CN107023318A - A kind of method for generating power, precession turbine and its engine - Google Patents

A kind of method for generating power, precession turbine and its engine Download PDF

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Publication number
CN107023318A
CN107023318A CN201611203911.XA CN201611203911A CN107023318A CN 107023318 A CN107023318 A CN 107023318A CN 201611203911 A CN201611203911 A CN 201611203911A CN 107023318 A CN107023318 A CN 107023318A
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China
Prior art keywords
passage
rotary body
jet pipe
fluid
precession
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CN201611203911.XA
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Chinese (zh)
Inventor
靳北彪
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Entropy Zero Technology Logic Engineering Group Co Ltd
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Entropy Zero Technology Logic Engineering Group Co Ltd
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Publication of CN107023318A publication Critical patent/CN107023318A/en
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/32—Non-positive-displacement machines or engines, e.g. steam turbines with pressure velocity transformation exclusively in rotor, e.g. the rotor rotating under the influence of jets issuing from the rotor, e.g. Heron turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/005—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the engine comprising a rotor rotating under the actions of jets issuing from this rotor

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Hydraulic Turbines (AREA)

Abstract

The invention discloses a kind of precession turbine, including rotary body and jet pipe, passage is set on the rotary body, and the jet pipe has square to set with the passage and revolution connects setting, and the fluid of the jet pipe injection enters the passage and rotation or spiral rotating in the passage.The precession turbine and its engine structure of the invention is simple, cost is low.The invention discloses a kind of new method for generating power, and precession turbine disclosed in this invention and the engine including it are respectively provided with that simple in construction, cost is low and advantage of efficiency high.

Description

A kind of method for generating power, precession turbine and its engine
Technical field
The present invention relates to heat energy and dynamic field, more particularly to precession turbine, the invention further relates to apply the precession turbine Engine.
Background technology
Using fluid, for example, the gas that combustion chamber is provided, the turbine of acting is extremely important, still, many levels are generally required The energy of fluid effectively can be converted into power, so, complicated, cost is high, and heavy.Accordingly, it would be desirable to send out A kind of bright new type power production method, turbine and its 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 method for generating power, sprays fluid using stationary nozzle, the fluid is being arranged on rotary body On revolution passage in form rotating flow and/or spiral rotating stream, externally export power with the rotary body.
Scheme 2：A kind of method for generating power, rotates forward nozzle on body and sprays fluid, make the stream using being arranged on Body forms rotating flow and/or spiral rotating stream in the revolution passage being arranged on reverse rotation body, with the reverse rotation body And/or the body that rotates forward externally exports power.
Scheme 3：On the basis of scheme 1 or 2, further make the center of circle between the beginning and end of the spiral rotating stream Angle be more than 45 °, more than 50 °, more than 60 °, more than 70 °, more than 80 °, more than 90 °, more than 100 °, more than 110 °, more than 120 °, More than 130 °, more than 140 °, more than 150 °, more than 160 °, more than 170 °, more than 180 °, more than 190 °, more than 200 °, be more than 210 °, more than 220 °, more than 230 °, more than 240 °, more than 250 °, more than 260 °, more than 270 °, more than 280 °, more than 290 °, More than 300, more than 310 °, more than 320 °, more than 330 °, more than 340 °, more than 350 °, more than 360 °, more than 370 °, be more than 380 °, more than 390 °, more than 400, more than 410 °, more than 420 °, more than 430 °, more than 440 °, more than 450 °, more than 460 °, More than 470 °, more than 480 °, more than 490 °, more than 500 °, more than 510 °, more than 520 °, more than 530 °, more than 540 °, be more than 550 °, more than 560 °, more than 570 °, more than 580 °, more than 590 °, more than 600, more than 610 °, more than 620 °, more than 630 °, More than 640 °, more than 650 °, more than 660 °, more than 670 °, more than 680 °, more than 690 °, more than 700, more than 710 ° or it is more than 720°。
Scheme 4：A kind of precession turbine, including rotary body and jet pipe, set passage on the rotary body, the jet pipe with The passage has square to set and revolution connection setting, and the fluid of the jet pipe injection enters the passage and in the passage inward turning Turn and/or spiral rotating.
