is in Fig. 7 shown in O-A-H on curve for the status parameter of gas working medium (being the temperature and pressure of working medium) point, 2. the status parameter of gas working medium (being the temperature and pressure of working medium) point is in the adiabatic relation curve of described working medium left side, the i.e. left side of the status parameter point of gas working medium curve shown in O-A-H in Fig. 7, 3. the status parameter of gas working medium (being the temperature and pressure of working medium) point is on the adiabatic relation curve of described working medium right side, be the right side of status parameter point curve shown in O-A-H in Fig. 7 of gas working medium, but the temperature of gas working medium not higher than the pressure of gas working medium thus by adiabatic relation calculate gained temperature add 1000K's and, add 950K and, add 900K and, add 850K and, add 800K and, add 750K and, add 700K and, add 650K and, add 600K and, add 550K and, add 500K and, add 450K and, add 400K and, add 350K and, add 300K and, add 250K and, add 200K and, add 190K and, add 180K and, add 170K and, add 160K and, add 150K and, add 140K and, add 130K and, add 120K and, add 110K and, add 100K and, add 90K and, add 80K and, add 70K and, add 60K and, add 50K and, add 40K and, add 30K's and/or not higher than add 20K and, as shown in Figure 7, the virtual condition point of described gas working medium is B point, A point is the point on the adiabatic relation curve that pressure is identical with B point, the temperature difference between A point and B point should be less than 1000K, 900K, 850K, 800K, 750K, 700K, 650K, 600K, 550K, 500K, 450K, 400K, 350K, 300K, 250K, 200K, 190K, 180K, 170K, 160K, 150K, 140K, 130K, 120K, 110K, 100K, 90K, 80K, 70K, 60K, 50K, 40K, 30K or be less than 20K.
In the present invention, the adiabatic relation of so-called class can be any in above-mentioned three kinds of situations, namely refers to: the status parameter of the gas working medium in described high-pressure working medium source (being the temperature and pressure of gas working medium) point is in the left field of adiabatic process curve E-B-D orderring by B as shown in Figure 7.
In the present invention, should, according to the known technology in energy and power engineering field, in necessary place, necessary parts, unit or system be set.
Beneficial effect of the present invention is as follows:
The present invention is simple in structure, specific power is high, efficiency is high.
Accompanying drawing explanation
Shown in Fig. 1 is the structural representation of the embodiment of the present invention 1;
Shown in Fig. 2 is the structural representation of the embodiment of the present invention 2;
Shown in Fig. 3 is the structural representation of the embodiment of the present invention 3;
Shown in Fig. 4 is the structural representation of the embodiment of the present invention 4;
Shown in Fig. 5 is the structural representation of the embodiment of the present invention 5;
Shown in Fig. 6 is the structural representation of the embodiment of the present invention 6;
Shown in Fig. 7 is the graph of a relation of temperature T and the pressure P of the gas working medium in high-pressure working medium source of the present invention.
In figure:
1 jet pipe, 2 is rotated in the forward structure, 3 counterrotating structures, 4 are rotated in the forward accessory structure body, 5 high-pressure working medium sources.
Embodiment
Air injection rotor engine as shown in Figure 1, comprise jet pipe 1, be rotated in the forward structure 2, counterrotating structure 3 and be rotated in the forward accessory structure body 4, described jet pipe 1 has square to be rotated in the forward on structure 2 described in being arranged on, described in being arranged on, described counterrotating structure 3 is rotated in the forward the outside of structure 2, the described accessory structure body 4 that is rotated in the forward arranges described counterrotating structure 3 outsides, described be rotated in the forward accessory structure body 4 with described in be rotated in the forward structure 2 and be connected, on described counterrotating structure 3, arrange and impact power transmitting fluids passage 31, described being rotated in the forward on accessory structure body 4, arranging and impact power transmitting fluids passage 41, the working medium entrance of described jet pipe 1 is communicated with high-pressure working medium source 5, the static pressure at the sender property outlet place of described jet pipe 1 is less than 0.3MPa, the high-speed gas of described jet pipe 1 ejection is rotated in the forward the described impact power transmitting fluids passage 41 impact transmissions on accessory structure body 4 again after being arranged on the described impact power transmitting fluids passage 31 impact transmissions on described counterrotating structure 3 described in being arranged on.
