CN108716474A - A kind of efficient hybrid power driven management device - Google Patents
A kind of efficient hybrid power driven management device Download PDFInfo
- Publication number
- CN108716474A CN108716474A CN201810493900.2A CN201810493900A CN108716474A CN 108716474 A CN108716474 A CN 108716474A CN 201810493900 A CN201810493900 A CN 201810493900A CN 108716474 A CN108716474 A CN 108716474A
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- China
- Prior art keywords
- cavity
- shaft
- sliding
- gear
- rotation
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/04—Units comprising pumps and their driving means the pump being fluid-driven
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/06—Units comprising pumps and their driving means the pump being electrically driven
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/06—Units comprising pumps and their driving means the pump being electrically driven
- F04D25/0673—Battery powered
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/08—Units comprising pumps and their driving means the working fluid being air, e.g. for ventilation
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/34—Blade mountings
- F04D29/36—Blade mountings adjustable
Abstract
The invention discloses a kind of efficient hybrid power driven management devices, including fuselage, it is arranged in the first cavity of the fuselage inner opening to the right and the second cavity in end wall on the left of the fuselage, the first sliding cavity of opening to the right is equipped in the first cavity left end wall, the first sliding shoe for being provided with left and right and extending that can be horizontally slipped in first sliding cavity, the first sliding shoe right end stretches into first cavity, the third cavity in first sliding shoe equipped with the first drive cavity and in end wall on the right side of first drive cavity；The device structure of the present invention is simple; it is easy to operate; it is realized using mechanical structure and drives handover management between wind energy and electric energy; storage management is carried out to fan blades using mechanical structure simultaneously; fan blades is protected, while fan blades angle is adjusted using mechanical structure, increases wind-force transfer efficiency; it cooperates and does not influence between each function, improve equipment practicability.
Description
Technical field
The present invention relates to hybrid power field, specifically a kind of efficient hybrid power driven management device.
Background technology
It is bad in the hollow flow of air of the large-scale confined space of workshop, warehouse etc., it is often necessary to which that air regenerating device is to room air
It swaps, conventional ventilation equipment is often using only a kind of driving ventilation fan in wind-force or electric power, conventional wind ventilation fan
Can not take a breath under no-wind environment, and simple electric power ventilation fan wastes electric energy, thus traditional equipment can not efficient ventilating, this device
Efficiently solve the problems, such as this.
Invention content
Technical problem to be solved by the invention is to provide a kind of efficient hybrid power driven management devices, can solve
The problems in above-mentioned present technology.
The present invention is achieved through the following technical solutions：A kind of efficient hybrid power driven management dress of the present invention
It sets, including fuselage, is arranged in the first cavity of the fuselage inner opening to the right and in end wall on the left of the fuselage
Two cavitys, the first cavity left end wall is interior to be equipped with the first sliding cavity of opening to the right, and cunning can be controlled in first sliding cavity
Dynamic the first sliding shoe for being provided with left and right and extending, the first sliding shoe right end stretches into first cavity, described
Third cavity in first sliding shoe equipped with the first drive cavity and in end wall on the right side of first drive cavity, described first
The first rotating shaft that left and right extends, the first rotating shaft left distal end are rotatably provided between drive cavity and the third cavity
It stretches into first drive cavity and is rotationally connected on the left of first drive cavity in end wall, the institute in first drive cavity
It states first rotating shaft outer surface and is installed with first bevel gear, the first rotating shaft right end stretches into the third cavity,
The first rotating shaft right end in the third cavity is installed with ratchet, and first drive cavity is equipped in lower face
The slot hole that left and right extends is equipped with the second drive cavity extended downwardly between first sliding cavity and second cavity, described
The rotation chamber through second drive cavity, the rotation intracavitary are provided with and communicated between first sliding cavity and second cavity
Rotatable to be provided with axle sleeve, the sleeve outer surface is installed with first pulley, and it is perforative to be equipped with left and right in the axle sleeve
First threaded hole, the first threaded hole screw-internal thread fit have the first threaded rod that left and right extends, the first threaded rod left side
End is stretched into second cavity, in the first threaded rod left distal end in second cavity and second cavity
The second sliding shoe right end face of sliding setting is fixedly connected, and the first threaded rod right end stretches into first sliding cavity
It is interior and be fixedly connected with the first sliding shoe left end face, the third transmission extended to the right is equipped with below second drive cavity
Chamber, the third transmission cavity roof is interior to be equipped with the second sliding cavity that Open Side Down, can horizontally slip in second sliding cavity
It is provided with the second sliding shoe, first motor is embedded in the second sliding shoe end face, the first motor main shaft extends downwardly
And bottom end outer surface be connected by power has first gear, and perforative second threaded hole in left and right is equipped in the second sliding shoe,
The second threaded hole screw-internal thread fit is connected with the second threaded rod that left and right extends, and second threaded rod extends into institute to the left
It states in the second drive cavity, the second threaded rod left distal end in second drive cavity is passed with being fixed at described second
The second motor power on the left of dynamic chamber in end wall connects, and the second screw thread rod outer surface in second drive cavity, which is fixed, to be connected
It is connected to the second belt wheel, second belt wheel is transmitted by belt with the first pulley and connected, the third transmission cavity and described the
The second shaft extended up and down is rotatably provided between one sliding cavity, the second shaft top end extends up through
The slot hole stretches into first drive cavity, and peace is fixed in the second shaft top end outer surface in first drive cavity
Equipped with the second bevel gear engaged with the first bevel gear, second shaft bottom extends down into the third transmission cavity
And distal outer surface is installed with second gear, the fuselage is equipped with device of solar generating, the solar power generation dress
It sets including solar panels and accumulator.
