CN108999751A - A kind of multi-functional air accumulator formula turbine - Google Patents
A kind of multi-functional air accumulator formula turbine Download PDFInfo
- Publication number
- CN108999751A CN108999751A CN201810785318.3A CN201810785318A CN108999751A CN 108999751 A CN108999751 A CN 108999751A CN 201810785318 A CN201810785318 A CN 201810785318A CN 108999751 A CN108999751 A CN 108999751A
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- China
- Prior art keywords
- cavity
- rotation axis
- fuselage
- chamber
- worm gear
- 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.)
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D9/00—Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
- F03D9/20—Wind motors characterised by the driven apparatus
- F03D9/25—Wind motors characterised by the driven apparatus the apparatus being an electrical generator
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D15/00—Transmission of mechanical power
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D9/00—Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
- F03D9/20—Wind motors characterised by the driven apparatus
- F03D9/28—Wind motors characterised by the driven apparatus the apparatus being a pump or a compressor
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D9/00—Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
- F03D9/30—Wind motors specially adapted for installation in particular locations
- F03D9/32—Wind motors specially adapted for installation in particular locations on moving objects, e.g. vehicles
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/728—Onshore wind turbines
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/16—Mechanical energy storage, e.g. flywheels or pressurised fluids
Abstract
The invention discloses a kind of multi-functional air accumulator formula turbines, including fuselage and the first cavity extended up and down in the fuselage is set, the worm gear chamber that left and right extends is equipped on the right side of first cavity, worm gear chamber left end, which communicates, is equipped with the air inlet of extension and opening upwards up and down, the connecting cavity that left and right extends is symmetrically arranged on the right side of the worm gear chamber, the connecting cavity right end is equipped with the discharge chamber that right end end communicates with the outside world, the fuselage bottom end face is fixedly connected with the first rotation axis extended up and down, first rotation axis bottom end is rotatably assorted the fastening turntable of connection, the fastening turntable bottom end end face is fixedly connected with supporting table, the second cavity that left and right extends is equipped in the supporting table, the third cavity that front and back extends is equipped with above second cavity, the 4th cavity is symmetrically arranged at left and right sides of the third cavity；The configuration of the present invention is simple, it is easy to operate, be conducive to enhance wind-power electricity generation.
Description
Technical field
The present invention relates to wind power generation field, specifically a kind of multi-functional air accumulator formula turbine.
Background technique
The development of new energy has been trend of the times, and under the vigorously supporting of national policy, the sector has stepped into flourishing
Phase, wind-power electricity generation is as important one of new energy, and China has a good wind power foundation, but the existing tradition in China
Wind power plant wind power utilization rate is insufficient, causes wind power generation efficiency not high, so the appearance of the invention, can efficiently solve
This problem.
Summary of the invention
Technical problem to be solved by the invention is to provide a kind of multi-functional air accumulator formula turbines, are able to solve
The problems in above-mentioned present technology.
The present invention is achieved through the following technical solutions: a kind of multi-functional air accumulator formula turbine of the invention
Machine including fuselage and is arranged in the first cavity extended up and down in the fuselage, is equipped with left and right on the right side of first cavity and prolongs
The worm gear chamber stretched, worm gear chamber left end, which communicates, is equipped with the air inlet of extension and opening upwards up and down, right on the right side of the worm gear chamber
Claim to be equipped with the connecting cavity that left and right extends, the connecting cavity right end is equipped with the discharge chamber that right end end communicates with the outside world, the fuselage
Bottom end face is fixedly connected with the first rotation axis extended up and down, and the be rotatably assorted fastening of connection of first rotation axis bottom end turns
Disk, the fastening turntable bottom end end face are fixedly connected with supporting table, the second cavity that left and right extends, institute are equipped in the supporting table
It states and is equipped with the third cavity that front and back extends above the second cavity, be symmetrically arranged with the 4th cavity, institute at left and right sides of the third cavity
State and be embedded with first motor on rear side of third cavity in inner wall, first motor front-end of spindle end protrude into the third cavity and
It has been connected by power first bevel gear, has been rotatably assorted between the third cavity and the 4th cavity and is connected with left and right extends the
Two rotation axis, second rotation axis far from described 4th cavity one end end protrude into the third cavity and be fixedly connected with
The second bevel gear of the ratcheting connection of first bevel gear, second rotation axis protrude into described far from third cavity one end
4th cavity and it is equipped with third hand tap gear, be rotatably assorted in the 4th cavity third rotation axis for being connected with and extending up and down, institute
