CN105480408B - Air generation plants - Google Patents
Air generation plants Download PDFInfo
- Publication number
- CN105480408B CN105480408B CN201610035401.XA CN201610035401A CN105480408B CN 105480408 B CN105480408 B CN 105480408B CN 201610035401 A CN201610035401 A CN 201610035401A CN 105480408 B CN105480408 B CN 105480408B
- Authority
- CN
- China
- Prior art keywords
- wing plate
- spiral
- screw rod
- spiral wing
- shell
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/001—Shrouded propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/16—Blades
- B64C11/18—Aerodynamic features
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/16—Blades
- B64C11/20—Constructional features
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C15/00—Attitude, flight direction, or altitude control by jet reaction
- B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
Abstract
A kind of air generation plants, including：Screw rod, the screw rod include shaft and the first spiral wing plate；Helical wing plate lantern ring, the helical wing plate lantern ring include tube body and the second spiral wing plate；Power input equipment, power input equipment and the screw rod power connector；The first spiral wing plate is arranged at intervals and is formed with the compression clearance for air compression with the second spiral wing plate；Blast injection mouth is offered on the twist collar.Based on said structure design, twist collar is sleeved on the outside of screw rod, twist collar and screw rod can form the positive and negative rotation of high speed, and compressed air assembles pressurization in twist collar, then spray to generate power at a high speed by the blast injection mouth opened up on twist collar.The present invention does not leak outside as power set, screw blade, and security is higher, small volume, and concealed be mounted in aircraft can be used so that aircraft keeps its streamlined flight of height more smoothly.
Description
Technical field
The present invention relates to technical field of power equipment, more specifically, more particularly to a kind of air generation plants.
Background technology
In the prior art, it is typically all using single screw or twin screw structure, spiral shell to commonly use propeller aero
Rotation paddle is arranged on the top of cockpit, and by driven by engine, its rotation generates power.
Propeller use open architecture, so there are the problem of be：1st, in flight course, the bird of airflight is easy
It bumps against on propeller, causes the accident；2nd, propeller generate power decentralized so that dynamical system it is less efficient.
The content of the invention
（One）Technical problem
Security when how to improve propeller aero flight and the service efficiency for improving propeller dynamical system,
Become those skilled in the art's urgent problem to be solved.
（Two）Technical solution
The present invention provides a kind of air generation plants, including：
Screw rod, the first spiral wing plate that the screw rod includes shaft and is arranged in the shaft, described
The first-class pitch auger in degree direction of one spiral wing plate along the shaft is set；
Twist collar, the twist collar include tube body and are arranged at the in vivo second spiral wing plate of the pipe, institute
The first-class pitch auger in degree direction for stating the second spiral wing plate along the tube body is set；
Power input equipment, the power input equipment are used to drive by transmission system with the screw rod power connector
The screw rod is rotated in the twist collar；
Wherein,
The screw rod is rotatablely arranged in the twist collar, the first spiral wing plate and second spiral
The hand of spiral of wing plate is on the contrary, the first spiral wing plate is arranged at intervals and is formed with for air with the second spiral wing plate
The compression clearance of compression；
The blast injection mouth sprayed for compressed air is offered on the twist collar.
Preferably, the first spiral wing plate is made of multi-disc wing plate unit, and whole wing plate units turns along described
The degree direction spiral of axis sets to form the first spiral wing plate；The second spiral wing plate is made of multi-disc wing plate unit, entirely
The degree direction spiral of the wing plate unit in portion along the shaft, which is set, to form the second spiral wing plate.
Preferably, present invention additionally comprises there is playpipe, the playpipe is arranged on the tube body, is opened on the playpipe
Equipped with blast injection mouth.
Preferably, the playpipe is integrally formed with the tube body.
Preferably, present invention additionally comprises have shell；The screw rod, which is arranged in the twist collar, forms dynamic list
Member；The power unit includes multiple, whole power unit axis and is set in parallel in the shell, described outer
Installing port is offered on shell, the blast injection mouth is oppositely arranged with the installing port, and the installing port is used to compress sky
The ejection of gas.
Preferably, whole power units is ordered in the shell.