Preferably technical solution, the fuselage bottom are equipped with the 4th cavity that Open Side Down, the 4th cavity with
Rotation is provided with the third shaft extended up and down between the third transmission cavity, and the third shaft upwardly extends top end and turns
Dynamic to be connected in the third transmission cavity upper end wall, the third shaft top end outer surface in the third transmission cavity is solid
Dingan County is equipped with the third gear for being detached from cooperation with the first gear and being engaged with the second gear, and the third shaft is downward
Extend bottom end and is installed with turbofan, the permeability cell being evenly distributed in the 4th cavity end wall outside connection.
Preferably technical solution, the fuselage lower section are provided with rotation seat, are equipped in the rotation seat and run through up and down
The 5th cavity, the fuselage bottom, which extends downwardly, to be stretched into the 5th cavity and end and connects with the 5th cavity end wall rotation
It connects, the rotation seat upper surface is equipped with boss, and the boss outer surface is equipped with external toothing, can in the third transmission cavity lower end wall
Rotation is provided with the 4th shaft extended up and down, and the 4th shaft top end in the third transmission cavity is fixedly mounted
There are the 4th gear engaged with the first gear, the 4th shaft to extend downwardly bottom end and stretch out the external fuselage sky
Between, the 4th shaft bottom end in the exterior space is installed with the 5th gear engaged with the external toothing.
Preferably technical solution, the ratchet is interior to be equipped with flute profile chamber, and ratchet is equipped in the flute profile cavity wall, described
Flute profile intracavitary is rotatably provided with rotating disc, is fixedly connected with the 5th shaft in the rotating disc left end face, and the described 5th
Shaft outer surface is rotatably assorted the pawl being connected with the ratchet engagement, elastic connection between the pawl and the rotating disc
There is spring.
Preferably technical solution, the rotation of first sliding shoe outer surface are provided with pivoted housing, pivoted housing left side end
End is rotationally connected in the first cavity left end face, the 6th turn extended equipped with left and right in end wall on the right side of the third cavity
Axis, the 6th shaft left distal end stretch into the third cavity, end on the left of the 6th shaft in the third cavity
End is fixedly connected with the rotating disc, and the 6th shaft extends through to the right end wall on the right side of the third cavity and stretches into external sky
Between, the 6th shaft right end is fixedly connected with fan frame in the exterior space, the fan frame surrounding annular spread have with
The fan blades of the fan frame articulated connection, the fan blades left end face is interior to be equipped with sliding groove, is equipped in the sliding groove slidable
Third sliding shoe, the sliding shoe left end face are hingedly connected with the push rod extended to the left, the push rod left distal end with it is described
Pivoted housing is articulated and connected.
Perforative flange hole up and down is distributed in preferably technical solution, the rotation seat annular.
Preferably technical solution, is fixedly installed solar panels on the fuselage upper surface, roof on the fuselage
The interior accumulator being equipped with as motor power supply.
The beneficial effects of the invention are as follows：In the initial state, the first motor is electric with described second for the equipment of the present invention
Machine is in stationary state, and first sliding shoe is located at first sliding cavity rightmost side, the first bevel gear and second
Bevel gear engages, and the second sliding shoe is located at second sliding cavity leftmost side, the first gear and the 4th gear
Engagement.