Air injection rotor engine as shown in Figure 2, comprise jet pipe 1, be rotated in the forward structure 2, counterrotating structure 3 and be rotated in the forward accessory structure body 4, described jet pipe 1 has square to be rotated in the forward on structure 2 described in being arranged on, the vertical plane of the axis of described jet pipe 1 and described in the angle that is rotated in the forward between the vertical plane of axis of structure 2 be less than 90 degree, described be rotated in the forward structure 2 with described in be rotated in the forward accessory structure body 4 on same axis by the axial direction setting that is connected, described in described counterrotating structure 3 suits are arranged on, be rotated in the forward structure 2 and described in be rotated in the forward the outside of the rotor that accessory structure body 4 forms, on described counterrotating structure 2, arrange and impact power transmitting fluids passage 31, described being rotated in the forward on accessory structure body 4, arranging and impact power transmitting fluids passage 41, the working medium entrance of described jet pipe 1 is communicated with high-pressure working medium source 5, the static pressure at the sender property outlet place of described jet pipe 1 is less than 0.3MPa, the high-speed gas of described jet pipe 1 ejection impacts after transmissions the trend axis of being turned back and the more described impact power transmitting fluids passage 41 being rotated in the forward on accessory structure body 4 described in being arranged on is impacted to transmissions being arranged on described impact power transmitting fluids passage 31 on described counterrotating structure 3.
Air injection rotor engine as shown in Figure 3, comprise jet pipe 1, be rotated in the forward structure 2, counterrotating structure 3 and be rotated in the forward accessory structure body 4, described jet pipe 1 has square to be rotated in the forward on structure 2 described in being arranged on, the vertical plane of the axis of described jet pipe 1 and described in the angle that is rotated in the forward between the vertical plane of axis of structure 2 be less than 90 degree, the described structure 2 that is rotated in the forward, described counterrotating structure 3 and described in be rotated in the forward accessory structure body 4 on same axis by axial direction setting, on described counterrotating structure 3, arrange and impact power transmitting fluids passage 31, described being rotated in the forward on accessory structure body 4, arranging and impact power transmitting fluids passage 41, the working medium entrance of described jet pipe 1 is communicated with high-pressure working medium source 5, the static pressure at the sender property outlet place of described jet pipe 1 is less than 0.3MPa, the high-speed gas of described jet pipe 1 ejection is rotated in the forward the described impact power transmitting fluids passage 41 impact transmissions on accessory structure body 4 again after being arranged on the described impact power transmitting fluids passage 31 impact transmissions on described counterrotating structure 3 described in being arranged on.
Air injection rotor engine as shown in Figure 4, comprise jet pipe 1, be rotated in the forward structure 2, counterrotating structure 3 and be rotated in the forward accessory structure body 4, described jet pipe 1 has square to be rotated in the forward on structure 2 described in being arranged on, described in being arranged on, described counterrotating structure 3 suits are rotated in the forward the outside of structure 2, the described accessory structure body 4 that is rotated in the forward is set with the outside that described counterrotating structure 3 is set, described be rotated in the forward accessory structure body 4 with described in be rotated in the forward structure 2 and be connected, on described counterrotating structure 3, arrange and impact power transmitting fluids passage 31, described being rotated in the forward on accessory structure body 4, arranging and impact power transmitting fluids passage 41, the working medium entrance of described jet pipe 1 is communicated with high-pressure working medium source 5, the static pressure at the sender property outlet place of described jet pipe 1 is less than 0.3MPa, the high-speed gas of described jet pipe 1 ejection is rotated in the forward the described impact power transmitting fluids passage 41 impact transmissions on accessory structure body 4 again after being arranged on the described impact power transmitting fluids passage 31 impact transmissions on described counterrotating structure 3 described in being arranged on.