（Three）Advantageous effect
Based on said structure design, twist collar is sleeved on the outside of screw rod, and twist collar and screw rod can be formed
The positive and negative rotation of high speed.When twist collar and the positive and negative high speed of screw rod rotate, the first spiral wing plate and the second spiral
Gap between wing plate can generate the pressurization phenomenon and simultaneous with the closing performance to fluid strongly that liquidates, and compressed air exists
Then aggregation pressurization in twist collar is sprayed at a high speed dynamic so as to generate by the blast injection mouth opened up on twist collar
Power.
For traditional propeller aero, by the use of the present invention as power set, screw blade does not leak outside, peace
Full property is higher.In addition, relative volume of the present invention is smaller, concealed be mounted in aircraft can be used so that aircraft keeps high
That spends is streamlined so that aircraft flight is more smoothly.
Description of the drawings
Fig. 1 is the structure diagram of screw rod in the embodiment of the present invention；
Fig. 2 is the structure diagram of twist collar in the embodiment of the present invention；
Fig. 3 is the structure diagram of air generation plants in the embodiment of the present invention；
Fig. 4 is the partial sectional view of air generation plants in the embodiment of the present invention；
Fig. 5 is that air generation plants is applied to the design sketch that dynamic air-flow is generated on aircraft in the embodiment of the present invention；
Component names and the correspondence of reference numeral are in Fig. 1 to Fig. 4：
Shaft 1, the first spiral wing plate 2, twist collar 3, playpipe 4,
Blast injection mouth 5, shell 6.
Specific embodiment
Embodiments of the present invention are described in further detail with reference to the accompanying drawings and examples.Following embodiment is used for
Illustrate the present invention, but cannot be used for limiting the scope of the invention.
In the description of the present invention, unless otherwise indicated, " multiple " are meant that two or more；Term " on ",
" under ", "left", "right", " interior ", " outer ", " front end ", " rear end ", " head ", the orientation of the instructions such as " afterbody " or position relationship be
Based on orientation shown in the drawings or position relationship, it is for only for ease of the description present invention and simplifies description rather than instruction or dark
Show that signified device or element there must be specific orientation, with specific azimuth configuration and operation, thus it is it is not intended that right
The limitation of the present invention.In addition, term " first ", " second ", " the 3rd " etc. be only used for description purpose, and it is not intended that instruction or
Imply relative importance.
In the description of the present invention, it is necessary to which explanation, unless otherwise clearly defined and limited, term " connected " " connects
Connect " it should be interpreted broadly, for example, it may be being fixedly connected or being detachably connected or be integrally connected；It can be machine
Tool is connected or is electrically connected；It can be directly connected, can also be indirectly connected by intermediary.For this field
For those of ordinary skill, the concrete meaning of above-mentioned term in the present invention can be understood with concrete condition.
It please refers to Fig.1 to Fig. 5, wherein, Fig. 1 is the structure diagram of screw rod in the embodiment of the present invention；Fig. 2 is the present invention
The structure diagram of twist collar in embodiment；Fig. 3 is the structure diagram of air generation plants in the embodiment of the present invention；Fig. 4
For the partial sectional view of air generation plants in the embodiment of the present invention；Fig. 5 is air generation plants application in the embodiment of the present invention
The design sketch of dynamic air-flow is generated on to aircraft.
The present invention provides a kind of air generation plants, which includes：Screw rod, screw rod include shaft 1
And the first spiral wing plate 2 in shaft 1 is arranged at, the first spiral wing plate 2 is set along the first-class pitch auger in degree direction of shaft 1
It puts；Twist collar 3, twist collar 3 include tube body and are arranged at the in vivo second spiral wing plate of pipe, the second spiral wing plate edge
The first-class pitch auger in degree direction of tube body is set；Power input equipment, power input equipment are moved by transmission system and screw rod
Power connects to drive screw rod in rotation in twist collar 3.Wherein, screw rod is rotatablely arranged in twist collar 3, the
The hand of spiral of one spiral wing plate 2 and the second spiral wing plate is on the contrary, the first spiral wing plate 2 and the second spiral wing plate are arranged at intervals simultaneously
It is formed with the compression clearance for air compression；The blast injection sprayed for compressed air is offered on twist collar 3
Mouth 5.
In said structure design,
The first spiral wing plate 2 is fixedly installed by techniques such as welding in shaft 1 using metal shaft as shaft 1 in screw rod.
