CN106762216A - Velocity profile acting mechanism engine - Google Patents
Velocity profile acting mechanism engine Download PDFInfo
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- CN106762216A CN106762216A CN201710087466.3A CN201710087466A CN106762216A CN 106762216 A CN106762216 A CN 106762216A CN 201710087466 A CN201710087466 A CN 201710087466A CN 106762216 A CN106762216 A CN 106762216A
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- air source
- jet pipe
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- velocity profile
- revolving combustor
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Abstract
The invention discloses a kind of velocity profile acting mechanism engine, including liquefied air source (11), non-rotating combustion chamber (2) and jet pipe (3), the liquefied air source (11), the non-rotating combustion chamber (2) and the jet pipe (3) are sequentially communicated, and the bearing capacity of the liquefied air source (11) is more than 5MPa.The velocity profile acting mechanism engine power density of the invention is high, and efficiency high, disposal of pollutants is few, and fuel diversity is good.
Description
The application is original applying number for 201410240416.0, original application day is on 05 30th, 2014, entitled speed
The divisional application of type acting mechanism engine.
Technical field
The present invention relates to heat energy and dynamic field, especially a kind of velocity profile acting mechanism engine.
Background technology
Internal-combustion piston engine power density is low, and disposal of pollutants is serious, and demanded fuel is harsh, and gas turbine proficiency is low, therefore
Need to invent a kind of new work engine.
The content of the invention
In order to solve the above problems, technical scheme proposed by the present invention is as follows：
Scheme 1, a kind of velocity profile acting mechanism engine, including compressed air source, non-rotating combustion chamber and jet pipe, it is described
Compressed air source, the non-rotating combustion chamber and the jet pipe are sequentially communicated, and the bearing capacity of the compressed air source is more than
5MPa, sets cooling duct on the wall of the non-rotating combustion chamber, and the compressed air source is through the cooling duct and described non-
Revolving combustor is connected.
Scheme 2, a kind of velocity profile acting mechanism engine, including compressed air source, non-rotating combustion chamber and turbine, it is described
Compressed air source, the non-rotating combustion chamber and the turbine are sequentially communicated, and the bearing capacity of the compressed air source is more than
5MPa, sets cooling duct on the wall of the non-rotating combustion chamber, and the compressed air source is through the cooling duct and described non-
Revolving combustor is connected.
Scheme 3, a kind of velocity profile acting mechanism engine, including compressed air source, non-rotating combustion chamber and jet pipe, it is described
Compressed air source, the non-rotating combustion chamber and the jet pipe are sequentially communicated, and the bearing capacity of the compressed air source is more than
5MPa, the velocity profile acting mechanism engine also includes cooling fluid source and cooling fluid vaporizer jet pipe, in the non-rotation
Turn to set cooling duct on the wall of combustion chamber, the cooling fluid source is connected with the cooling duct, the cooling duct and described
Cooling fluid vaporizer jet pipe is connected.
Scheme 4, a kind of velocity profile acting mechanism engine, including compressed air source, non-rotating combustion chamber and turbine, it is described
Compressed air source, the non-rotating combustion chamber and the turbine are sequentially communicated, and the bearing capacity of the compressed air source is more than
5MPa, the velocity profile acting mechanism engine also includes cooling fluid source and cooling fluid vaporizer turbine, in the non-rotation
Turn to set cooling duct on the wall of combustion chamber, the cooling fluid source is connected with the cooling duct, the cooling duct and described
Cooling fluid vaporizer turbine is connected.
Scheme 5, a kind of velocity profile acting mechanism engine, including compressed air source, non-rotating combustion chamber and jet pipe, it is described
Compressed air source, the non-rotating combustion chamber and the jet pipe are sequentially communicated, and the bearing capacity of the compressed air source is more than
5MPa, the velocity profile acting mechanism engine also includes cooling fluid source, and cooling is set on the wall of the non-rotating combustion chamber
Passage, the cooling fluid source is connected with the cooling duct, the cooling duct and the non-rotating combustion chamber.
Scheme 6, a kind of velocity profile acting mechanism engine, including compressed air source, non-rotating combustion chamber and turbine, it is described
Compressed air source, the non-rotating combustion chamber and the turbine are sequentially communicated, and the bearing capacity of the compressed air source is more than
5MPa, the velocity profile acting mechanism engine also includes cooling fluid source, and cooling is set on the wall of the non-rotating combustion chamber
Passage, the cooling fluid source is connected with the cooling duct, the cooling duct and the non-rotating combustion chamber.
Scheme 7, a kind of velocity profile acting mechanism engine, including liquefied air source, non-rotating combustion chamber and jet pipe, it is described
Liquefied air source, the non-rotating combustion chamber and the jet pipe are sequentially communicated, and the bearing capacity in the liquefied air source is more than
5MPa。
Scheme 8, a kind of velocity profile acting mechanism engine, including liquefied air source, non-rotating combustion chamber and turbine, it is described
Liquefied air source, the non-rotating combustion chamber and the turbine are sequentially communicated, and the bearing capacity in the liquefied air source is more than
5MPa。
Scheme 9, on the basis of scheme 7 or 8, sets cooling duct, the liquid on the wall of the non-rotating combustion chamber
Change air-source through the cooling duct and the non-rotating combustion chamber.
Scheme 10, on the basis of scheme 7, the velocity profile acting mechanism engine also includes cooling fluid source and cooling
Fluid vaporization thing jet pipe, sets cooling duct on the wall of the non-rotating combustion chamber, and the cooling fluid source is logical with the cooling
Road is connected, and the cooling duct connects with the cooling fluid vaporizer jet pipe.
Scheme 11, on the basis of scheme 8, the velocity profile acting mechanism engine also includes cooling fluid source and cooling
Fluid vaporization thing turbine, sets cooling duct on the wall of the non-rotating combustion chamber, and the cooling fluid source is logical with the cooling
Road is connected, and the cooling duct connects with the cooling fluid vaporizer turbine.