Scheme 5：On the basis of scheme 4, the fluid of the jet pipe injection is further set to be rotated in the passage inside spin Beginning and end between central angle be more than 45 °, more than 50 °, more than 60 °, more than 70 °, more than 80 °, more than 90 °, be more than 100 °, more than 110 °, more than 120 °, more than 130 °, more than 140 °, more than 150 °, more than 160 °, more than 170 °, more than 180 °, More than 190 °, more than 200 °, more than 210 °, more than 220 °, more than 230 °, more than 240 °, more than 250 °, more than 260 °, be more than 270 °, more than 280 °, more than 290 °, more than 300, more than 310 °, more than 320 °, more than 330 °, more than 340 °, more than 350 °, More than 360 °, more than 370 °, more than 380 °, more than 390 °, more than 400, more than 410 °, more than 420 °, more than 430 °, be more than 440 °, more than 450 °, more than 460 °, more than 470 °, more than 480 °, more than 490 °, more than 500 °, more than 510 °, more than 520 °, More than 530 °, more than 540 °, more than 550 °, more than 560 °, more than 570 °, more than 580 °, more than 590 °, more than 600, it is more than 610 °, more than 620 °, more than 630 °, more than 640 °, more than 650 °, more than 660 °, more than 670 °, more than 680 °, more than 690 °, More than 700, more than 710 ° or more than 720 °.
Scheme 6：A kind of precession turbine, including rotary body and jet pipe, set helical duct, the spiral shell on the rotary body Revolve the precession axis of passage to set with the axis non-colinear of the rotary body, the helical duct is connected with jet pipe revolution and set Put, the fluid of the jet pipe injection enters the helical duct.
Scheme 7：On the basis of scheme 6, further make the central angle between the entrance and exit of the helical duct big In 45 °, more than 50 °, more than 60 °, more than 70 °, more than 80 °, more than 90 °, more than 100 °, more than 110 °, more than 120 °, be more than 130 °, more than 140 °, more than 150 °, more than 160 °, more than 170 °, more than 180 °, more than 190 °, more than 200 °, more than 210 °, More than 220 °, more than 230 °, more than 240 °, more than 250 °, more than 260 °, more than 270 °, more than 280 °, more than 290 °, be more than 300th, more than 310 °, more than 320 °, more than 330 °, more than 340 °, more than 350 °, more than 360 °, more than 370 °, more than 380 °, More than 390 °, more than 400, more than 410 °, more than 420 °, more than 430 °, more than 440 °, more than 450 °, more than 460 °, be more than 470 °, more than 480 °, more than 490 °, more than 500 °, more than 510 °, more than 520 °, more than 530 °, more than 540 °, more than 550 °, More than 560 °, more than 570 °, more than 580 °, more than 590 °, more than 600, more than 610 °, more than 620 °, more than 630 °, be more than 640 °, more than 650 °, more than 660 °, more than 670 °, more than 680 °, more than 690 °, more than 700, more than 710 ° or more than 720 °.
Scheme 8：A kind of precession turbine, including rotary body, set axle stream helical duct, the axle stream on the rotary body The precession axis of helical duct and the axis non-colinear of the rotary body are set.
Scheme 9：On the basis of scheme 8, further make the center of circle between the entrance and exit of the axle stream helical duct Angle be more than 45 °, more than 50 °, more than 60 °, more than 70 °, more than 80 °, more than 90 °, more than 100 °, more than 110 °, more than 120 °, More than 130 °, more than 140 °, more than 150 °, more than 160 °, more than 170 °, more than 180 °, more than 190 °, more than 200 °, be more than 210 °, more than 220 °, more than 230 °, more than 240 °, more than 250 °, more than 260 °, more than 270 °, more than 280 °, more than 290 °, More than 300, more than 310 °, more than 320 °, more than 330 °, more than 340 °, more than 350 °, more than 360 °, more than 370 °, be more than 380 °, more than 390 °, more than 400, more than 410 °, more than 420 °, more than 430 °, more than 440 °, more than 450 °, more than 460 °, More than 470 °, more than 480 °, more than 490 °, more than 500 °, more than 510 °, more than 520 °, more than 530 °, more than 540 °, be more than 550 °, more than 560 °, more than 570 °, more than 580 °, more than 590 °, more than 600, more than 610 °, more than 620 °, more than 630 °, More than 640 °, more than 650 °, more than 660 °, more than 670 °, more than 680 °, more than 690 °, more than 700, more than 710 ° or it is more than 720°。
Scheme 10：The engine of precession turbine described in a kind of application scheme 4 or 5, the fluid intake and working medium of the jet pipe Source is connected.