Set a metal tube that the second spiral wing plate is fixedly installed by techniques such as welding in tube body as tube body.Screw rod is revolved
Turn to be nested into twist collar 3, by being cut out the second spiral wing plate so that screw rod can be in 3 inward turning of twist collar
Turn, and there is certain gap between the first spiral wing plate 2 and the second spiral wing plate, which is for compressed air
Compression clearance.
Based on said structure design, twist collar 3 is sleeved on the outside of screw rod, and twist collar 3 and screw rod being capable of shapes
Into the positive and negative rotation of high speed.When twist collar 3 and the positive and negative high speed of screw rod rotate, the first spiral wing plate 2 and second
Gap between spiral wing plate can generate the pressurization phenomenon and simultaneous with the closing performance to fluid strongly of liquidating, and compression is empty
Gas aggregation pressurization in the twist collar 3, is then sprayed at a high speed by the blast injection mouth 5 opened up on twist collar 3 thus
Generate power.
For traditional propeller aero, by the use of the present invention as power set, screw blade does not leak outside, peace
Full property is higher.In addition, relative volume of the present invention is smaller, concealed be mounted in aircraft can be used so that aircraft keeps high
That spends is streamlined so that aircraft flight is more smoothly.
In the present invention, power input equipment can be internal combustion engine or motor.
The present invention can generate larger inertia energy, and aircraft can generate huge drawing under inertia energy effect, push away
Power, effect be intended to front end can generate huge relative vacuum thus using body carry out float.
The application range of the present invention：
1st, it is meteorological without the comprehensive aircraft of propeller, hovering formula（Military radar is commanded）Platform, a variety of jet flights
The VTOL ancillary equipment of device, aerial wrecked preceding safety（It is additional）Compensate equipment, without propeller unmanned plane, rocket（Guided missile）
Air Launched Platform, especially big, the pneumatic rig for testing wind energy engine of large size, hurricane // cyclone tunnel test equipment.
2nd, big pressure fan, compressor, fluid convey pressurizer, fluid-mixing pressurizer, apart from fluid, mixed flow in pipe
In body pipe in pressurized equipment, pipeline // trapped orbit bullet train, the efficiently clean row // turbine of internal combustion engine // whirlpool set booster can be with
Energy-saving and emission-reduction.
Specifically, the first spiral wing plate 2 is made of multi-disc wing plate unit, degree direction of whole wing plate units along shaft 1
Spiral sets to form the first spiral wing plate 2；Second spiral wing plate is made of multi-disc wing plate unit, and whole wing plate units is along shaft
1 degree direction spiral sets to form the second spiral wing plate.First spiral wing plate 2 and the second spiral wing plate are designed as multiple wings
Plate unit is seamlessly connected between each wing plate unit.Certainly, the first spiral wing plate 2 and the second spiral wing plate can also use
Integrated formed structure.
In the present invention, air generation plants has further included playpipe 4, and playpipe 4 is arranged on tube body, on playpipe 4
Offer blast injection mouth 5.It is additional that playpipe 4 is set, by adjusting installation site of the playpipe 4 in tube body, established angle
The spatial position of degree adjustment blast injection mouth 5, consequently facilitating air generation plants is installed on adjustment in aircraft.
Specifically, playpipe 4 is integrally formed with tube body.
In the present invention, air generation plants has further included shell 6；Screw rod be arranged in twist collar 3 be formed with it is dynamic
Power unit；Power unit includes multiple, whole power unit axis and is set in parallel in shell 6, is offered on shell 6
Installing port, blast injection mouth 5 are oppositely arranged with installing port, and installing port is used for the ejection of compressed air；Whole power lists
Meta-rule is arranged in shell 6.
It should be noted that：The surface of the first spiral wing plate 2 and the second spiral wing plate passes through polishing in the present invention
Processing can so make its surface for smooth flexure plane, and guarantee gas is orderly, constant compression.
The embodiment of the present invention provides for the sake of example and description, and is not exhaustively or by this to send out
It is bright to be limited to disclosed form.Many modifications and variations are obvious for the ordinary skill in the art.Choosing
It is to more preferably illustrate the principle of the present invention and practical application to select and describe embodiment, and makes those of ordinary skill in the art
It will be appreciated that the present invention is so as to designing the various embodiments with various modifications suitable for special-purpose.