Scheme 12, on the basis of scheme 7, the velocity profile acting mechanism engine also includes cooling fluid source, in institute
Cooling duct is set on the wall for stating non-rotating combustion chamber, the cooling fluid source is connected with the cooling duct, the cooling duct
With the non-rotating combustion chamber.
Scheme 13, on the basis of scheme 8, the velocity profile acting mechanism engine also includes cooling fluid source, in institute
Cooling duct is set on the wall for stating non-rotating combustion chamber, the cooling fluid source is connected with the cooling duct, the cooling duct
With the non-rotating combustion chamber.
Scheme 14, a kind of velocity profile acting mechanism engine, including compressed air source, revolving combustor and jet pipe, it is described
Jet pipe has square to set with the revolving combustor, and the compressed air source, the revolving combustor and the jet pipe are sequentially communicated,
The bearing capacity of the compressed air source is more than 5MPa, and cooling duct is set on the wall of the revolving combustor, and the compression is empty
Source of the gas is connected through the cooling duct with the revolving combustor.
Scheme 15, a kind of velocity profile acting mechanism engine, including compressed air source, revolving combustor and turbine, it is described
Compressed air source, the revolving combustor and the turbine are sequentially communicated, and the bearing capacity of the compressed air source is more than 5MPa,
Cooling duct is set on the wall of the revolving combustor, the compressed air source is through the cooling duct and the revolving combustor
Connection.
Scheme 16, a kind of velocity profile acting mechanism engine, including compressed air source, revolving combustor and jet pipe, it is described
Jet pipe has square to set with the revolving combustor, and the compressed air source, the revolving combustor and the jet pipe are sequentially communicated,
The bearing capacity of the compressed air source is more than 5MPa, and velocity profile acting mechanism engine also includes cooling fluid source and cold
But fluid vaporization thing jet pipe, sets cooling duct on the wall of the revolving combustor, and the cooling fluid source is logical with the cooling
Road is connected, and the cooling duct connects with the cooling fluid vaporizer jet pipe.
Scheme 17, a kind of velocity profile acting mechanism engine, including compressed air source, revolving combustor and turbine, it is described
Compressed air source, the revolving combustor and the turbine are sequentially communicated, and the bearing capacity of the compressed air source is more than 5MPa,
The velocity profile acting mechanism engine also includes cooling fluid source and cooling fluid vaporizer turbine, in the revolving combustor
Wall on set cooling duct, the cooling fluid source is connected with the cooling duct, the cooling duct and the cooling fluid
Vaporizer turbine is connected.
Scheme 18, a kind of velocity profile acting mechanism engine, including compressed air source, revolving combustor and jet pipe, it is described
Jet pipe has square to set with the revolving combustor, and the compressed air source, the revolving combustor and the jet pipe are sequentially communicated,
The bearing capacity of the compressed air source is more than 5MPa, and the velocity profile acting mechanism engine also includes cooling fluid source,
Cooling duct is set on the wall of the revolving combustor, the cooling fluid source is connected with the cooling duct, the cooling duct
Connected with the revolving combustor.
Scheme 19, a kind of velocity profile acting mechanism engine, including compressed air source, revolving combustor and turbine, it is described
Compressed air source, the revolving combustor and the turbine are sequentially communicated, and the bearing capacity of the compressed air source is more than 5MPa,
The velocity profile acting mechanism engine also includes cooling fluid source, and cooling duct, institute are set on the wall of the revolving combustor
State cooling fluid source to be connected with the cooling duct, the cooling duct connects with the revolving combustor.
Scheme 20, a kind of velocity profile acting mechanism engine, including liquefied air source, revolving combustor and jet pipe, it is described
Jet pipe has square to set with the revolving combustor, and the liquefied air source, the revolving combustor and the jet pipe are sequentially communicated,
The bearing capacity in the liquefied air source is more than 5MPa, and cooling duct is set on the wall of the revolving combustor, and the liquefaction is empty
Source of the gas is connected through the cooling duct with the revolving combustor.
Scheme 21, a kind of velocity profile acting mechanism engine, including liquefied air source, revolving combustor and jet pipe, it is described
Jet pipe has square to set with the revolving combustor, and the liquefied air source, the revolving combustor and the jet pipe are sequentially communicated,
The bearing capacity in the liquefied air source is more than 5MPa, and velocity profile acting mechanism engine also includes cooling fluid source and cold
But fluid vaporization thing jet pipe, sets cooling duct on the wall of the revolving combustor, and the cooling fluid source is logical with the cooling
Road is connected, and the cooling duct connects with the cooling fluid vaporizer jet pipe.
Scheme 22, a kind of velocity profile acting mechanism engine, including liquefied air source, revolving combustor and jet pipe, it is described
Jet pipe has square to set with the revolving combustor, and the liquefied air source, the revolving combustor and the jet pipe are sequentially communicated,
The bearing capacity in the liquefied air source is more than 5MPa, and the velocity profile acting mechanism engine also includes cooling fluid source,
Cooling duct is set on the wall of the revolving combustor, the cooling fluid source is connected with the cooling duct, the cooling duct
Connected with the revolving combustor.
Scheme 23, a kind of velocity profile acting mechanism engine, including liquefied air source, revolving combustor and turbine, it is described
Liquefied air source, the revolving combustor and the turbine are sequentially communicated, and the bearing capacity in the liquefied air source is more than 5MPa.
Scheme 24, on the basis of scheme 23, sets cooling duct, the liquefied air on the wall of the revolving combustor
Source connects through the cooling duct with the revolving combustor.
Scheme 25, on the basis of scheme 23, velocity profile acting mechanism engine also includes cooling fluid source and cold
But fluid vaporization thing turbine, sets cooling duct on the wall of the revolving combustor, and the cooling fluid source is logical with the cooling
Road is connected, and the cooling duct connects with the cooling fluid vaporizer turbine.