The present embodiment is also a kind of concrete form of implementation of the embodiment 1.
Air injection rotor engine as shown in Figure 5, comprise jet pipe 1, be rotated in the forward structure 2, counterrotating structure 3 and be rotated in the forward accessory structure body 4, described jet pipe 1 has square to be rotated in the forward on structure 2 described in being arranged on, described in being arranged on, described counterrotating structure 3 suits are rotated in the forward the inside of structure 2, the described accessory structure body 4 that is rotated in the forward is set with the inside that described counterrotating structure 3 is set, described be rotated in the forward accessory structure body 4 with described in be rotated in the forward structure 2 and be connected, on described counterrotating structure 3, arrange and impact power transmitting fluids passage 31, described being rotated in the forward on accessory structure body 4, arranging and impact power transmitting fluids passage 41, the working medium entrance of described jet pipe 1 is communicated with high-pressure working medium source 5, the static pressure at the sender property outlet place of described jet pipe 1 is less than 0.3MPa, the high-speed gas of described jet pipe 1 ejection is rotated in the forward the described impact power transmitting fluids passage 41 impact transmissions on accessory structure body 4 again after being arranged on the described impact power transmitting fluids passage 31 impact transmissions on described counterrotating structure 3 described in being arranged on.
Embodiment 6
Air injection rotor engine as shown in Figure 6, comprise jet pipe 1, be rotated in the forward structure 2, counterrotating structure 3 and be rotated in the forward accessory structure body 4, it is characterized in that: described jet pipe 1 has square to be rotated in the forward on structure 2 described in being arranged on, the vertical plane of the axis of described jet pipe 1 and described in the angle that is rotated in the forward between the vertical plane of axis of structure 2 be less than 90 degree, described be rotated in the forward structure 2 with described in be rotated in the forward accessory structure body 4 on same axis by the axial direction setting that is connected, described in described counterrotating structure 3 suits are arranged on, be rotated in the forward structure 2 and described in be rotated in the forward the inside of the rotor that accessory structure body 4 forms, on described counterrotating structure 3, arrange and impact power transmitting fluids passage 31, described being rotated in the forward on accessory structure body 4, arranging and impact power transmitting fluids passage 41, the working medium entrance of described jet pipe 1 is communicated with high-pressure working medium source 5, the static pressure at the sender property outlet place of described jet pipe 1 is less than 0.3MPa, the high-speed gas of described jet pipe 1 ejection impacts after transmissions to be turned back and the more described impact power transmitting fluids passage 41 being rotated in the forward on accessory structure body 4 described in being arranged on is impacted to transmissions away from axis being arranged on described impact power transmitting fluids passage 31 on described counterrotating structure 3.
The injection direction when injection direction of the described jet pipe 1 in accompanying drawing corresponding to various embodiments of the present invention does not represent practical application, it is only in order to facilitate the trend of signal working medium, while practicing, described jet pipe 1 should have square to be rotated in the forward on structure 2 described in being arranged on, and should make the high-speed gas of described jet pipe 1 ejection can impact on the described impact power transmitting fluids passage 31 being arranged on described counterrotating structure 3.
In above-mentioned all embodiments of the present invention, described high-pressure working medium source 5 can be made as to internal combustion firing chamber, internal combustion evaporation device, external combustion vaporizer or be made as pressurized gas.
Above-mentioned all mode of executions of the present invention in the specific implementation, can be made as the pressure of described high-pressure working medium source 5 to be greater than 0.5MPa, 0.6MPa, 0.7MPa, 0.8MPa, 0.9MPa, 1.0MPa, 1.1MPa, 1.2MPa, 1.3MPa, 1.4MPa, 1.5MPa, 1.6MPa, 1.7MPa, 1.8 MPa, 1.9MPa or to be greater than 2.0MPa.