When the ventilation of the equipment utilization wind energy of the present invention, start the first motor, the first motor rotation drives institute
It states first gear to rotate, the first gear rotation drives the 4th gear rotation, the 4th gear to rotate described in drive
5th gear rotates, and since the 5th gear is engaged with the external toothing, the 5th gear rotation drives the fuselage to turn
It is dynamic, when the fan blades is consistent with wind direction, the first motor is closed, the fan blades rotates under wind effect, and the fan blades turns
Dynamic that the fan frame is driven to rotate, the fan frame, which rotates, drives the first rotating shaft rotation, described in the first rotating shaft rotation drive
First bevel gear rotates, and the first bevel gear rotation drives the second bevel gear rotation, the second bevel gear to rotate band
The dynamic second gear rotation, the second gear rotation drive the third gear rotation, the third gear rotation to drive
Room air is pumped into the 5th cavity, is then excluded from the permeability cell by the turbofan rotation, the turbofan rotation.
When the ventilation of the equipment equipment utilization electric energy of the present invention, start the second motor rotation, second motor turns
It is dynamic that the rotation of the second threaded rod, the second threaded rod rotation is driven to drive the second belt wheel rotation, the second belt wheel rotation
The first pulley is driven to rotate, the first pulley rotation drives the axle sleeve rotation, and the axle sleeve rotation drives described the
One threaded rod moves to left, and first threaded rod, which moves to left, drives first sliding shoe to move to left, and first sliding shoe moves to left drive
The fan frame moves to left, and the fan frame, which moves to left, drives the fan blades to move to left, and the fan blades is turned over to the right under push rod effect at this time
Turn, the fan blades is received into first cavity, at the same time when second threaded rod rotation drives second sliding
Block moves to right, and the second sliding shoe, which moves to right, drives the first gear to move to right, when the first gear and the third gear are nibbled
When conjunction, second motor to be closed, starts the first motor, the first motor rotation drives the first gear rotation,
The first gear rotation drives the third gear rotation, the third gear rotation to drive the turbofan rotation by Interior Space
Gas is pumped into the 5th cavity, is then excluded from the permeability cell.
The device structure of the present invention is simple, easy to operate, is realized using mechanical structure and drives switching between wind energy and electric energy
Management, while storage management is carried out to fan blades using mechanical structure, fan blades is protected, while fan blades angle is adjusted using mechanical structure
Degree increases wind-force transfer efficiency, cooperates and do not influence between each function, improve equipment practicability.
Description of the drawings
The present invention is described in detail by following specific embodiment and attached drawing for ease of explanation,.
Fig. 1 is a kind of efficient hybrid power driven management device overall structure diagram of the present invention；
Fig. 2 is the structural schematic diagram of A in Fig. 1；
Fig. 3 is the structural schematic diagram of B in Fig. 1.
Specific implementation mode
As shown in Figure 1-Figure 3, a kind of efficient hybrid power driven management device of the invention, including fuselage 100, setting exist
The first cavity 136 of 100 inner opening of the fuselage to the right and the second cavity 104 in 100 left side end wall of the fuselage,
It is equipped with the first sliding cavity 142 of opening to the right in first cavity, 136 left end wall, can be controlled in first sliding cavity 142
The first sliding shoe 135 for being provided with left and right and extending of sliding, 135 right end of the first sliding shoe stretch into first cavity
The first drive cavity 137 is equipped in 136, in first sliding shoe 135 and in first drive cavity, 137 right side end wall
Third cavity 129, be rotatably provided between first drive cavity 137 and the third cavity 129 left and right extend
First rotating shaft 139,139 left distal end of the first rotating shaft stretch into first drive cavity 137 and are rotationally connected with described the
In one drive cavity, 137 left side end wall, 139 outer surface of the first rotating shaft in first drive cavity 137 is installed with
One bevel gear 141,139 right end of the first rotating shaft stretch into the third cavity 129, in the third cavity 129
139 right end of the first rotating shaft is installed with ratchet 124, and being equipped with left and right in 137 lower face of the first drive cavity prolongs
The slot hole 123 stretched is equipped with the second drive cavity extended downwardly between first sliding cavity 142 and second cavity 104
143, it is provided with and communicated between first sliding cavity 142 and second cavity 104 and turns through second drive cavity 143