Scheme 26, on the basis of scheme 23, the velocity profile acting mechanism engine also includes cooling fluid source, in institute
State and cooling duct set on the wall of revolving combustor, the cooling fluid source is connected with the cooling duct, the cooling duct and
The revolving combustor connection.
Scheme 27, a kind of velocity profile acting mechanism engine, including liquefied air source, revolving combustor, centrifugation supercharging stream
Body passage and jet pipe, the jet pipe have square to set with the revolving combustor, the liquefied air source, the centrifugation charging fluid
Passage, the revolving combustor and the jet pipe are sequentially communicated, and the bearing capacity of the centrifugation charging fluid passage is more than 5MPa.
Scheme 28, a kind of velocity profile acting mechanism engine, including liquefied air source, revolving combustor, centrifugation supercharging stream
Body passage and turbine, the liquefied air source, the centrifugation charging fluid passage, the revolving combustor and the turbine are successively
Connection, the bearing capacity of the centrifugation charging fluid passage is more than 5MPa.
Scheme 29, on the basis of scheme 27 or 28, sets cooling duct, the liquid on the wall of the revolving combustor
Change air-source to be connected with the revolving combustor through the cooling duct.
Scheme 30, on the basis of scheme 27, velocity profile acting mechanism engine also includes cooling fluid source and cold
But fluid vaporization thing jet pipe, sets cooling duct on the wall of the revolving combustor, and the cooling fluid source is logical with the cooling
Road is connected, and the cooling duct connects with the cooling fluid vaporizer jet pipe.
Scheme 31, on the basis of scheme 28, velocity profile acting mechanism engine also includes cooling fluid source and cold
But fluid vaporization thing turbine, sets cooling duct on the wall of the revolving combustor, and the cooling fluid source is logical with the cooling
Road is connected, and the cooling duct connects with the cooling fluid vaporizer turbine.
Scheme 32, on the basis of scheme 27, the velocity profile acting mechanism engine also includes cooling fluid source, in institute
State and cooling duct set on the wall of revolving combustor, the cooling fluid source is connected with the cooling duct, the cooling duct and
The revolving combustor connection.
Scheme 33, on the basis of scheme 28, the velocity profile acting mechanism engine also includes cooling fluid source, in institute
State and cooling duct set on the wall of revolving combustor, the cooling fluid source is connected with the cooling duct, the cooling duct and
The revolving combustor connection.
In the present invention, so-called " jet pipe has square to set with the revolving combustor " refers to the jet pipe injection when institute
The reaction force being subject to produces the set-up mode of moment of torsion to the rotation axis of the revolving combustor.
In the present invention, the compressed air source can be compressed air reservoir, it is also possible to be to provide compressed air system,
Unit or mechanism.
In the present invention, the bearing capacity of the compressed air source more than 5MPa, 5.5MPa, 6.0MPa, 6.5MPa,
7.0MPa、7.5MPa、8.0MPa、8.5MPa、9.0MPa、9.5MPa、10.0MPa、10.5MPa、11.0MPa、11.5MPa、
12.0MPa、12.5MPa、13.0MPa、13.5MPa、14.0MPa、14.5MPa、15.0MPa、15.5MPa、16.0MPa、
16.5MPa、17.0MPa、17.5MPa、18.0MPa、18.5MPa、19.0MPa、19.5MPa、20.0MPa、20.5MPa、
21.0MPa、21.5MPa、22.0MPa、22.5MPa、23.0MPa、23.5MPa、24.0MPa、24.5MPa、25.0MPa、
25.5MPa, 26.0MPa, 26.5MPa, 27.0MPa, 27.5MPa, 28.0MPa, 28.5MPa, 29.0MPa, 29.5MPa are more than
30.0MPa。
In the present invention, the power pressure of the compressed air source should match with its bearing capacity, i.e., described compressed air
Highest power pressure in source reaches its bearing capacity.
In the present invention, the bearing capacity in the liquefied air source more than 5MPa, 5.5MPa, 6.0MPa, 6.5MPa,
7.0MPa、7.5MPa、8.0MPa、8.5MPa、9.0MPa、9.5MPa、10.0MPa、10.5MPa、11.0MPa、11.5MPa、
12.0MPa、12.5MPa、13.0MPa、13.5MPa、14.0MPa、14.5MPa、15.0MPa、15.5MPa、16.0MPa、
16.5MPa、17.0MPa、17.5MPa、18.0MPa、18.5MPa、19.0MPa、19.5MPa、20.0MPa、20.5MPa、
21.0MPa、21.5MPa、22.0MPa、22.5MPa、23.0MPa、23.5MPa、24.0MPa、24.5MPa、25.0MPa、
25.5MPa, 26.0MPa, 26.5MPa, 27.0MPa, 27.5MPa, 28.0MPa, 28.5MPa, 29.0MPa, 29.5MPa are more than
30.0MPa。
In the present invention, the power pressure in the liquefied air source should match with its bearing capacity, i.e., described liquefied air
Highest power pressure in source reaches its bearing capacity.
In the present invention, it is described centrifugation charging fluid passage bearing capacity more than 5MPa, 5.5MPa, 6.0MPa, 6.5MPa,
7.0MPa、7.5MPa、8.0MPa、8.5MPa、9.0MPa、9.5MPa、10.0MPa、10.5MPa、11.0MPa、11.5MPa、
12.0MPa、12.5MPa、13.0MPa、13.5MPa、14.0MPa、14.5MPa、15.0MPa、15.5MPa、16.0MPa、
16.5MPa、17.0MPa、17.5MPa、18.0MPa、18.5MPa、19.0MPa、19.5MPa、20.0MPa、20.5MPa、
21.0MPa、21.5MPa、22.0MPa、22.5MPa、23.0MPa、23.5MPa、24.0MPa、24.5MPa、25.0MPa、
25.5MPa, 26.0MPa, 26.5MPa, 27.0MPa, 27.5MPa, 28.0MPa, 28.5MPa, 29.0MPa, 29.5MPa are more than
30.0MPa。
In the present invention, it is described centrifugation charging fluid passage power pressure should match with its bearing capacity, i.e., it is described from
Highest power pressure in heart charging fluid passage reaches its bearing capacity.