Third rotation axis is stated equipped with the 4th bevel gear with the ratcheting connection of the third hand tap gear, the third rotation axis bottom end
It is cooperatively connected through second cavity and with the supporting table lower rotation, is equipped in second cavity and turns with the third
Moving axis is threadedly engaged the top plate of connection, and the top plate bottom end face is symmetrically arranged with extension up and down and bottom end stretches out described second
Cavity and the fixed feet being slidably connected with supporting table, the fuselage left side is equipped with the 4th rotation axis that left and right extends, described
4th rotation axis left end end stretches out the fuselage and is equipped with propeller, and the 4th rotation axis right end end protrudes into described first
Cavity and be equipped with the first spur gear, the worm gear it is intracavitary be equipped with left and right extend the 5th rotation axis, the 5th rotation axis left end
End protrudes into first cavity and is equipped with the second spur gear with the ratcheting connection of the first spur gear, the 5th rotation axis
Right end protrudes into the discharge chamber and is rotatably assorted with the fuselage and connect, and the 5th rotation axis is fixedly connected with symmetrical
Worm gear, the discharge chamber bottom are embedded with fixed case, are equipped with generator, generator shaft left end end in the fixed case
It protrudes into the discharge chamber and is equipped with spiral fan, the fuselage roof end face is fixedly connected with the orientation axes extended up and down, described
Orientation axes are fixedly connected with the deflecting plate that left and right extends, and the fuselage top is rotatably assorted the support rod for being connected with and extending up and down,
The support bar top end is equipped with wind vane.
Preferably technical solution, discharge chamber right end end is equipped with mesh enclosure, to prevent having foreign matter when off working state
The electrical power generators are influenced into the discharge chamber.
Preferably technical solution, the front fuselage end face are equipped with wind-force display instrument, become to observe wind-force in real time
Change.
Preferably technical solution, the supporting table bottom end face are symmetrically arranged with wheel, are used for off working state fashionable dress
The movement set.
Preferably technical solution, the general illumination device include the fixation being arranged on box body right end end face
Block is equipped in the fixed block and connects electric chamber, it is described meet electric bottom of chamber portion and communicate be equipped with sliding slot, the company of being slidably matched in the sliding slot
Be connected to the distributing module extended up and down, put at the top of the distributing module it is described to connect electricity intracavitary, and electric contact is equipped on four end faces,
Driving motor is embedded in the sliding trench bottom inner wall, the driving motor top end is connected by power the spiral shell extended up and down
Rasp bar, the threaded rod are threadedly engaged with the distributing module and connect, described to connect electric chamber four inner walls opposite with the electric contact
Interior perforation is equipped with trolley pole, and the trolley pole stretches out outside the fixed block end face and is equipped with lampshade.
The beneficial effects of the present invention are: being embedded with first motor, the first motor in inner wall on rear side of the third cavity
Front end has been connected by power first bevel gear, and left and right extends second is equipped between the third cavity and the 4th cavity
Rotation axis, second rotation axis protrude into the third cavity far from described 4th cavity one end and are equipped with and the first cone tooth
The second bevel gear of ratcheting connection is taken turns, second rotation axis protrudes into the 4th cavity far from third cavity one end and sets
There is a third hand tap gear, is equipped with and extends up and down and top and the fastening turntable are rotatably assorted the third of connection in the 4th cavity
Rotation axis, the third rotation axis are equipped with the 4th bevel gear with the ratcheting connection of the third hand tap gear, the third rotation
Axis bottom end protrudes into second cavity and is rotatably assorted with second cavity bottom and connect, and is equipped in second cavity
The top plate of connection is threadedly engaged with the third rotation axis, the top plate bottom end face is symmetrically arranged with extension and bottom end up and down
The fixed feet for stretching out the supporting table is conducive to the fixation of device, makes its stable working.
The fuselage left end is equipped with the 4th rotation axis that left and right extends, and the machine is stretched out in the 4th rotation axis left end end
Body and be equipped with propeller, the 4th rotation axis right end end protrude into first cavity and be equipped with the first spur gear, the snail
Take turns it is intracavitary be equipped with left and right extend the 5th rotation axis, the 5th rotation axis left end end protrude into first cavity and be equipped with
The second bevel gear of the ratcheting connection of first bevel gear, the 5th rotation axis right end protrude into the discharge chamber and with the machine
Body is rotatably assorted connection, and the 5th rotation axis is symmetrically arranged with worm gear, and the discharge chamber bottom is embedded with fixed case, the fixation
Generator is equipped in case, generator left end end is fixedly connected with spiral fan, so wind-force drives the propeller to turn
It is dynamic, to drive the worm gear, makes the intracavitary wind-force enhancing of its worm gear, and then make its spiral fan quick rotation, improve wind-force benefit
With rate, enhance generating effect.