Chamber 103 is moved, is rotatably provided with axle sleeve 101 in the rotation chamber 103,101 outer surface of the axle sleeve is installed with first
Belt wheel 144, the axle sleeve 101 is interior to be equipped with perforative first threaded hole 102 in left and right, 102 screw-internal thread fit of the first threaded hole
There is the first threaded rod 152 that left and right extends, 152 left distal end of the first threaded rod stretches into second cavity 104, described
Second sliding of 152 left distal end of the first threaded rod and sliding setting in second cavity 104 in the second cavity 104
145 right end face of block is fixedly connected, 152 right end of the first threaded rod stretch into first sliding cavity 142 and with institute
It states 135 left end face of the first sliding shoe to be fixedly connected, second drive cavity, 143 lower section is equipped with the third transmission cavity extended to the right
120,120 roof of third transmission cavity is interior to be equipped with the second sliding cavity 151 that Open Side Down, can in second sliding cavity 151
What is horizontally slipped is provided with the second sliding shoe 109, is embedded with first motor 111 in 109 end face of the second sliding shoe, and described
One motor, 111 main shaft extends downwardly and bottom end outer surface be connected by power has first gear 150, the second sliding shoe 109
Interior to be equipped with perforative second threaded hole 153 in left and right, 153 screw-internal thread fit of the second threaded hole is connected with second that left and right extends
Threaded rod 108, second threaded rod 108 are extended into the left in second drive cavity 143, in second drive cavity 143
108 left distal end of the second threaded rod and the second motor for being fixed in second drive cavity, 143 left side end wall
106 be connected by powers, 108 outer surface of the second threaded rod in second drive cavity 143 are fixedly connected with the second belt wheel
107, second belt wheel 107 and the first pulley 144 are transmitted by belt 105 and are connected, the third transmission cavity 120 with it is described
The second shaft 122 extended up and down, 122 top end of the second shaft are rotatably provided between first sliding cavity 142
It extends up through the slot hole 123 and stretches into first drive cavity 137, described second turn in first drive cavity 137
122 top end outer surface of axis is installed with the second bevel gear 140 engaged with the first bevel gear 141, and described second
122 bottom of shaft extends down into the third transmission cavity 120 and distal outer surface is installed with second gear 121, described
Fuselage 100 is equipped with device of solar generating, and the device of solar generating includes solar panels 201 and accumulator 200.
Valuably, 100 bottom of the fuselage is equipped with the 4th cavity 117 that Open Side Down, the 4th cavity 117 with it is described
Rotation is provided with the third shaft 114 extended up and down between third transmission cavity 120, and the third shaft 114 upwardly extends top
End is rotationally connected in 120 upper end wall of third transmission cavity, the third shaft 114 in the third transmission cavity 120
Top end outer surface is installed with for being detached from cooperation with the first gear 150 and engaging with the second gear 121
Three gears 119, the third shaft 114 extend downwardly bottom end and are installed with turbofan 116,117 end of the 4th cavity
The permeability cell 115 being evenly distributed in wall outside connection, convenient for equipment and exterior space air circulation.
Valuably, the lower section of the fuselage 100 is provided with rotation seat 113, and up and down perforative the is equipped in the rotation seat 113
Five cavitys 118,100 bottom of the fuselage, which extends downwardly, stretches into the 5th cavity 118 and end and 118 end of the 5th cavity
Wall is rotatablely connected, and 113 upper surface of the rotation seat is equipped with boss 149, and the boss outer surface is equipped with external toothing 148, and described the
The 4th shaft 112 extended up and down is rotatably provided in three transmission cavities, 120 lower end wall, in the third transmission cavity 120
4th shaft, 112 top end is installed with the 4th gear 110 engaged with the first gear 150, and the described 4th
Shaft 112 extends downwardly bottom end and stretches out 100 exterior space of fuselage, 112 bottom of the 4th shaft in the exterior space
End is installed with the 5th gear 147 engaged with the external toothing 148, is turned to convenient for the fuselage 100.
Valuably, it is equipped with flute profile chamber 130 in the ratchet 124, ratchet, the tooth are equipped in 130 inner wall of flute profile chamber
It is rotatably provided with rotating disc 126 in cavity 130, the 5th shaft is fixedly connected in 126 left end face of the rotating disc
154,154 outer surface of the 5th shaft be rotatably assorted be connected with the pawl of the ratchet engagement 155, the pawl 155 with
Spring 156 is elasticly connected between the rotating disc 126, convenient for controlling the turbofan one-directional rotation.