Scheme 11：The engine of precession turbine described in a kind of application scheme 6 or 7, the fluid intake and working medium of the jet pipe Source is connected.
Scheme 12：A kind of engine of precession turbine described in application scheme 8 or 9, the fluid of the axle stream helical duct enters Mouth is connected with working medium source.
Scheme 13：In scheme 10 to 12 on the basis of either a program, the working medium source is further set to be set to combustion chamber, vapour Change device or be set to compressed gas source.
In the present invention, entered using the gyroscopic effect and the centrifugal action of rotary body produced by working medium rotation or spiral rotating And precession power is produced, so as to improve the level to working medium energy utilization.
In the present invention, so-called " jet pipe has square setting with the passage " refers to that the fluid of the jet pipe injection can Locus required for rotation or spiral rotating are formed in the passage sets relation.
In the present invention, so-called " A connects setting with B revolutions " refers to relatively rotate between A and B, and fluid is interconnected, and Non-co- axis sets relation.
In the present invention, so-called " revolution passage " refers to be arranged on the fluid passage beyond the center of rotation of tumbler, i.e., The overall fluid passage turned round according to tumbler axle center.
In the present invention, so-called " forward direction ", " reverse " only represent the difference of direction of rotation.
In the present invention, necessary part, list should be set in necessary place according to heat energy and the known technology of dynamic field Member or system etc..
Beneficial effects of the present invention are as follows:
The invention discloses a kind of new method for generating power, and precession turbine disclosed in this invention and the hair including it Motivation is respectively provided with that simple in construction, cost is low and advantage of efficiency high.
Brief description of the drawings
Fig. 1：The structural representation of the embodiment of the present invention 1；
Fig. 2：The structural representation of the embodiment of the present invention 2；
Fig. 3：The structural representation of the embodiment of the present invention 3；
Fig. 4：The structural representation of the embodiment of the present invention 4.
Embodiment
A kind of method for generating power of the present invention, sprays fluid using stationary nozzle, the fluid is being arranged on rotation Rotating flow and/or spiral rotating stream are formed in revolution passage on body, power is externally exported with the rotary body.
Another method for generating power of the present invention, rotates forward nozzle on body and sprays fluid, make institute using being arranged on State fluid and form rotating flow and/or spiral rotating stream in the revolution passage being arranged on reverse rotation body, with the reverse rotation Swivel and/or the body that rotates forward externally export power.
As disposable embodiment, preceding method further can optionally select to make the spiral rotating stream Central angle between beginning and end be more than 45 °, more than 50 °, more than 60 °, more than 70 °, more than 80 °, more than 90 °, be more than 100 °, more than 110 °, more than 120 °, more than 130 °, more than 140 °, more than 150 °, more than 160 °, more than 170 °, more than 180 °, More than 190 °, more than 200 °, more than 210 °, more than 220 °, more than 230 °, more than 240 °, more than 250 °, more than 260 °, be more than 270 °, more than 280 °, more than 290 °, more than 300, more than 310 °, more than 320 °, more than 330 °, more than 340 °, more than 350 °, More than 360 °, more than 370 °, more than 380 °, more than 390 °, more than 400, more than 410 °, more than 420 °, more than 430 °, be more than 440 °, more than 450 °, more than 460 °, more than 470 °, more than 480 °, more than 490 °, more than 500 °, more than 510 °, more than 520 °, More than 530 °, more than 540 °, more than 550 °, more than 560 °, more than 570 °, more than 580 °, more than 590 °, more than 600, it is more than 610 °, more than 620 °, more than 630 °, more than 640 °, more than 650 °, more than 660 °, more than 670 °, more than 680 °, more than 690 °, More than 700, more than 710 ° or more than 720 °.