Device structure of the invention is simple, easy to operate, and by the way that fixed mechanism is arranged, Optimization Work environment can make its dress
The operation is stable is set, and uses the reasonable utilization to worm gear, improves the efficiency of device, is additionally equipped with corresponding auxiliary dress
It sets, improves the reliability of device, meanwhile, also improve device practicability.
Detailed description of the invention
The present invention is described in detail by following specific embodiments and drawings for ease of explanation,；
Fig. 1 is a kind of multi-functional air accumulator formula turbine interior overall structure diagram of the invention；
Fig. 2 is another working state schematic representation of a kind of multi-functional air accumulator formula turbine of the invention.
Specific embodiment
As depicted in figs. 1 and 2, a kind of multi-functional air accumulator formula turbine of the invention, including fuselage 130 and set
The first cavity 138 extended up and down in the fuselage 130 is set, the worm gear that left and right extends is equipped on the right side of first cavity 138
Chamber 135,135 left end of worm gear chamber, which communicates, is equipped with the air inlet 140 of extension and opening upwards up and down, and the worm gear chamber 135 is right
Side is symmetrically arranged with the connecting cavity 125 that left and right extends, and 125 right end of connecting cavity is equipped with the discharge chamber that right end end communicates with the outside world
129,130 bottom end face of fuselage is fixedly connected with the first rotation axis 123 extended up and down, 123 bottom of the first rotation axis
The fastening turntable 124 for the connection that is rotatably assorted is held, the 124 bottom end end face of fastening turntable is fixedly connected with supporting table 111, the branch
It supports and is equipped with the second cavity 110 that left and right extends in platform 111, the third cavity that front and back extends is equipped with above second cavity 110
122, the 4th cavity 106 is symmetrically arranged at left and right sides of the third cavity 122, is embedded in the 122 rear side inner wall of third cavity
There is first motor 117, the 117 front-end of spindle end of first motor protrudes into the third cavity 122 and has been connected by power first
Bevel gear 118 is rotatably assorted between the third cavity 122 and the 4th cavity 106 and is connected with second turn that left and right extends
Moving axis 115, second rotation axis 115 protrude into the third cavity 122 far from 106 one end end of the 4th cavity and fix
It is connected with the second bevel gear 116 with the ratcheting connection of the first bevel gear 118, second rotation axis 115 is far from described
Three cavitys, 122 one end protrudes into the 4th cavity 106 and is equipped with third hand tap gear 108, is rotatably assorted in the 4th cavity 106
It is connected with the third rotation axis 109 extended up and down, the third rotation axis 109 is equipped with ratcheting with the third hand tap gear 108
Connection the 4th bevel gear 107,109 bottom end of third rotation axis through second cavity 110 and with the support
111 lower rotation of platform is cooperatively connected, and is equipped in second cavity 110 and is threadedly engaged connection with the third rotation axis 109
Top plate 114,114 bottom end face of top plate be symmetrically arranged with extend up and down and bottom end stretch out second cavity 110 and with
The fixed feet 113 that supporting table 111 is slidably connected is equipped with the 4th rotation axis 104 that left and right extends on the left of the fuselage 130,
4th rotation axis, the 104 left end end stretches out the fuselage 130 and is equipped with propeller 105,104 right end of the 4th rotation axis
End protrudes into first cavity 138 and is equipped with the first spur gear 102, and the left and right extends the 5th is equipped in the worm gear chamber 135
Rotation axis 136, the 136 left end end of the 5th rotation axis are protruded into first cavity 138 and are equipped with and first spur gear
Second spur gear 103 of 102 ratcheting connections, 136 right end of the 5th rotation axis protrude into the discharge chamber 129 and with the fuselage
130 are rotatably assorted connection, and the 5th rotation axis 136 is fixedly connected with symmetrical worm gear 134,129 bottom of discharge chamber
Portion is embedded with fixed case 126, is equipped with generator 127 in the fixed case 126, the 127 main shaft left end end of generator is protruded into
The discharge chamber 129 and it is equipped with spiral fan 128,130 top end surface of fuselage is fixedly connected with the orientation axes extended up and down
133, the orientation axes 133 are fixedly connected with the deflecting plate 132 that left and right extends, and 130 top of fuselage, which is rotatably assorted, to be connected with
The support rod 101 extended up and down, 101 top end of support rod are equipped with wind vane 137.