Valuably, 135 outer surface of the first sliding shoe rotation is provided with pivoted housing 138, and 138 left distal end of the pivoted housing turns
It is dynamic to be connected in 136 left end face of the first cavity, the left and right extends the 6th is equipped in 129 right side end wall of the third cavity
Shaft 128,128 left distal end of the 6th shaft stretch into the third cavity 129, described in the third cavity 129
6th shaft, 128 left distal end is fixedly connected with the rotating disc 126, and the 6th shaft 128 extends through to the right described
Three cavitys, 129 right side end wall stretches into exterior space, and 128 right end of the 6th shaft is fixedly connected in the exterior space
Frame 127 is fanned, the fan 127 surrounding annular spread of frame has the fan blades 134 being articulated and connected with the fan frame 127, the fan blades 134 left
It is equipped with sliding groove 133 in side end face, slidable third sliding shoe 131, the sliding shoe 131 are equipped in the sliding groove 133
Left end face is hingedly connected with the push rod 132 extended to the left, and 132 left distal end of the push rod is articulated and connected with the pivoted housing 138,
Convenient for carrying out shrink process to the fan blades.
Valuably, perforative flange hole 146 up and down is distributed in 113 annular of the rotation seat, convenient for the equipment of the present invention
Installation.
Valuably, it is fixedly installed solar panels 201 on 100 upper surface of the fuselage, is set in roof on the fuselage 100
The accumulator 200 of the promising motor power supply is converted to the sunlight when the solar panels 201 receive sunlight
Electric energy is stored in the accumulator 200, and the equipment uses altogether.
In the initial state, the first motor 111 is in static shape to the equipment of the present invention with second motor 106
State, first sliding shoe 135 are located at 142 rightmost side of the first sliding cavity, the first bevel gear 141 and second bevel gear
140 engagements, the second sliding shoe 109 are located at 151 leftmost side of the second sliding cavity, the first gear 150 and described the
Four gears 110 engage.
When the ventilation of the equipment utilization wind energy of the present invention, start the first motor 111, the first motor 111 rotates
The first gear 150 is driven to rotate, the rotation of the first gear 150 drives the 4th gear 110 rotation, the 4th tooth
110 rotation of wheel drives the 5th gear 147 rotation, described since the 5th gear 147 is engaged with the external toothing 148
The rotation of 5th gear 147 drives the fuselage 100 to rotate, and when the fan blades is consistent with wind direction, closes the first motor
111, the fan blades 134 rotates under wind effect, and the rotation of the fan blades 134 drives the fan frame 127 to rotate, the fan frame 127
Rotation drives the first rotating shaft 139 to rotate, and the rotation of the first rotating shaft 139 drives the first bevel gear 141 to rotate, described
The rotation of first bevel gear 141 drives the second bevel gear 140 to rotate, and the rotation of the second bevel gear 140 drives described second
Gear 121 rotates, and the rotation of the second gear 121 drives the third gear 119 to rotate, and the third gear 119 rotates band
The dynamic turbofan 116 rotates, and room air is pumped into the 5th cavity 118 by the rotation of the turbofan 116, then from described ventilative
Pipe 115 excludes.
When the ventilation of the equipment equipment utilization electric energy of the present invention, starts second motor 106 and rotate, second motor
106 rotations drive the rotation of the second threaded rod 108, the rotation of the second threaded rod 108 that second belt wheel 107 is driven to rotate, institute
Stating the rotation of the second belt wheel 107 drives the first pulley 144 to rotate, and the rotation of the first pulley 144 drives 101 turns of the axle sleeve
Dynamic, the rotation of the axle sleeve 101 drives first threaded rod 152 to move to left, and first threaded rod 152 moves to left drive described first
Sliding shoe 135 moves to left, and first sliding shoe 135, which moves to left, drives the fan frame 127 to move to left, and the fan frame 127, which moves to left, drives institute
It states fan blades 134 to move to left, the fan blades 134 is overturn to the right under the effect of the push rod 132 at this time, and the fan blades 134 is received into
At the same time first cavity 136 drives the second sliding shoe 109 to move to right when second threaded rod 108 rotates, described
The second sliding shoe 109, which moves to right, drives the first gear 150 to move to right, when the first gear 150 and the third gear 119 are nibbled
When conjunction, second motor 106 is closed, starts the first motor 111, the rotation of the first motor 111 drives described first
Gear 150 rotates, and the rotation of the first gear 150 drives the third gear 119 to rotate, and the third gear 119 rotates band
Room air is pumped into the 5th cavity 118 by the dynamic rotation of the turbofan 116, is then excluded from the permeability cell 115.