In the present invention, when using the revolving combustor, the liquefied air source can be by swivel joint or using distant
Connected with the revolving combustor for form.
In the present invention, when using the revolving combustor, the compressed air source can be by swivel joint and the rotation
Turn combustion chamber.
In the present invention, when using the revolving combustor, and during including the cooling fluid source, the revolving combustor and
The cooling fluid source can use concentric bilayer swivel joint and communicating downstream；When downstream feed be liquid when, can use
Distant supplier's formula downstream feed.
In the present invention, so-called " distant supplier's formula " refers to non-contact liquid transmission form, for example, A uses distant confession form
It refers to A with B on the premise of in the absence of solid contact to be connected with B, the connection form that the fluid in A enters in B, including instills shape
Formula, inject form, penetrating form, suction form and spiral and pump into form etc., do not pump into connection form including centrifugation.
In the present invention, the purpose for setting the cooling duct is cold in order to be carried out to chamber wall and related heated portion
But, ensureing system stabilization working properly.
In the present invention, the purpose for setting the centrifugation charging fluid passage is the pressure in order to improve liquid before vaporization of being heated
Power.
In the present invention, the operation principle of the centrifugation charging fluid passage is identical with liquid centrifugal pump.
In the present invention, the centrifugation charging fluid passage is provided on the revolving combustor, in the rotation combustion
Burn under the centrifugal action produced by the rotation of room, Fluid pressure can be produced to increase effect and the pressure that the present invention is limited is increased to
The passage of power, for example, with the revolving combustor axial line as object of reference, being set to away from the revolving combustor direction of axis line
The fluid passage put.
In the present invention, the jet pipe can be with Laval nozzle.
In the present invention, when using the revolving combustor, the external outputting rotary power of revolving combustor.
In the present invention, when using the non-rotating combustion chamber, the jet pipe or the external outputting rotary power of the turbine.
In the present invention, should according to known technology to providing fuel in the non-rotating combustion chamber and the revolving combustor,
And igniter is set up when necessary.
In the present invention, necessary part, list should be set in necessary place according to heat energy and the known technology of dynamic field
Unit or system etc..
Beneficial effects of the present invention are as follows:
The velocity profile acting mechanism engine power density of the invention is high, and efficiency high, disposal of pollutants is few, and fuel is various
Property is good.
Brief description of the drawings
Fig. 1 is the structural representation of the embodiment of the present invention 1；
Fig. 2 is the structural representation of the embodiment of the present invention 2；
Fig. 3 is the structural representation of the embodiment of the present invention 3；
Fig. 4 is the structural representation of the embodiment of the present invention 4；
Fig. 5 is the structural representation of the embodiment of the present invention 5；
Fig. 6 is the structural representation of the embodiment of the present invention 6；
Fig. 7 is the structural representation of the embodiment of the present invention 7；
Fig. 8 is the structural representation of the embodiment of the present invention 8；
Fig. 9 is the structural representation of the embodiment of the present invention 9；
Figure 10 is the structural representation of the embodiment of the present invention 10；
Figure 11 is the structural representation of the embodiment of the present invention 11；
Figure 12 is the structural representation of the embodiment of the present invention 12；
Figure 13 is the structural representation of the embodiment of the present invention 13；
Figure 14 is the structural representation of the embodiment of the present invention 14；
Figure 15 is the structural representation of the embodiment of the present invention 15；
Figure 16 is the structural representation of the embodiment of the present invention 16；
Figure 17 is the structural representation of the embodiment of the present invention 17；
Figure 18 is the structural representation of the embodiment of the present invention 18；
Figure 19 is the structural representation of the embodiment of the present invention 19；
Figure 20 is the structural representation of the embodiment of the present invention 20；
Figure 21 is the structural representation of the embodiment of the present invention 21；
Figure 22 is the structural representation of the embodiment of the present invention 22；
Figure 23 is the structural representation of the embodiment of the present invention 23；
Figure 24 is the structural representation of the embodiment of the present invention 24；
Figure 25 is the structural representation of the embodiment of the present invention 25；
Figure 26 is the structural representation of the embodiment of the present invention 26；
Figure 27 is the structural representation of the embodiment of the present invention 27；
Figure 28 is the structural representation of the embodiment of the present invention 28；
Figure 29 is the structural representation of the embodiment of the present invention 29；
Figure 30 is the structural representation of the embodiment of the present invention 30；
Figure 31 is the structural representation of the embodiment of the present invention 31；
Figure 32 is the structural representation of the embodiment of the present invention 32；
Figure 33 is the structural representation of the embodiment of the present invention 33；
Figure 34 is the structural representation of the embodiment of the present invention 34.
Specific embodiment
Embodiment 1
Velocity profile acting mechanism engine as shown in Figure 1, including compressed air source 1, non-rotating combustion chamber 2 and jet pipe 3, institute
State compressed air source 1, the non-rotating combustion chamber 2 and the jet pipe 3 to be sequentially communicated, the bearing capacity of the compressed air source 1
More than 5MPa, cooling duct 201 is set on the wall of the non-rotating combustion chamber 2, the compressed air source 1 is through the cooling duct
201 connect with the non-rotating combustion chamber 2.
Embodiment 2
Velocity profile acting mechanism engine as shown in Figure 2, including compressed air source 1, non-rotating combustion chamber 2 and turbine 4,
The compressed air source 1, the non-rotating combustion chamber 2 and the turbine 4 are sequentially communicated, the pressure-bearing energy of the compressed air source 1
Power is more than 5MPa, and cooling duct 201 is set on the wall of the non-rotating combustion chamber 2, and the compressed air source 1 is logical through the cooling
Road 201 is connected with the non-rotating combustion chamber 2.
