CN106256992A - A kind of jet pipe inertia electromotor - Google Patents

A kind of jet pipe inertia electromotor Download PDF

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Publication number
CN106256992A
CN106256992A CN201610423866.2A CN201610423866A CN106256992A CN 106256992 A CN106256992 A CN 106256992A CN 201610423866 A CN201610423866 A CN 201610423866A CN 106256992 A CN106256992 A CN 106256992A
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CN
China
Prior art keywords
jet pipe
structure body
electromotor
rotational structure
inertia
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201610423866.2A
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Chinese (zh)
Inventor
靳北彪
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shangling Co Ltd
Original Assignee
Shangling Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shangling Co Ltd filed Critical Shangling Co Ltd
Publication of CN106256992A publication Critical patent/CN106256992A/en
Pending legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/32Non-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

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

The invention discloses a kind of jet pipe inertia electromotor, including rotational structure body and jet pipe, described jet pipe is arranged on described rotational structure body or described jet pipe and described rotational structure body integrated setting, and working medium his part non-of described jet pipe injection acts on described rotational structure body.Jet pipe inertia electromotor disclosed in this invention is not only simple in structure, and has efficiency height, pollutes little advantage.

Description

A kind of jet pipe inertia electromotor
Technical field
The present invention relates to heat energy and dynamic field, particularly relate to a kind of jet pipe inertia electromotor.
Background technology
Traditional combustion engine, gas turbine and steam turbine system structure are the most considerably complicated.It is thus desirable to invention one knot The simple new work engine of structure.
Summary of the invention
In order to solve the problems referred to above, the technical scheme that the present invention proposes is as follows:
Scheme 1: a kind of jet pipe inertia electromotor, including rotational structure body and jet pipe, described jet pipe is arranged on described rotation On structure or described jet pipe and described rotational structure body integrated setting, working medium his part non-of described jet pipe injection acts on institute State on rotational structure body.
Scheme 2: on the basis of scheme 1, makes the injection direction of described jet pipe and the footpath of described rotational structure body further Angle between to is more than or less than 90 °.
Scheme 3: on the basis of scheme 1 or 2, makes the injection direction of described jet pipe and described rotational structure body further The most identical, or the rotation axis of the injection direction described rotational structure body of sensing of described jet pipe, or the injection side of described jet pipe To pointing to the rotation axis away from described rotational structure body.
Scheme 4: in scheme 1 to 3 on the basis of either a program, makes working medium entrance and the working medium source of described jet pipe further Connection.
Scheme 5: on the basis of scheme 4, makes described working medium source can be set to combustor, carburator, compressed gas further Source or be set to mixed-burned gas liquefaction source.
Scheme 6: in scheme 1 to 5 on the basis of either a program, makes described jet pipe be set to Laval nozzle further.
In the present invention, fluid warp and the another one parts effect will ejected by the runner on a certain structure or jet pipe After, remake for described structure, i.e. movable vane runner working medium remakes for movable vane through stator blade, or stator blade runner working medium is through movable vane Remake for stator blade, or forward movable vane runner working medium remakes the conventional speed type hydraulic mechanism for forward movable vane through reverse movable vane Model of action be defined as his part effect, namely working medium flows in two different parts;
In the present invention, so-called " non-he part " refers to the model of action that working medium flows in parts, including through same The cyclogenesis of parts, steering-effecting and turning effect etc..
In the present invention, according to heat energy and the known technology of dynamic field, the parts of necessity, list should be set in necessary place Unit or system etc..
Inventors believe that, celestial body mutually moves and necessarily leads to gravitational interaction, and gravitational interaction necessarily leads to thing Mass flow is moved and/or object deformation, owing to material flowing and object deformation are irreversible process, is i.e. the mistake producing heat Journey, therefore the flowing of the material under gravitational field effect and object deformation necessarily lead to heat, and the heat that this form produces necessarily disappears The kinetic energy of consumption celestial body, As time goes on, through very long process, sky cognition gradually loses kinetic energy, and final sky is known from experience mutually Merging (or mutually phagocytosis), final universe forms a particle, and the temperature and pressure of this particle all can be ramping up, thus shape Violent blast (owing to temperature and pressure is ramping up also causing chemical reaction and nuclear reaction), blast is become to re-form celestial body Kinestate, even if celestial body has kinetic energy, forms mutual relative motion and interaction again between celestial body, enter the next one and follow Ring.It can be considered that the existence in universe is a thermodynamic cyclic process with development in fact.The essence of this process can letter It is summarised as " you invite me, and I am the most certain swallows you " singlely, understandable, it can be seen that, there is its final final result of main body of alternating action It is exactly mutually phagocytosis, mutually merges.