Valuably, the 129 right end end of discharge chamber is equipped with mesh enclosure 139, to prevent there is foreign matter to enter institute when off working state
Stating discharge chamber 129 influences the power generation of generator 127.
Valuably, 130 front end surface of fuselage is equipped with wind-force display instrument 131, to observe wind-force variation in real time.
Valuably, 111 bottom end face of supporting table is symmetrically arranged with wheel 112, the shifting of device when for off working state
It is dynamic.
Valuably, the general illumination device includes the fixed block 204 being arranged on the 100 right end end face of box body, institute
State to be equipped in fixed block 204 and connect electric chamber 208, it is described connect electric 208 bottom of chamber and communicate be equipped with sliding slot 201, in the sliding slot 201
Be slidably connected with the distributing module 209 extended up and down, put at the top of the distributing module 209 it is described connect in electric chamber 208, and four
A end face is equipped with electric contact 203, is embedded with driving motor 200, the driving motor in sliding 201 bottom interior wall of slot
200 top ends are connected by power the threaded rod 202 extended up and down, and the threaded rod 202 is threadedly engaged with the distributing module 209
Connection, described connect in electric chamber 208 four inner walls opposite with the electric contact 203 penetrate through equipped with trolley pole 205, the trolley pole
205 stretch out outside 204 end face of fixed block and are equipped with lampshade 206.
Device is moved to level ground, starts the first motor 117 by equipment of the invention when standard works, because
First bevel gear 118, the third cavity 122 and the 4th sky have been connected by power for 117 front end of first motor
The second rotation axis 115 that left and right extends is equipped between chamber 106, second rotation axis 115 is far from described 4th cavity, 106 one end
It protrudes into the third cavity 122 and is equipped with the second bevel gear 116 with the ratcheting connection of the first bevel gear 118, described second
Rotation axis 115 protrudes into the 4th cavity 106 far from described 122 one end of third cavity and is equipped with third hand tap gear 108, and described the
It is equipped with and extends up and down and top and the fastening turntable 124 are rotatably assorted the third rotation axis 109 of connection, institute in four cavitys 106
Third rotation axis 109 is stated equipped with the 4th bevel gear 107 with the ratcheting connection of the third hand tap gear 108, the third rotation
109 bottom end of axis protrudes into second cavity 110 and is cooperatively connected with 120 lower rotation of the second cavity, and described second
The top plate 114 that connection is threadedly engaged with the third rotation axis 109 is equipped in cavity 110,114 bottom end face of top plate is symmetrical
Equipped with upper and lower extension and bottom end stretches out the fixed feet 113 of the supporting table 111, and the fixed feet 113 moves down
Earth's surface is put in, the device is fixed.
When being worked using equipment of the invention, it is primarily due to 130 top end surface of fuselage and is fixedly connected with
The orientation axes 133 of lower extension, the orientation axes 133 are fixedly connected with the deflecting plate 132 that left and right extends, and the orientation axes 133 are left
Side is equipped with the support rod 101 extended up and down, and 101 top end of support rod is equipped with wind vane 137,101 bottom of support rod
Portion protrudes into end in the fuselage 130 and is rotatably assorted with the fuselage 130 and connect, and 130 bottom end face of fuselage is fixed to be connected
It is connected to the first rotation axis 123 extended up and down, 123 bottom end of the first rotation axis is rotatably assorted the fastening turntable 124 of connection, institute
It states fastening 124 bottom end end face of turntable and is equipped with supporting table 111, so 130 front end face wind optimum orientation of fuselage described in the device,
Then again because 130 left end of fuselage is equipped with the 4th rotation axis 104 that left and right extends, 104 left end of the 4th rotation axis end
End stretches out the fuselage 130 and is equipped with propeller 105, and first cavity 138 is protruded into the 104 right end end of the 4th rotation axis
And it is equipped with the first spur gear 102, the 5th rotation axis 136 that left and right extends, the 5th rotation axis are equipped in the worm gear chamber 135
136 left ends end protrude into first cavity 138 and are equipped with the second bevel gear with the ratcheting connection of the first bevel gear 102
103,136 right end of the 5th rotation axis protrudes into the discharge chamber 129 and is rotatably assorted with the fuselage 130 and connect, and described
Five rotation axis 136 are symmetrically arranged with worm gear 134, and 129 bottom of discharge chamber is embedded with fixed case 126, sets in the fixed case 126
There is generator 127, the 127 left end end of generator is fixedly connected with spiral fan 128, so wind-force drives the propeller
105 rotations enhance wind-force in its worm gear chamber 135, and then turn its spiral fan 128 quickly to drive the worm gear 134
It is dynamic, enhance generating efficiency.