Embodiment 3
Velocity profile acting mechanism engine as shown in Figure 3, including compressed air source 1, non-rotating combustion chamber 2 and jet pipe 3,
The compressed air source 1, the non-rotating combustion chamber 2 and the jet pipe 3 are sequentially communicated, the pressure-bearing energy of the compressed air source 1
Power is more than 5MPa, and the velocity profile acting mechanism engine also includes cooling fluid source 5 and cooling fluid vaporizer jet pipe 31,
Cooling duct 201 is set on the wall of the non-rotating combustion chamber 2, the cooling fluid source 5 is connected with the cooling duct 201, institute
Cooling duct 201 is stated to be connected with the cooling fluid vaporizer jet pipe 31.
Embodiment 4
A kind of velocity profile acting mechanism engine as shown in Figure 4, including compressed air source 1, non-rotating combustion chamber 2 and thoroughly
Flat 4, the compressed air source 1, the non-rotating combustion chamber 2 and the turbine 4 are sequentially communicated, and the compressed air source 1 holds
Pressure energy power is more than 5MPa, and the velocity profile acting mechanism engine also includes cooling fluid source 5 and cooling fluid vaporizer turbine
41, cooling duct 201 is set on the wall of the non-rotating combustion chamber 2, the cooling fluid source 5 connects with the cooling duct 201
Logical, the cooling duct 201 connects with the cooling fluid vaporizer turbine 41.
Embodiment 5
Velocity profile acting mechanism engine as shown in Figure 5, including compressed air source 1, non-rotating combustion chamber 2 and jet pipe 3,
The compressed air source 1, the non-rotating combustion chamber 2 and the jet pipe 3 are sequentially communicated, the pressure-bearing energy of the compressed air source 1
Power is more than 5MPa, and the velocity profile acting mechanism engine also includes cooling fluid source 5, in the wall of the non-rotating combustion chamber 2
On set cooling duct 201, the cooling fluid source 5 is connected with the cooling duct 201, the cooling duct 201 and described non-
Revolving combustor 2 is connected.
Embodiment 6
Velocity profile acting mechanism engine as shown in Figure 6, including compressed air source 1, non-rotating combustion chamber 2 and turbine 4,
The compressed air source 1, the non-rotating combustion chamber 2 and the turbine 4 are sequentially communicated, the pressure-bearing energy of the compressed air source 1
Power is more than 5MPa, and the velocity profile acting mechanism engine also includes cooling fluid source 5, in the wall of the non-rotating combustion chamber 2
On set cooling duct 201, the cooling fluid source 5 is connected with the cooling duct 201, the cooling duct 201 and described non-
Revolving combustor 2 is connected.
Embodiment 7
Velocity profile acting mechanism engine as shown in Figure 7, including liquefied air source 11, non-rotating combustion chamber 2 and jet pipe
3, the liquefied air source 11, the non-rotating combustion chamber 2 and the jet pipe 3 are sequentially communicated, and the liquefied air source 11 is held
Pressure energy power is more than 5MPa.
Embodiment 8
Velocity profile acting mechanism engine as shown in Figure 8, including liquefied air source 11, non-rotating combustion chamber 2 and turbine
4, the liquefied air source 11, the non-rotating combustion chamber 2 and the turbine 4 are sequentially communicated, and the liquefied air source 11 is held
Pressure energy power is more than 5MPa.
Embodiment 9
Velocity profile acting mechanism engine as shown in Figure 9, on the basis of embodiment 7, in the non-rotating combustion chamber 2
Wall on set cooling duct 201, the liquefied air source 11 connects through the cooling duct 201 with the non-rotating combustion chamber 2.
Embodiment 10
Velocity profile acting mechanism engine as shown in Figure 10, on the basis of embodiment 8, in the non-rotating combustion chamber
Cooling duct 201 is set on 2 wall, the liquefied air source 11 connects through the cooling duct 201 and the non-rotating combustion chamber 2
It is logical.
Embodiment 11
Velocity profile acting mechanism engine as shown in figure 11, on the basis of embodiment 7, the velocity profile acting mechanism
Engine also includes cooling fluid source 5 and cooling fluid vaporizer jet pipe 31, and cooling is set on the wall of the non-rotating combustion chamber 2
Passage 201, the cooling fluid source 5 is connected with the cooling duct 201, the cooling duct 201 and the cooling fluid vapour
Compound jet pipe 31 is connected.
Embodiment 12
Velocity profile acting mechanism engine as shown in figure 12, on the basis of embodiment 8, the velocity profile acting mechanism
Engine also includes cooling fluid source 5 and cooling fluid vaporizer turbine 41, and cooling is set on the wall of the non-rotating combustion chamber 2
Passage 201, the cooling fluid source 5 is connected with the cooling duct 201, the cooling duct 201 and the cooling fluid vapour
Compound turbine 41 is connected.
Embodiment 13
Velocity profile acting mechanism engine as shown in fig. 13 that, on the basis of embodiment 7, the velocity profile does work mechanism
Engine also includes cooling fluid source 5, and cooling duct 201, the cooling fluid source are set on the wall of the non-rotating combustion chamber 2
5 connect with the cooling duct 201, and the cooling duct 201 connects with the non-rotating combustion chamber 2.
Embodiment 14
Velocity profile acting mechanism engine as shown in figure 14, on the basis of embodiment 8, the velocity profile acting mechanism
Engine also includes cooling fluid source 5, and cooling duct 201, the cooling fluid source are set on the wall of the non-rotating combustion chamber 2
5 connect with the cooling duct 201, and the cooling duct 201 connects with the non-rotating combustion chamber 2.
Embodiment 15
A kind of velocity profile acting mechanism engine as shown in figure 15, including compressed air source 1, revolving combustor 21 and spray
Pipe 3, the jet pipe 3 has square to set with the revolving combustor 21, the compressed air source 1, the revolving combustor 21 and institute
State jet pipe 3 to be sequentially communicated, the bearing capacity of the compressed air source 1 is more than 5MPa, is set on the wall of the revolving combustor 21
Cooling duct 201, the compressed air source 1 is connected through the cooling duct 201 with the revolving combustor 21.