The present inventor thinks according to thermodynamic (al) ultimate principle and the observation to universe phenomenon: do not having external factor shadow On the premise of sound, heat can not absolutely be converted into other any type of energy or material.Conventional thermal mechanics second is fixed Rule only elaborating, heat can not absolutely be changed successfully, and this law is just on the premise of not having external factor impact True, but be unilateral.With popular language, heat can be defined as the minimum form of energy, or referred to as this is universe Rubbish.Through analyzing, the present inventor is additionally considered that: the growth course of any biology (animal, plant, microorganism, virus and antibacterial) It it is all heat release.Through analyzing, the present inventor is additionally considered that: any one process or any one circulation (are not limited to thermodynamics mistake Journey, such as chemical reaction process, biochemical reaction process, photochemical reaction process, biological growth process, growing process It is included) its maximum acting ability conservation, inventors believe that not having photosynthetic growing process is to carry Its acting ability high, say, that the acting ability of bean sprout is impossible to absorb plus it higher than the acting ability of bean or pea The acting ability sum of nutrient;Why the acting ability of one tree wood is greater than the acting ability of seedling, be because sunlight with Photosynthetic form take part in by the growth course of seedling to trees.
It is known that in economics, Nobel Prize was all authorized in the research to information asymmetry and information symmetrical, it is seen that Both parties have Determines transaction success or failure, the fairness of transaction and the profit of transaction of information.The essence of transaction is in fact Information trading.For inventors believe that, patent has information zero symmetry, i.e. both parties and the true value of patent is all known it The fewest.Patent information zero symmetric properties, if do not cracked, operation is difficulty with.Information zero symmetry of patent determines patent fortune The science of battalion and complexity.In general goods is concluded the business, information asymmetry may advantageously facilitate transaction, improves profit.And to specially For profit, the most entirely different, patent needs to solve technical problem, and the value of patent is quickly known in patent exploitation, so Patent must be out-and-out, and information zero is symmetrical and information asymmetry is inevitable all can seriously hinder patent operation, solves patent information Zero AXIALLY SYMMETRIC PROBLEMS, making both parties' information symmetrical on high level is that the basic of patent operation enterprise works.
Beneficial effects of the present invention is as follows: jet pipe inertia electromotor disclosed in this invention is not only simple in structure, and has Effective percentage is high, pollute little advantage.
Accompanying drawing explanation
The structural representation of Fig. 1: the embodiment of the present invention 1;
The structural representation of Fig. 2: the embodiment of the present invention 2;
The structural representation of Fig. 3: the embodiment of the present invention 3;
The structural representation of Fig. 4: the embodiment of the present invention 4;
The structural representation of Fig. 5: the embodiment of the present invention 5;
The structural representation of Fig. 6: the embodiment of the present invention 6;
The structural representation of Fig. 7: the embodiment of the present invention 7;
Fig. 8: working medium source is set to the structural representation of carburator;
In figure: 1 rotational structure body, 2 jet pipes, 3 working medium sources.
Detailed description of the invention
Embodiment 1
A kind of jet pipe inertia electromotor, as it is shown in figure 1, include rotational structure body 1 and jet pipe 2, described jet pipe 2 is arranged on institute State on rotational structure body 1 or described jet pipe 2 and described rotational structure body 1 integrated setting, the working medium of described jet pipe 2 injection non-he Part acts on described rotational structure body 1.
Embodiment 2
A kind of jet pipe inertia electromotor, as in figure 2 it is shown, on the basis of embodiment 1, make the spray of described jet pipe 2 further Penetrate the angle α between the radial direction of direction and described rotational structure body 1 more than 90 °.
Embodiment 3
A kind of jet pipe inertia electromotor, as it is shown on figure 3, on the basis of embodiment 1, make the spray of described jet pipe 2 further Penetrate the angle β between the radial direction of direction and described rotational structure body 1 less than 90 °
Embodiment 4
A kind of jet pipe inertia electromotor, as shown in Figure 4, on the basis of embodiment 1, makes the spray of described jet pipe 2 further Penetrate direction identical with the radial direction of described rotational structure body 1.
The injection direction of described jet pipe 2 all can be made further as disposable embodiment, embodiment 2 and embodiment 3 Identical with the radial direction of described rotational structure body 1.
Embodiment 5
A kind of jet pipe inertia electromotor, as it is shown in figure 5, on the basis of embodiment 1, make the spray of described jet pipe 2 further Penetrate direction and point to the rotation axis of described rotational structure body 1.
The injection direction of described jet pipe 2 all can be made further as disposable embodiment, embodiment 2 and embodiment 3 Point to the rotation axis of described rotational structure body 1.
Embodiment 6
A kind of jet pipe inertia electromotor, as shown in Figure 6, on the basis of embodiment 1, makes the spray of described jet pipe 2 further Penetrate direction and point to the rotation axis away from described rotational structure body 1.
The injection direction of described jet pipe 2 all can be made further as disposable embodiment, embodiment 2 and embodiment 3 Point to the rotation axis away from described rotational structure body 1.
Embodiment 7
A kind of jet pipe inertia electromotor, as it is shown in fig. 7, on the basis of embodiment 1, make the work of described jet pipe 2 further Matter entrance connects with working medium source 3.
All can enter as disposable embodiment, the embodiment of the present invention 2 to embodiment 6 and disposable embodiment thereof One step makes the working medium entrance of described jet pipe 2 connect with working medium source 3.
As disposable embodiment, all embodiments containing described working medium source of the present invention all can select further Property ground select make described working medium source 3 be set to combustor, carburator (as shown in Figure 8), compressed gas source or be set to mixed-burned gas liquefaction Source.
As disposable embodiment, all embodiments of the present invention all can make described jet pipe 2 be set to Bearing score further That jet pipe.
In the present invention, the O point in Figure of description represents the center of rotation of rotational structure body 1.
In the present invention, the injection direction that direction is described jet pipe 2 of arrow indication at jet pipe 2 in Figure of description.
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 also being regarded as is the protection model of the present invention Enclose.