The beneficial effects of the present invention are: being embedded with first motor, the first motor in inner wall on rear side of the third cavity
Front end has been connected by power first bevel gear, and left and right extends second is equipped between the third cavity and the 4th cavity
Rotation axis, second rotation axis protrude into the third cavity far from described 4th cavity one end and are equipped with and the first cone tooth
The second bevel gear of ratcheting connection is taken turns, second rotation axis protrudes into the 4th cavity far from third cavity one end and sets
There is a third hand tap gear, is equipped with and extends up and down and top and the fastening turntable are rotatably assorted the third of connection in the 4th cavity
Rotation axis, the third rotation axis are equipped with the 4th bevel gear with the ratcheting connection of the third hand tap gear, the third rotation
Axis bottom end protrudes into second cavity and is rotatably assorted with second cavity bottom and connect, and is equipped in second cavity
The top plate of connection is threadedly engaged with the third rotation axis, the top plate bottom end face is symmetrically arranged with extension and bottom end up and down
The fixed feet for stretching out the supporting table is conducive to the fixation of device, makes its stable working.
The fuselage left end is equipped with the 4th rotation axis that left and right extends, and the machine is stretched out in the 4th rotation axis left end end
Body and be equipped with propeller, the 4th rotation axis right end end protrude into first cavity and be equipped with the first spur gear, the snail
Take turns it is intracavitary be equipped with left and right extend the 5th rotation axis, the 5th rotation axis left end end protrude into first cavity and be equipped with
The second bevel gear of the ratcheting connection of first bevel gear, the 5th rotation axis right end protrude into the discharge chamber and with the machine
Body is rotatably assorted connection, and the 5th rotation axis is symmetrically arranged with worm gear, and the discharge chamber bottom is embedded with fixed case, the fixation
Generator is equipped in case, generator left end end is fixedly connected with spiral fan, so wind-force drives the propeller to turn
It is dynamic, to drive the worm gear, makes the intracavitary wind-force enhancing of its worm gear, and then make its spiral fan quick rotation, improve wind-force benefit
With rate, enhance generating effect.
Device structure of the invention is simple, easy to operate, and by the way that fixed mechanism is arranged, Optimization Work environment can make its dress
The operation is stable is set, and uses the reasonable utilization to worm gear, improves the efficiency of device, is additionally equipped with corresponding auxiliary dress
It sets, improves the reliability of device, meanwhile, also improve device practicability.
The above description is merely a specific embodiment, but scope of protection of the present invention is not limited thereto, any
The change or replacement expected without creative work, should be covered by the protection scope of the present invention.Therefore, of the invention
Protection scope should be determined by the scope of protection defined in the claims.