Embodiment 16
Velocity profile acting mechanism engine as shown in figure 16, including compressed air source 1, revolving combustor 21 and turbine 4,
The compressed air source 1, the revolving combustor 21 and the turbine 4 are sequentially communicated, the bearing capacity of the compressed air source 1
More than 5MPa, cooling duct 201 is set on the wall of the revolving combustor 21, the compressed air source 1 is through the cooling duct
201 connect with the revolving combustor 21.
Embodiment 17
Velocity profile acting mechanism engine as shown in figure 17, including compressed air source 1, revolving combustor 21 and jet pipe 3,
The jet pipe 3 has square to set with the revolving combustor 21, the compressed air source 1, the revolving combustor 21 and the spray
Pipe 3 is sequentially communicated, and the bearing capacity of the compressed air source 1 is more than 5MPa, and the velocity profile acting mechanism engine also includes
Cooling fluid source 5 and cooling fluid vaporizer jet pipe 31, set cooling duct 201 on the wall of the revolving combustor 21, described
Cooling fluid source 5 is connected with the cooling duct 201, and the cooling duct 201 and the cooling fluid vaporizer jet pipe 31 connect
It is logical.
Embodiment 18
Velocity profile acting mechanism engine as shown in figure 18, including compressed air source 1, revolving combustor 21 and turbine 4,
The compressed air source 1, the revolving combustor 21 and the turbine 4 are sequentially communicated, the bearing capacity of the compressed air source 1
More than 5MPa, the velocity profile acting mechanism engine also includes cooling fluid source 5 and cooling fluid vaporizer turbine 41, in institute
Cooling duct 201 is set on the wall for stating revolving combustor 21, the cooling fluid source 5 is connected with the cooling duct 201, described cold
But passage 201 is connected with the cooling fluid vaporizer turbine 41.
Embodiment 19
Velocity profile acting mechanism engine as shown in figure 19, including compressed air source 1, revolving combustor 21 and jet pipe 3,
The jet pipe 3 has square to set with the revolving combustor 21, the compressed air source 1, the revolving combustor 21 and the spray
Pipe 3 is sequentially communicated, and the bearing capacity of the compressed air source 1 is more than 5MPa, and the velocity profile acting mechanism engine also includes
Cooling fluid source 5, sets cooling duct 201 on the wall of the revolving combustor 21, and the cooling fluid source 5 is logical with the cooling
Road 201 is connected, and the cooling duct 201 connects with the revolving combustor 21.
Embodiment 20
Velocity profile acting mechanism engine as shown in figure 20, including compressed air source 1, revolving combustor 21 and turbine 4,
The compressed air source 1, the revolving combustor 21 and the turbine 4 are sequentially communicated, the bearing capacity of the compressed air source 1
More than 5MPa, the velocity profile acting mechanism engine also includes cooling fluid source 5, is set on the wall of the revolving combustor 21
Cooling duct 201, the cooling fluid source 5 is connected with the cooling duct 201, and the cooling duct 201 and the rotation are fired
Room 21 is burnt to connect.
Embodiment 21
Velocity profile acting mechanism engine as shown in figure 21, including liquefied air source 11, revolving combustor 21 and jet pipe
3, the jet pipe 3 has square to set with the revolving combustor 21, the liquefied air source 11, the revolving combustor 21 and described
Jet pipe 3 is sequentially communicated, and the bearing capacity in the liquefied air source 11 is more than 5MPa, sets cold on the wall of the revolving combustor 21
But passage 201, the liquefied air source 11 connects through the cooling duct 201 with the revolving combustor 21.
Embodiment 22
Velocity profile acting mechanism engine as shown in figure 22, including liquefied air source 11, revolving combustor 21 and turbine
4, the liquefied air source 11, the revolving combustor 21 and the turbine 4 are sequentially communicated, the pressure-bearing in the liquefied air source 11
Ability is more than 5MPa.Cooling duct 201 is set on the wall of the revolving combustor 21, the liquefied air source 11 is through the cooling
Passage 201 is connected with the revolving combustor 21.
As disposable implementation method, it is also possible to which the cooling optionally removed on the wall of the revolving combustor 21 is led to
Road 201, i.e., described liquefied air source 11 directly connects with the revolving combustor 21.
Embodiment 23
Velocity profile acting mechanism engine as shown in figure 23, including liquefied air source 11, revolving combustor 21 and jet pipe
3, the jet pipe 3 has square to set with the revolving combustor 21, the liquefied air source 11, the revolving combustor 21 and described
Jet pipe 3 is sequentially communicated, and the bearing capacity in the liquefied air source 11 is more than 5MPa, and the velocity profile acting mechanism engine is also wrapped
Cooling fluid source 5 and cooling fluid vaporizer jet pipe 31 are included, cooling duct 201, institute are set on the wall of the revolving combustor 21
State cooling fluid source 5 to be connected with the cooling duct 201, the cooling duct 201 and the cooling fluid vaporizer jet pipe 31
Connection.
Embodiment 24
As of fig. 24 velocity profile acting mechanism engine, on the basis of embodiment 22, the velocity profile working machine
Structure engine also includes cooling fluid source 5 and cooling fluid vaporizer turbine 41, sets cold on the wall of the revolving combustor 21
But passage 201, the cooling fluid source 5 is connected with the cooling duct 201, the cooling duct 201 and the cooling fluid
Vaporizer turbine 41 is connected.
Embodiment 25
Velocity profile acting mechanism engine as shown in figure 25, including liquefied air source 11, revolving combustor 21 and jet pipe
3, the jet pipe 3 has square to set with the revolving combustor 21, the liquefied air source 11, the revolving combustor 21 and described
Jet pipe 3 is sequentially communicated, and the bearing capacity in the liquefied air source 11 is more than 5MPa, and the velocity profile acting mechanism engine is also wrapped
Cooling fluid source 5 is included, cooling duct 201, the cooling fluid source 5 and the cooling are set on the wall of the revolving combustor 21
Passage 201 is connected, and the cooling duct 201 connects with the revolving combustor 21.