Above-mentioned method for generating power is described further with reference to specific embodiments and the drawings：
Embodiment 1
A kind of precession turbine, as shown in figure 1, including rotary body 1 and jet pipe 2, passage 3, institute are set on the rotary body 1 Stating jet pipe 2 and the passage 3 has that square is set and revolution connect settings, the fluid of the injection of jet pipe 2 into the passage 3 and The inside spin of passage 3 rotation.
As disposable embodiment, the embodiment of the present invention 1 further can optionally make in the inside spin of passage 3 Rotation axis non-colinear and non-parallel setting of the precession axis of the fluid of rotation with the rotary body 1.
As disposable embodiment, spiral rotating described in the embodiment of the present invention 1, which is selectively chosen, is set to flaring Spiral rotating, the rotation of spiral flaring or non-flaring screw type rotary.
As disposable embodiment, the embodiment of the present invention 1 and its disposable embodiment also can be selected further Select to selecting property central angle of the fluid for spraying the jet pipe 2 between the beginning and end that the passage inside spin rotates big In 45 °, more than 50 °, more than 60 °, more than 70 °, more than 80 °, more than 90 °, more than 100 °, more than 110 °, more than 120 °, be more than 130 °, more than 140 °, more than 150 °, more than 160 °, more than 170 °, more than 180 °, more than 190 °, more than 200 °, more than 210 °, More than 220 °, more than 230 °, more than 240 °, more than 250 °, more than 260 °, more than 270 °, more than 280 °, more than 290 °, be more than 300th, more than 310 °, more than 320 °, more than 330 °, more than 340 °, more than 350 °, more than 360 °, more than 370 °, more than 380 °, More than 390 °, more than 400, more than 410 °, more than 420 °, more than 430 °, more than 440 °, more than 450 °, more than 460 °, be more than 470 °, more than 480 °, more than 490 °, more than 500 °, more than 510 °, more than 520 °, more than 530 °, more than 540 °, more than 550 °, More than 560 °, more than 570 °, more than 580 °, more than 590 °, more than 600, more than 610 °, more than 620 °, more than 630 °, be more than 640 °, more than 650 °, more than 660 °, more than 670 °, more than 680 °, more than 690 °, more than 700, more than 710 ° or more than 720 °.
Embodiment 2
A kind of precession turbine, as shown in Fig. 2 including rotary body 1 and jet pipe 2, passage 3, institute are set on the rotary body 1 Stating jet pipe 2 and the passage 3 has that square is set and revolution connect settings, the fluid of the injection of jet pipe 2 into the passage 3 and Rotated in the passage 3.
As disposable embodiment, the embodiment of the present invention 2 also further can optionally select to make to enter described logical The rotation axis non-colinear and non-parallel setting (not shown) of the rotation axis of fluid in road 3 and the rotary body 1.
Embodiment 3
A kind of precession turbine, as shown in figure 3, including rotary body 1 and jet pipe 2, helical duct is set on the rotary body 1 4, the precession axis of the helical duct 4 and the axis non-colinear of the rotary body 1 are set, the helical duct 4 and the spray The revolution connection of pipe 2 is set, and the fluid that the jet pipe 2 sprays enters the helical duct 4.
As disposable embodiment, spiral rotating described in the embodiment of the present invention 3, which is selectively chosen, is set to flaring Spiral rotating, the rotation of spiral flaring or non-flaring screw type rotary.
As disposable embodiment, the embodiment of the present invention 3 and its disposable embodiment can also be selected further Select to make the precession axis of the helical duct 4 and the axis non-colinear of the rotary body 1 and non-parallel setting to property.