Claims (5)
1. including fuselage and the first of extension up and down is arranged in the fuselage in a kind of multi-functional air accumulator formula turbine
Cavity, it is characterised in that: the worm gear chamber that left and right extends is equipped on the right side of first cavity, worm gear chamber left end is communicated equipped with upper
The air inlet of lower extension and opening upwards, the worm gear chamber right side are symmetrically arranged with the connecting cavity that left and right extends, and the connecting cavity is right
End is equipped with the discharge chamber that right end end communicates with the outside world, and the fuselage bottom end face is fixedly connected with the first rotation extended up and down
Axis, first rotation axis bottom end are rotatably assorted the fastening turntable of connection, and the fastening turntable bottom end end face is fixedly connected with branch
Platform is supportted, the second cavity that left and right extends is equipped in the supporting table, it is empty that the third that front and back extends is equipped with above second cavity
Chamber, the third cavity left and right sides are symmetrically arranged with the 4th cavity, are embedded with first motor in inner wall on rear side of the third cavity,
First motor front-end of spindle end protrudes into the third cavity and has been connected by power first bevel gear, the third cavity with
It is rotatably assorted between 4th cavity and is connected with the second rotation axis that left and right extends, second rotation axis is far from the described 4th
Cavity one end end protrudes into the third cavity and is fixedly connected with the second bevel gear with the ratcheting connection of the first bevel gear,
Second rotation axis protrudes into the 4th cavity far from third cavity one end and is equipped with third hand tap gear, and the described 4th is empty
The intracavitary third rotation axis for being connected with and extending up and down that is rotatably assorted, the third rotation axis are equipped with and the third hand tap gear tooth
The 4th bevel gear of connection is closed, the third rotation axis bottom end turns through second cavity and with the supporting table bottom
It is dynamic to be cooperatively connected, the top plate that connection is threadedly engaged with the third rotation axis, the top plate bottom are equipped in second cavity
End surface symmetric is equipped with extension and bottom end up and down and stretches out second cavity and the fixed feet with supporting table sliding connection,
The 4th rotation axis that left and right extends is equipped on the left of the fuselage, the 4th rotation axis left end end is stretched out the fuselage and is equipped with
Propeller, the 4th rotation axis right end end protrude into first cavity and are equipped with the first spur gear, and the worm gear is intracavitary to be set
The 5th rotation axis for having left and right to extend, the 5th rotation axis left end end are protruded into first cavity and are equipped with and described first
Second spur gear of the ratcheting connection of spur gear, the 5th rotation axis right end protrude into the discharge chamber and match with fuselage rotation
Connection is closed, the 5th rotation axis is fixedly connected with symmetrical worm gear, and the discharge chamber bottom is embedded with fixed case, described
Generator is equipped in fixed case, generator shaft left end end protrudes into the discharge chamber and is equipped with spiral fan, the machine
Body top end surface is fixedly connected with the orientation axes extended up and down, and the orientation axes are fixedly connected with the deflecting plate that left and right extends, institute
It states fuselage top to be rotatably assorted the support rod for being connected with and extending up and down, the support bar top end is equipped with wind vane.
2. a kind of multi-functional air accumulator formula turbine according to claim 1, it is characterised in that: the discharge chamber is right
It holds end to be equipped with mesh enclosure, influences the electrical power generators to prevent there is foreign matter to enter the discharge chamber when off working state.
3. a kind of multi-functional air accumulator formula turbine according to claim 1, it is characterised in that: the front fuselage
End face is equipped with wind-force display instrument, to observe wind-force variation in real time.
4. a kind of multi-functional air accumulator formula turbine according to claim 1, it is characterised in that: the supporting table bottom
End surface is symmetrically arranged with wheel, the movement of device when for off working state.
5. a kind of multi-functional air accumulator formula turbine according to claim 1, it is characterised in that: the general illumination
Device includes the fixed block being arranged on box body right end end face, is equipped in the fixed block and connects electric chamber, described to connect electric bottom of chamber
Portion, which communicates, is equipped with sliding slot, and the distributing module extended up and down is slidably connected in the sliding slot, is stretched at the top of the distributing module
To connect electricity intracavitary into described, and electric contact is equipped on four end faces, is embedded with driving motor in the sliding trench bottom inner wall, institute
It states driving motor top end and is connected by power the threaded rod extended up and down, the threaded rod and the distributing module are threadedly engaged company
It connects, described connect is penetrated through in electric chamber four inner walls opposite with the electric contact equipped with trolley pole, and the trolley pole stretches out described solid
Determine outside block end face and is equipped with lampshade.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810785318.3A CN108999751A (en) | 2018-07-17 | 2018-07-17 | A kind of multi-functional air accumulator formula turbine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810785318.3A CN108999751A (en) | 2018-07-17 | 2018-07-17 | A kind of multi-functional air accumulator formula turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108999751A true CN108999751A (en) | 2018-12-14 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810785318.3A Withdrawn CN108999751A (en) | 2018-07-17 | 2018-07-17 | A kind of multi-functional air accumulator formula turbine |
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| CN (1) | CN108999751A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109795315A (en) * | 2019-03-08 | 2019-05-24 | 安徽能通新能源科技有限公司 | A kind of pure electric vehicle emergency break down lorry |
-
2018
- 2018-07-17 CN CN201810785318.3A patent/CN108999751A/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109795315A (en) * | 2019-03-08 | 2019-05-24 | 安徽能通新能源科技有限公司 | A kind of pure electric vehicle emergency break down lorry |
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