Embodiment 26
Velocity profile acting mechanism engine as shown in figure 26, on the basis of embodiment 22, the velocity profile working machine
Structure engine also includes cooling fluid source 5, and cooling duct 201, the cooling fluid are set on the wall of the revolving combustor 21
Source 5 connects with the cooling duct 201, and the cooling duct 201 connects with the revolving combustor 21.
Embodiment 27
Velocity profile acting mechanism engine as shown in figure 27, including liquefied air source 11, revolving combustor 21, centrifugation increasing
Pressure fluid passage 6 and jet pipe 3, the jet pipe 3 has square to set with the revolving combustor 21, the liquefied air source 11, described
The centrifugation charging fluid passage 6, revolving combustor 21 and the jet pipe 3 are sequentially communicated, the centrifugation charging fluid passage 6
Bearing capacity is more than 5MPa.
Embodiment 28
Velocity profile acting mechanism engine as shown in figure 28, including liquefied air source 11, revolving combustor 21, centrifugation increasing
Pressure fluid passage 6 and turbine 4, the liquefied air source 11, the centrifugation charging fluid passage 6, and of the revolving combustor 21
The turbine 4 is sequentially communicated, and the bearing capacity of the centrifugation charging fluid passage 6 is more than 5MPa.
Embodiment 29
Velocity profile acting mechanism engine as shown in figure 29, on the basis of embodiment 27, in the revolving combustor
Cooling duct 201 is set on 21 wall, the liquefied air source 11 connects through the cooling duct 201 and the revolving combustor 21
It is logical.
Embodiment 30
Velocity profile acting mechanism engine as shown in figure 30, on the basis of embodiment 28, in the revolving combustor
Cooling duct 201 is set on 21 wall, the liquefied air source 11 connects through the cooling duct 201 and the revolving combustor 21
It is logical.
Embodiment 31
Velocity profile acting mechanism engine as shown in figure 31, on the basis of embodiment 27, the velocity profile working machine
Structure engine also includes cooling fluid source 5 and cooling fluid vaporizer jet pipe 31, sets cold on the wall of the revolving combustor 21
But passage 201, the cooling fluid source 5 is connected with the cooling duct 201, the cooling duct 201 and the cooling fluid
Vaporizer jet pipe 31 is connected.
Embodiment 32
Velocity profile acting mechanism engine as shown in figure 32, on the basis of embodiment 28, the velocity profile working machine
Structure engine also includes cooling fluid source 5 and cooling fluid vaporizer turbine 41, sets cold on the wall of the revolving combustor 21
But passage 201, the cooling fluid source 5 is connected with the cooling duct 201, the cooling duct 201 and the cooling fluid
Vaporizer turbine 41 is connected.
Embodiment 33
Velocity profile acting mechanism engine as shown in figure 33, on the basis of embodiment 27, the velocity profile working machine
Structure engine also includes cooling fluid source 5, and cooling duct 201, the cooling fluid are set on the wall of the revolving combustor 21
Source 5 connects with the cooling duct 201, and the cooling duct 201 connects with the revolving combustor 21.
Embodiment 34
Velocity profile acting mechanism engine as shown in figure 34, on the basis of embodiment 28, the velocity profile working machine
Structure engine also includes cooling fluid source 5, and cooling duct 201, the cooling fluid are set on the wall of the revolving combustor 21
Source 5 connects with the cooling duct 201, and the cooling duct 201 connects with the revolving combustor 21.
It is all in the present invention to be provided with the implementation method of the compressed air source, can be by the pressure-bearing of the compressed air source
Ability change be set to more than 5.5MPa, 6.0MPa, 6.5MPa, 7.0MPa, 7.5MPa, 8.0MPa, 8.5MPa, 9.0MPa, 9.5MPa,
10.0MPa、10.5MPa、11.0MPa、11.5MPa、12.0MPa、12.5MPa、13.0MPa、13.5MPa、14.0MPa、
14.5MPa、15.0MPa、15.5MPa、16.0MPa、16.5MPa、17.0MPa、17.5MPa、18.0MPa、18.5MPa、
19.0MPa、19.5MPa、20.0MPa、20.5MPa、21.0MPa、21.5MPa、22.0MPa、22.5MPa、23.0MPa、
23.5MPa、24.0MPa、24.5MPa、25.0MPa、25.5MPa、26.0MPa、26.5MPa、27.0MPa、27.5MPa、
28.0MPa, 28.5MPa, 29.0MPa, 29.5MPa or more than 30.0MPa.
It is all in the present invention to be provided with the implementation method in the liquefied air source, can be by the pressure-bearing in the liquefied air source
Ability change be set to more than 5.5MPa, 6.0MPa, 6.5MPa, 7.0MPa, 7.5MPa, 8.0MPa, 8.5MPa, 9.0MPa, 9.5MPa,
10.0MPa、10.5MPa、11.0MPa、11.5MPa、12.0MPa、12.5MPa、13.0MPa、13.5MPa、14.0MPa、
14.5MPa、15.0MPa、15.5MPa、16.0MPa、16.5MPa、17.0MPa、17.5MPa、18.0MPa、18.5MPa、
19.0MPa、19.5MPa、20.0MPa、20.5MPa、21.0MPa、21.5MPa、22.0MPa、22.5MPa、23.0MPa、
23.5MPa、24.0MPa、24.5MPa、25.0MPa、25.5MPa、26.0MPa、26.5MPa、27.0MPa、27.5MPa、
28.0MPa, 28.5MPa, 29.0MPa, 29.5MPa or more than 30.0MPa.