As disposable embodiment, the embodiment of the present invention 3 and its disposable embodiment can be selected further Property select to make central angle between the entrance and exit of the helical duct be more than 45 °, more than 50 °, more than 60 °, be more than 70 °, more than 80 °, more than 90 °, more than 100 °, more than 110 °, more than 120 °, more than 130 °, more than 140 °, more than 150 °, it is big In 160 °, more than 170 °, more than 180 °, more than 190 °, more than 200 °, more than 210 °, more than 220 °, more than 230 °, be more than 240 °, more than 250 °, more than 260 °, more than 270 °, more than 280 °, more than 290 °, more than 300, more than 310 °, more than 320 °, More than 330 °, more than 340 °, more than 350 °, more than 360 °, more than 370 °, more than 380 °, more than 390 °, more than 400, it is more than 410 °, more than 420 °, more than 430 °, more than 440 °, more than 450 °, more than 460 °, more than 470 °, more than 480 °, more than 490 °, More than 500 °, more than 510 °, more than 520 °, more than 530 °, more than 540 °, more than 550 °, more than 560 °, more than 570 °, be more than 580 °, more than 590 °, more than 600, more than 610 °, more than 620 °, more than 630 °, more than 640 °, more than 650 °, more than 660 °, More than 670 °, more than 680 °, more than 690 °, more than 700, more than 710 ° or more than 720 °.
Embodiment 4
A kind of precession turbine, as shown in figure 4, including rotary body 1, axle stream helical duct, institute are set on the rotary body 1 The precession axis of axle stream helical duct is stated to set with the axis non-colinear of the rotary body 1.
As disposable embodiment, the embodiment of the present invention 4 also further can optionally select to make the axle stream spiral shell Revolve the precession axis of passage and the axis non-colinear of the rotary body 1 and non-parallel setting.
As disposable embodiment, the embodiment of the present invention 4 further can optionally select to make the axle stream spiral shell Revolve passage entrance and exit between central angle be more than 45 °, more than 50 °, more than 60 °, more than 70 °, more than 80 °, be more than 90 °, more than 100 °, more than 110 °, more than 120 °, more than 130 °, more than 140 °, more than 150 °, more than 160 °, more than 170 °, More than 180 °, more than 190 °, more than 200 °, more than 210 °, more than 220 °, more than 230 °, more than 240 °, more than 250 °, be more than 260 °, more than 270 °, more than 280 °, more than 290 °, more than 300, more than 310 °, more than 320 °, more than 330 °, more than 340 °, More than 350 °, more than 360 °, more than 370 °, more than 380 °, more than 390 °, more than 400, more than 410 °, more than 420 °, be more than 430 °, more than 440 °, more than 450 °, more than 460 °, more than 470 °, more than 480 °, more than 490 °, more than 500 °, more than 510 °, More than 520 °, more than 530 °, more than 540 °, more than 550 °, more than 560 °, more than 570 °, more than 580 °, more than 590 °, be more than 600th, more than 610 °, more than 620 °, more than 630 °, more than 640 °, more than 650 °, more than 660 °, more than 670 °, more than 680 °, More than 690 °, more than 700, more than 710 ° or more than 720 °.
Embodiment 5
A kind of engine of precession turbine described in Application Example 1, the fluid intake of the jet pipe 2 is connected with working medium source.
As disposable embodiment, the embodiment of the present invention 2 and embodiment 3 and its disposable embodiment and reality Applying precession turbine described in the disposable embodiment of example 1 can be with precession turbine described in alternate embodiment 5.
Embodiment 6
The engine of precession turbine described in a kind of Application Example 4, the fluid intake and working medium of the axle stream helical duct Source is connected.
As disposable embodiment, precession turbine described in the disposable embodiment of the embodiment of the present invention 4 Precession turbine described in alternate embodiment 6.
As disposable embodiment, described in the embodiment of the present invention 5 and embodiment 6 and its disposable embodiment Working medium source is set to combustion chamber, vaporizer or is set to compressed gas source.
It is clear that the invention is not restricted to above example, according to techniques known and technology disclosed in this invention Scheme, can be derived or association goes out many flexible programs, all these flexible programs, also be regarded as be the present invention protection model Enclose.

Claims (10)

1. a kind of method for generating power, it is characterised in that：Fluid is sprayed using stationary nozzle, the fluid is being arranged on rotation Rotating flow and/or spiral rotating stream are formed in revolution passage on body, power is externally exported with the rotary body.