Claims (5)
1. a kind of air generation plants, which is characterized in that
Including：
Screw rod, the first spiral wing plate that the screw rod includes shaft and is arranged in the shaft, first spiral shell
The first-class pitch auger of length direction of rotor plate along the shaft is set；
Screw shell, the screw shell include tube body and are arranged at the in vivo second spiral wing plate of the pipe, and described
The first-class pitch auger of length direction of two spiral wing plate along the tube bodies is set；
Power input equipment, the power input equipment are described for driving by transmission system and the screw rod power connector
Screw rod is rotated in the screw shell；
Wherein,
The screw rod is rotatablely arranged in the screw shell, the first spiral wing plate and the second spiral wing plate
The hand of spiral on the contrary, the first spiral wing plate and the second spiral wing plate are arranged at intervals and are formed with for air compression
Compression clearance；
The blast injection mouth sprayed for compressed air is offered on the screw shell；
Shell is further included, the screw rod is arranged in the screw shell and is formed with power unit；The power unit bag
It has included multiple, whole power unit axis to be set in parallel in the shell, installing port is offered on the shell,
The blast injection mouth is oppositely arranged with the installing port, and the installing port is used for the ejection of compressed air.
2. air generation plants according to claim 1, which is characterized in that
The first spiral wing plate is made of multi-disc wing plate unit, length direction of whole wing plate units along the shaft
Spiral sets to form the first spiral wing plate；
The second spiral wing plate is made of multi-disc wing plate unit, length direction of whole wing plate units along the shaft
Spiral sets to form the second spiral wing plate.
3. air generation plants according to claim 1, which is characterized in that
Playpipe is further included, the playpipe is arranged on the tube body, and blast injection is offered on the playpipe
Mouthful.
4. air generation plants according to claim 3, which is characterized in that
The playpipe is integrally formed with the tube body.
5. air generation plants according to claim 1, which is characterized in that
Whole power units are ordered in the shell.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610035401.XA CN105480408B (en) | 2016-01-19 | 2016-01-19 | Air generation plants |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610035401.XA CN105480408B (en) | 2016-01-19 | 2016-01-19 | Air generation plants |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105480408A CN105480408A (en) | 2016-04-13 |
| CN105480408B true CN105480408B (en) | 2018-05-25 |
Family
ID=55667764
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610035401.XA Expired - Fee Related CN105480408B (en) | 2016-01-19 | 2016-01-19 | Air generation plants |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105480408B (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20000074653A (en) * | 1999-05-19 | 2000-12-15 | 김성흠 | Cohesive power utiltzation propeller |
| CN102233951A (en) * | 2010-04-28 | 2011-11-09 | 鄂雨松 | Flying disk engine |
| CN103318393A (en) * | 2012-03-23 | 2013-09-25 | 马勤荣 | Spiral pressure-guiding drive impeller of runner |
| CN203272132U (en) * | 2011-07-25 | 2013-11-06 | 复盛股份有限公司 | Water-spraying type double-helix air compressor |
| CN203876979U (en) * | 2014-05-25 | 2014-10-15 | 何长青 | Dish-shaped air lifting device |
| CN205499335U (en) * | 2016-01-19 | 2016-08-24 | 邱俊 | Air force device |
-
2016
- 2016-01-19 CN CN201610035401.XA patent/CN105480408B/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20000074653A (en) * | 1999-05-19 | 2000-12-15 | 김성흠 | Cohesive power utiltzation propeller |
| CN102233951A (en) * | 2010-04-28 | 2011-11-09 | 鄂雨松 | Flying disk engine |
| CN203272132U (en) * | 2011-07-25 | 2013-11-06 | 复盛股份有限公司 | Water-spraying type double-helix air compressor |
| CN103318393A (en) * | 2012-03-23 | 2013-09-25 | 马勤荣 | Spiral pressure-guiding drive impeller of runner |
| CN203876979U (en) * | 2014-05-25 | 2014-10-15 | 何长青 | Dish-shaped air lifting device |
| CN205499335U (en) * | 2016-01-19 | 2016-08-24 | 邱俊 | Air force device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105480408A (en) | 2016-04-13 |
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| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180525 Termination date: 20220119 |