As the mode of execution that can convert, in above-mentioned all mode of executions of the present invention, the static pressure at the sender property outlet place of described jet pipe 1 can be changed to be made as to be less than 0.25MPa, 0.2MPa, 0.15MPa, 0.10MPa, 0.05MPa, 0.04MPa, 0.03MPa, 0.02MPa or to change to be made as and be less than 0.01MPa and replace the static pressure at the sender property outlet place of described jet pipe 1 to be made as and to be less than 0.3MPa.
As disposable mode of execution, in all mode of executions of the present invention, the number of described jet pipe 1 all can increase and decrease on existing basis, does not affect the realization of the object of the invention.
In all of the embodiments of the present invention, described high-pressure working medium source 5 all with described in be rotated in the forward structure and be arranged for 2 minutes, during described air injection rotor engine work, described high-pressure working medium source 5 does not rotate with the described structure 2 that is rotated in the forward, as the mode of execution that can convert, described high-pressure working medium source 5 can change into and is rotated in the forward on structure 2 described in being arranged on or changes into the described structure 2 that is rotated in the forward and being connected, and when described air injection rotor engine work, with the described structure 2 that is rotated in the forward, rotate.
Obviously, the invention is not restricted to above embodiment, according to the known technology of related domain and technological scheme disclosed in this invention, can derive or association goes out many flexible programs, all these flexible programs, also should think protection scope of the present invention.
Claims (7)
1. an air injection rotor engine, comprise jet pipe (1), be rotated in the forward structure (2), counterrotating structure (3) and be rotated in the forward accessory structure body (4), it is characterized in that: described jet pipe (1) has square to be rotated in the forward on structure (2) described in being arranged on, described in being arranged on, described counterrotating structure (3) is rotated in the forward the outside of structure (2), describedly be rotated in the forward the outside that accessory structure body (4) is arranged on described counterrotating structure (3), described be rotated in the forward accessory structure body (4) with described in be rotated in the forward structure (2) and be connected, on described counterrotating structure (3), arrange and impact power transmitting fluids passage (31), described being rotated in the forward on accessory structure body (4), arranging and impact power transmitting fluids passage (41), the working medium entrance of described jet pipe (1) is communicated with high-pressure working medium source (5), the static pressure at the sender property outlet place of described jet pipe (1) is less than 0.3MPa, the high-speed gas of described jet pipe (1) ejection is rotated in the forward described impact power transmitting fluids passage (41) the impact transmission on accessory structure body (4) again after being arranged on described impact power transmitting fluids passage (31) the impact transmission on described counterrotating structure (3) described in being arranged on.
2. an air injection rotor engine, comprise jet pipe (1), be rotated in the forward structure (2), counterrotating structure (3) and be rotated in the forward accessory structure body (4), it is characterized in that: described jet pipe (1) has square to be rotated in the forward on structure (2) described in being arranged on, the vertical plane of the axis of described jet pipe (1) and described in the angle that is rotated in the forward between the vertical plane of axis of structure (2) be less than 90 degree, described be rotated in the forward structure (2) with described in be rotated in the forward accessory structure body (4) on same axis by the axial direction setting that is connected, described counterrotating structure (3) suit be arranged on by described be rotated in the forward structure (2) and described in be rotated in the forward the outside of the rotor that accessory structure body (4) forms, on described counterrotating structure (3), arrange and impact power transmitting fluids passage (31), described being rotated in the forward on accessory structure body (4), arranging and impact power transmitting fluids passage (41), the working medium entrance of described jet pipe (1) is communicated with high-pressure working medium source (5), the static pressure at the sender property outlet place of described jet pipe (1) is less than 0.3MPa, the high-speed gas of described jet pipe (1) ejection impacts after transmission the trend axis of being turned back and the more described impact power transmitting fluids passage (41) being rotated in the forward on accessory structure body (4) described in being arranged on is impacted to transmission being arranged on described impact power transmitting fluids passage (31) on described counterrotating structure (3).