2. a kind of method for generating power, it is characterised in that：The nozzle rotated forward using being arranged on body sprays fluid, makes described Fluid forms rotating flow and/or spiral rotating stream in the revolution passage being arranged on reverse rotation body, is reversely rotated with described Body and/or the body that rotates forward externally export power.
3. method for generating power as claimed in claim 1 or 2, it is characterised in that：The beginning and end of the spiral rotating stream it Between central angle be more than 45 °, more than 50 °, more than 60 °, more than 70 °, more than 80 °, more than 90 °, more than 100 °, more than 110 °, More than 120 °, more than 130 °, more than 140 °, more than 150 °, more than 160 °, more than 170 °, more than 180 °, more than 190 °, be more than 200 °, more than 210 °, more than 220 °, more than 230 °, more than 240 °, more than 250 °, more than 260 °, more than 270 °, more than 280 °, More than 290 °, more than 300, more than 310 °, more than 320 °, more than 330 °, more than 340 °, more than 350 °, more than 360 °, be more than 370 °, more than 380 °, more than 390 °, more than 400, more than 410 °, more than 420 °, more than 430 °, more than 440 °, more than 450 °, More than 460 °, more than 470 °, more than 480 °, more than 490 °, more than 500 °, more than 510 °, more than 520 °, more than 530 °, be more than 540 °, more than 550 °, more than 560 °, more than 570 °, more than 580 °, more than 590 °, more than 600, more than 610 °, more than 620 °, More than 630 °, more than 640 °, more than 650 °, more than 660 °, more than 670 °, more than 680 °, more than 690 °, more than 700, it is more than 710 ° or more than 720 °.
4. a kind of precession turbine, including rotary body (1) and jet pipe (2), it is characterised in that：Set on the rotary body (1) logical Road, the jet pipe (2) has square to set with the passage and revolution connects setting, and the fluid of jet pipe (2) injection enters described Passage and rotation and/or spiral rotating in the passage.
5. precession turbine as claimed in claim 4, it is characterised in that：The fluid of jet pipe (2) injection spiral shell in the passage Revolve rotation beginning and end between central angle be more than 45 °, more than 50 °, more than 60 °, more than 70 °, more than 80 °, be more than 90 °, more than 100 °, more than 110 °, more than 120 °, more than 130 °, more than 140 °, more than 150 °, more than 160 °, more than 170 °, More than 180 °, more than 190 °, more than 200 °, more than 210 °, more than 220 °, more than 230 °, more than 240 °, more than 250 °, be more than 260 °, more than 270 °, more than 280 °, more than 290 °, more than 300, more than 310 °, more than 320 °, more than 330 °, more than 340 °, More than 350 °, more than 360 °, more than 370 °, more than 380 °, more than 390 °, more than 400, more than 410 °, more than 420 °, be more than 430 °, more than 440 °, more than 450 °, more than 460 °, more than 470 °, more than 480 °, more than 490 °, more than 500 °, more than 510 °, More than 520 °, more than 530 °, more than 540 °, more than 550 °, more than 560 °, more than 570 °, more than 580 °, more than 590 °, be more than 600th, more than 610 °, more than 620 °, more than 630 °, more than 640 °, more than 650 °, more than 660 °, more than 670 °, more than 680 °, More than 690 °, more than 700, more than 710 ° or more than 720 °.
6. a kind of precession turbine, including rotary body (1) and jet pipe (2), it is characterised in that：Spiral shell is set on the rotary body (1) Passage is revolved, the precession axis of the helical duct and the axis non-colinear of the rotary body (1) are set, the helical duct and institute State jet pipe (2) revolution connection to set, the fluid of jet pipe (2) injection enters the helical duct.