It is all in the present invention to be provided with the implementation method of the centrifugation charging fluid passage, can be by the centrifugation supercharging stream
The bearing capacity of body passage change be set to more than 5.5MPa, 6.0MPa, 6.5MPa, 7.0MPa, 7.5MPa, 8.0MPa, 8.5MPa,
9.0MPa、9.5MPa、10.0MPa、10.5MPa、11.0MPa、11.5MPa、12.0MPa、12.5MPa、13.0MPa、
13.5MPa、14.0MPa、14.5MPa、15.0MPa、15.5MPa、16.0MPa、16.5MPa、17.0MPa、17.5MPa、
18.0MPa、18.5MPa、19.0MPa、19.5MPa、20.0MPa、20.5MPa、21.0MPa、21.5MPa、22.0MPa、
22.5MPa、23.0MPa、23.5MPa、24.0MPa、24.5MPa、25.0MPa、25.5MPa、26.0MPa、26.5MPa、
27.0MPa, 27.5MPa, 28.0MPa, 28.5MPa, 29.0MPa, 29.5MPa or more than 30.0MPa.
It is clear that the invention is not restricted to above example, according to techniques known and technology disclosed in this invention
Scheme, can derive or association goes out many flexible programs, all these flexible programs, and it is protection model of the invention also to be regarded as
Enclose.
Claims (10)
1. a kind of velocity profile acting mechanism engine, including liquefied air source (11), non-rotating combustion chamber (2) and jet pipe (3), its
It is characterised by：The liquefied air source (11), the non-rotating combustion chamber (2) and the jet pipe (3) are sequentially communicated, the liquefaction
The bearing capacity of air-source (11) is more than 5MPa.
2. a kind of velocity profile acting mechanism engine, including liquefied air source (11), non-rotating combustion chamber (2) and turbine (4), its
It is characterised by：The liquefied air source (11), the non-rotating combustion chamber (2) and the turbine (4) are sequentially communicated, the liquefaction
The bearing capacity of air-source (11) is more than 5MPa.
3. velocity profile as claimed in claim 1 acting mechanism engine, it is characterised in that：The velocity profile acting mechanism engine
Also include cooling fluid source (5) and cooling fluid vaporizer jet pipe (31), cooling is set on the wall of the non-rotating combustion chamber (2)
Passage (201), the cooling fluid source (5) connects with the cooling duct (201), the cooling duct (201) and described cold
But fluid vaporization thing jet pipe (31) connection.
4. velocity profile as claimed in claim 2 acting mechanism engine, it is characterised in that：The velocity profile acting mechanism engine
Also include cooling fluid source (5) and cooling fluid vaporizer turbine (41), cooling is set on the wall of the non-rotating combustion chamber (2)
Passage (201), the cooling fluid source (5) connects with the cooling duct (201), the cooling duct (201) and described cold
But fluid vaporization thing turbine (41) connection.
5. a kind of velocity profile acting mechanism engine, including liquefied air source (11), revolving combustor (21) and jet pipe (3), its
It is characterised by：The jet pipe (3) has square to set with the revolving combustor (21), the liquefied air source (11), the rotation
Combustion chamber (21) and the jet pipe (3) are sequentially communicated, and the bearing capacity of the liquefied air source (11) is more than 5MPa, in the rotation
Cooling duct (201) is set on the wall for turning combustion chamber (21), the liquefied air source (11) is through the cooling duct (201) and described
Revolving combustor (21) is connected.
6. a kind of velocity profile acting mechanism engine, including liquefied air source (11), revolving combustor (21) and jet pipe (3), its
It is characterised by：The jet pipe (3) has square to set with the revolving combustor (21), the liquefied air source (11), the rotation
Combustion chamber (21) and the jet pipe (3) are sequentially communicated, and the bearing capacity of the liquefied air source (11) is more than 5MPa, the speed
Type acting mechanism engine also includes cooling fluid source (5) and cooling fluid vaporizer jet pipe (31), in the revolving combustor
(21) cooling duct (201) is set on wall, the cooling fluid source (5) connects with the cooling duct (201), the cooling is logical
Road (201) is connected with the cooling fluid vaporizer jet pipe (31).
7. a kind of velocity profile acting mechanism engine, including liquefied air source (11), revolving combustor (21) and jet pipe (3), its
It is characterised by：The jet pipe (3) has square to set with the revolving combustor (21), the liquefied air source (11), the rotation
Combustion chamber (21) and the jet pipe (3) are sequentially communicated, and the bearing capacity of the liquefied air source (11) is more than 5MPa, the speed
Type acting mechanism engine also includes cooling fluid source (5), and cooling duct is set on the wall of the revolving combustor (21)
(201), the cooling fluid source (5) is connected with the cooling duct (201), and the cooling duct (201) and the rotation are fired
Burn room (21) connection.
8. a kind of velocity profile acting mechanism engine, including liquefied air source (11), revolving combustor (21) and turbine (4), its
It is characterised by：The liquefied air source (11), the revolving combustor (21) and the turbine (4) are sequentially communicated, the liquefaction
The bearing capacity of air-source (11) is more than 5MPa.
9. a kind of velocity profile acting mechanism engine, including liquefied air source (11), revolving combustor (21), centrifugation charging fluid
Passage (6) and jet pipe (3), it is characterised in that：The jet pipe (3) has square to set with the revolving combustor (21), the liquefaction
Air-source (11), centrifugation charging fluid passage (6), the revolving combustor (21) and the jet pipe (3) are sequentially communicated, institute
The bearing capacity for stating centrifugation charging fluid passage (6) is more than 5MPa.
10. a kind of velocity profile acting mechanism engine, including liquefied air source (11), revolving combustor (21), centrifugation supercharging stream
Body passage (6) and turbine (4), it is characterised in that：The liquefied air source (11), centrifugation charging fluid passage (6), described
Revolving combustor (21) and the turbine (4) are sequentially communicated, and the bearing capacity of centrifugation charging fluid passage (6) is more than
5MPa。
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| CN201410240416.0A CN104214007A (en) | 2013-06-01 | 2014-05-30 | Velocity-type work-applying mechanism engine |
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