3. an air injection rotor engine, comprise jet pipe (1), be rotated in the forward structure (2), counterrotating structure (3) and be rotated in the forward accessory structure body (4), it is characterized in that: described jet pipe (1) has square to be rotated in the forward on structure (2) described in being arranged on, the vertical plane of the axis of described jet pipe (1) and described in the angle that is rotated in the forward between the vertical plane of axis of structure (2) be less than 90 degree, the described structure (2) that is rotated in the forward, described counterrotating structure (3) and described in be rotated in the forward accessory structure body (4) and by axial direction, set gradually on same axis, on described counterrotating structure (3), arrange and impact power transmitting fluids passage (31), described being rotated in the forward on accessory structure body (4), arranging and impact power transmitting fluids passage (41), the working medium entrance of described jet pipe (1) is communicated with high-pressure working medium source (5), the static pressure at the sender property outlet place of described jet pipe (1) is less than 0.3MPa, the high-speed gas of described jet pipe (1) ejection is rotated in the forward described impact power transmitting fluids passage (41) the impact transmission on accessory structure body (4) again after being arranged on described impact power transmitting fluids passage (31) the impact transmission on described counterrotating structure (3) described in being arranged on.
4. an air injection rotor engine, comprise jet pipe (1), be rotated in the forward structure (2), counterrotating structure (3) and be rotated in the forward accessory structure body (4), it is characterized in that: described jet pipe (1) has square to be rotated in the forward on structure (2) described in being arranged on, described in being arranged on, described counterrotating structure (3) suit is rotated in the forward the outside of structure (2), the described accessory structure body (4) that is rotated in the forward is set with the outside that is arranged on described counterrotating structure (3), described be rotated in the forward accessory structure body (4) with described in be rotated in the forward structure (2) and be connected, on described counterrotating structure (3), arrange and impact power transmitting fluids passage (31), described being rotated in the forward on accessory structure body (4), arranging and impact power transmitting fluids passage (41), the working medium entrance of described jet pipe (1) is communicated with high-pressure working medium source (5), the static pressure at the sender property outlet place of described jet pipe (1) is less than 0.3MPa, the high-speed gas of described jet pipe (1) ejection is rotated in the forward described impact power transmitting fluids passage (41) the impact transmission on accessory structure body (4) again after being arranged on described impact power transmitting fluids passage (31) the impact transmission on described counterrotating structure (3) described in being arranged on.
5. an air injection rotor engine, comprise jet pipe (1), be rotated in the forward structure (2), counterrotating structure (3) and be rotated in the forward accessory structure body (4), it is characterized in that: described jet pipe (1) has square to be rotated in the forward on structure (2) described in being arranged on, described in being arranged on, described counterrotating structure (3) suit is rotated in the forward the inside of structure (2), the described accessory structure body (4) that is rotated in the forward is set with the inside that is arranged on described counterrotating structure (3), described be rotated in the forward accessory structure body (4) with described in be rotated in the forward structure (2) and be connected, on described counterrotating structure (3), arrange and impact power transmitting fluids passage (31), described being rotated in the forward on accessory structure body (4), arranging and impact power transmitting fluids passage (41), the working medium entrance of described jet pipe (1) is communicated with high-pressure working medium source (5), the static pressure at the sender property outlet place of described jet pipe (1) is less than 0.3MPa, the high-speed gas of described jet pipe (1) ejection is rotated in the forward described impact power transmitting fluids passage (41) the impact transmission on accessory structure body (4) again after being arranged on described impact power transmitting fluids passage (31) the impact transmission on described counterrotating structure (3) described in being arranged on.