7. precession turbine as claimed in claim 6, it is characterised in that：Central angle between the entrance and exit of the helical duct More than 45 °, more than 50 °, more than 60 °, more than 70 °, more than 80 °, more than 90 °, more than 100 °, more than 110 °, more than 120 °, it is big In 130 °, more than 140 °, more than 150 °, more than 160 °, more than 170 °, more than 180 °, more than 190 °, more than 200 °, be more than 210 °, more than 220 °, more than 230 °, more than 240 °, more than 250 °, more than 260 °, more than 270 °, more than 280 °, more than 290 °, More than 300, more than 310 °, more than 320 °, more than 330 °, more than 340 °, more than 350 °, more than 360 °, more than 370 °, be more than 380 °, more than 390 °, more than 400, more than 410 °, more than 420 °, more than 430 °, more than 440 °, more than 450 °, more than 460 °, More than 470 °, more than 480 °, more than 490 °, more than 500 °, more than 510 °, more than 520 °, more than 530 °, more than 540 °, be more than 550 °, more than 560 °, more than 570 °, more than 580 °, more than 590 °, more than 600, more than 610 °, more than 620 °, more than 630 °, More than 640 °, more than 650 °, more than 660 °, more than 670 °, more than 680 °, more than 690 °, more than 700, more than 710 ° or it is more than 720°。
8. a kind of precession turbine, including rotary body (1), it is characterised in that：Axle stream spiral is set to lead on the rotary body (1) Road, the precession axis of the axle stream helical duct is set with the axis non-colinear of the rotary body (1).
9. precession turbine as claimed in claim 8, it is characterised in that：Circle between the entrance and exit of the axle stream helical duct Heart angle be more than 45 °, more than 50 °, more than 60 °, more than 70 °, more than 80 °, more than 90 °, more than 100 °, more than 110 °, be more than 120 °, more than 130 °, more than 140 °, more than 150 °, more than 160 °, more than 170 °, more than 180 °, more than 190 °, more than 200 °, More than 210 °, more than 220 °, more than 230 °, more than 240 °, more than 250 °, more than 260 °, more than 270 °, more than 280 °, be more than 290 °, more than 300, more than 310 °, more than 320 °, more than 330 °, more than 340 °, more than 350 °, more than 360 °, more than 370 °, More than 380 °, more than 390 °, more than 400, more than 410 °, more than 420 °, more than 430 °, more than 440 °, more than 450 °, be more than 460 °, more than 470 °, more than 480 °, more than 490 °, more than 500 °, more than 510 °, more than 520 °, more than 530 °, more than 540 °, More than 550 °, more than 560 °, more than 570 °, more than 580 °, more than 590 °, more than 600, more than 610 °, more than 620 °, be more than 630 °, more than 640 °, more than 650 °, more than 660 °, more than 670 °, more than 680 °, more than 690 °, more than 700, more than 710 ° or More than 720 °.
10. the engine of precession turbine any one of a kind of application claim 4 to 7, it is characterised in that：The jet pipe (2) fluid intake is connected with working medium source.
CN201611203911.XA 2015-12-25 2016-12-23 A kind of method for generating power, precession turbine and its engine Pending CN107023318A (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
CN201510997446 2015-12-25
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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2544154A (en) * 1947-11-14 1951-03-06 Elmer N Hampton Tubular turbine
DE1088765B (en) * 1957-07-30 1960-09-08 Waldemar Kulikoff Dipl Ing Gas or steam turbine with propellant gas jet directed in a helical shape
CN1643260A (en) * 2002-01-25 2005-07-20 乔纳森·B·罗塞弗斯基 Ribbon drive power generation for variable flow conditions
CN201330619Y (en) * 2009-01-19 2009-10-21 杨仁金 Industrial exhaust heat steam and pneumatic helical engine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2544154A (en) * 1947-11-14 1951-03-06 Elmer N Hampton Tubular turbine
DE1088765B (en) * 1957-07-30 1960-09-08 Waldemar Kulikoff Dipl Ing Gas or steam turbine with propellant gas jet directed in a helical shape
CN1643260A (en) * 2002-01-25 2005-07-20 乔纳森·B·罗塞弗斯基 Ribbon drive power generation for variable flow conditions
CN201330619Y (en) * 2009-01-19 2009-10-21 杨仁金 Industrial exhaust heat steam and pneumatic helical engine

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Application publication date: 20170808