Claims (9)

1. a jet pipe inertia electromotor, including rotational structure body (1) and jet pipe (2), it is characterised in that: described jet pipe (2) sets Put or described jet pipe (2) upper described rotational structure body (1) and described rotational structure body (1) integrated setting, described jet pipe (2) Working medium his part non-of injection acts on described rotational structure body (1).
2. jet pipe inertia electromotor as claimed in claim 1, it is characterised in that: the injection direction of described jet pipe (2) and described rotation Angle between the radial direction of rotation structure body (1) is more than or less than 90 °.
3. jet pipe inertia electromotor as claimed in claim 1, it is characterised in that: the injection direction of described jet pipe (2) and described rotation The radial direction of rotation structure body (1) is identical, or the injection direction of described jet pipe (2) points to the rotation axis of described rotational structure body (1), Or the injection direction of described jet pipe (2) points to the rotation axis away from described rotational structure body (1).
4. jet pipe inertia electromotor as claimed in claim 2, it is characterised in that: the injection direction of described jet pipe (2) and described rotation The radial direction of rotation structure body (1) is identical, or the injection direction of described jet pipe (2) points to the rotation axis of described rotational structure body (1), Or the injection direction of described jet pipe (2) points to the rotation axis away from described rotational structure body (1).
5. jet pipe inertia electromotor as according to any one of Claims 1-4, it is characterised in that: the working medium of described jet pipe (2) enters Mouth connects with working medium source (3).
6. jet pipe inertia electromotor as according to any one of Claims 1-4, it is characterised in that: described jet pipe (2) is set to Bearing score That jet pipe.
7. jet pipe inertia electromotor as claimed in claim 5, it is characterised in that: described jet pipe (2) is set to Laval nozzle.
8. jet pipe inertia electromotor as claimed in claim 5, it is characterised in that: described working medium source (3) is set to combustor, vaporization Device, compressed gas source or be set to mixed-burned gas liquefaction source.
9. jet pipe inertia electromotor as claimed in claim 7, it is characterised in that: described working medium source (3) is set to combustor, vaporization Device, compressed gas source or be set to mixed-burned gas liquefaction source.
CN201610423866.2A 2015-06-19 2016-06-15 A kind of jet pipe inertia electromotor Pending CN106256992A (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
CN2015103476194 2015-06-19
CN201510347619 2015-06-19
CN201510350790 2015-06-23
CN2015103507900 2015-06-23

Publications (1)

Publication Number Publication Date
CN106256992A true CN106256992A (en) 2016-12-28

Family

ID=57713629

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610423866.2A Pending CN106256992A (en) 2015-06-19 2016-06-15 A kind of jet pipe inertia electromotor

Country Status (1)

Country Link
CN (1) CN106256992A (en)

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Application publication date: 20161228