6. an air injection rotor engine, comprise jet pipe (1), be rotated in the forward structure (2), counterrotating structure (3) and be rotated in the forward accessory structure body (4), it is characterized in that: described jet pipe (1) has square to be rotated in the forward on structure (2) described in being arranged on, the vertical plane of the axis of described jet pipe (1) and described in the angle that is rotated in the forward between the vertical plane of axis of structure (2) be less than 90 degree, described be rotated in the forward structure (2) with described in be rotated in the forward accessory structure body (4) on same axis by the axial direction setting that is connected, described in described counterrotating structure (3) suit is arranged on, be rotated in the forward structure (2) and described in be rotated in the forward the inside of the rotor of accessory structure body (4) formation, on described counterrotating structure (3), arrange and impact power transmitting fluids passage (31), described being rotated in the forward on accessory structure body (4), arranging and impact power transmitting fluids passage (41), the working medium entrance of described jet pipe (1) is communicated with high-pressure working medium source (5), the static pressure at the sender property outlet place of described jet pipe (1) is less than 0.3MPa, the high-speed gas of described jet pipe (1) ejection impacts after transmission to be turned back and the more described impact power transmitting fluids passage (41) being rotated in the forward on accessory structure body (41) described in being arranged on is impacted to transmission away from axis being arranged on described impact power transmitting fluids passage (31) on described counterrotating structure (3).
7. air injection rotor engine as described in any one in claim 1 to 6, is characterized in that: described high-pressure working medium source (5) is made as internal combustion firing chamber, internal combustion evaporation device, external combustion vaporizer or is made as compressed gas source.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310726889.7A CN103644042A (en) | 2012-12-25 | 2013-12-25 | Jet rotor engine |
Applications Claiming Priority (7)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210572500 | 2012-12-25 | ||
| CN201210572500.3 | 2012-12-25 | ||
| CN201310000613.0 | 2013-01-03 | ||
| CN201310000613 | 2013-01-03 | ||
| CN201310025399 | 2013-01-23 | ||
| CN201310025399.4 | 2013-01-23 | ||
| CN201310726889.7A CN103644042A (en) | 2012-12-25 | 2013-12-25 | Jet rotor engine |
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| Publication Number | Publication Date |
|---|---|
| CN103644042A true CN103644042A (en) | 2014-03-19 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310726889.7A Pending CN103644042A (en) | 2012-12-25 | 2013-12-25 | Jet rotor engine |
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| CN (1) | CN103644042A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108519203A (en) * | 2018-03-14 | 2018-09-11 | 蔡斌奇 | New gas vibrator |
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| US5560196A (en) * | 1993-12-15 | 1996-10-01 | Schlote; Andrew | Rotary heat engine |
| CN1354322A (en) * | 2000-11-17 | 2002-06-19 | 祝长宇 | Jet rotary engine |
| CN1423033A (en) * | 2001-11-22 | 2003-06-11 | 白葆山 | External-compression rotary piston engine |
| US20070214794A1 (en) * | 2006-03-15 | 2007-09-20 | Tweeton Erik H | Supercharged subsonic rotary ramjet turbine with vibration free piston air compressor |
| CN102278233A (en) * | 2010-07-07 | 2011-12-14 | 靳北彪 | Supersonic rotor engine |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5560196A (en) * | 1993-12-15 | 1996-10-01 | Schlote; Andrew | Rotary heat engine |
| CN1354322A (en) * | 2000-11-17 | 2002-06-19 | 祝长宇 | Jet rotary engine |
| CN1423033A (en) * | 2001-11-22 | 2003-06-11 | 白葆山 | External-compression rotary piston engine |
| US20070214794A1 (en) * | 2006-03-15 | 2007-09-20 | Tweeton Erik H | Supercharged subsonic rotary ramjet turbine with vibration free piston air compressor |
| CN102278233A (en) * | 2010-07-07 | 2011-12-14 | 靳北彪 | Supersonic rotor engine |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN108519203A (en) * | 2018-03-14 | 2018-09-11 | 蔡斌奇 | New gas vibrator |
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Application publication date: 20140319 |