The beneficial effects of the invention are as follows：In the initial state, the first motor is electric with described second for the equipment of the present invention
Machine is in stationary state, and first sliding shoe is located at first sliding cavity rightmost side, the first bevel gear and second
Bevel gear engages, and the second sliding shoe is located at second sliding cavity leftmost side, the first gear and the 4th gear
Engagement.
When the ventilation of the equipment utilization wind energy of the present invention, start the first motor, the first motor rotation drives institute
It states first gear to rotate, the first gear rotation drives the 4th gear rotation, the 4th gear to rotate described in drive
5th gear rotates, and since the 5th gear is engaged with the external toothing, the 5th gear rotation drives the fuselage to turn
It is dynamic, when the fan blades is consistent with wind direction, the first motor is closed, the fan blades rotates under wind effect, and the fan blades turns
Dynamic that the fan frame is driven to rotate, the fan frame, which rotates, drives the first rotating shaft rotation, described in the first rotating shaft rotation drive
First bevel gear rotates, and the first bevel gear rotation drives the second bevel gear rotation, the second bevel gear to rotate band
The dynamic second gear rotation, the second gear rotation drive the third gear rotation, the third gear rotation to drive
Room air is pumped into the 5th cavity, is then excluded from the permeability cell by the turbofan rotation, the turbofan rotation.
When the ventilation of the equipment equipment utilization electric energy of the present invention, start the second motor rotation, second motor turns
It is dynamic that the rotation of the second threaded rod, the second threaded rod rotation is driven to drive the second belt wheel rotation, the second belt wheel rotation
The first pulley is driven to rotate, the first pulley rotation drives the axle sleeve rotation, and the axle sleeve rotation drives described the
One threaded rod moves to left, and first threaded rod, which moves to left, drives first sliding shoe to move to left, and first sliding shoe moves to left drive
The fan frame moves to left, and the fan frame, which moves to left, drives the fan blades to move to left, and the fan blades is turned over to the right under push rod effect at this time
Turn, the fan blades is received into first cavity, at the same time when second threaded rod rotation drives second sliding
Block moves to right, and the second sliding shoe, which moves to right, drives the first gear to move to right, when the first gear and the third gear are nibbled
When conjunction, second motor to be closed, starts the first motor, the first motor rotation drives the first gear rotation,
The first gear rotation drives the third gear rotation, the third gear rotation to drive the turbofan rotation by Interior Space
Gas is pumped into the 5th cavity, is then excluded from the permeability cell.
The device structure of the present invention is simple, easy to operate, is realized using mechanical structure and drives switching between wind energy and electric energy
Management, while storage management is carried out to fan blades using mechanical structure, fan blades is protected, while fan blades angle is adjusted using mechanical structure
Degree increases wind-force transfer efficiency, cooperates and do not influence between each function, improve equipment 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 domain should be determined by the scope of protection defined in the claims.
Claims (7)
1. the present invention a kind of efficient hybrid power driven management device, including fuselage, setting the fuselage inner opening to the right
The first cavity and the second cavity on the left of the fuselage in end wall, be equipped in the first cavity left end wall opening to
The first right sliding cavity, the first sliding shoe for being provided with left and right and extending that can be horizontally slipped in first sliding cavity, described the
One sliding shoe right end stretches into first cavity, the first drive cavity is equipped in first sliding shoe and positioned at described
Third cavity on the right side of first drive cavity in end wall, is rotatably provided between first drive cavity and the third cavity
The first rotating shaft that left and right extends, the first rotating shaft left distal end stretch into first drive cavity and are rotationally connected with described the
On the left of one drive cavity in end wall, the first rotating shaft outer surface in first drive cavity is installed with first bevel gear,
The first rotating shaft right end stretches into the third cavity, and the first rotating shaft right end in the third cavity is solid
Dingan County is equipped with ratchet, is equipped with the slot hole that left and right extends in first drive cavity lower face, first sliding cavity and described the
It is equipped with the second drive cavity extended downwardly between two cavitys, is provided with and communicated between first sliding cavity and second cavity
Through the rotation chamber of second drive cavity, the rotation intracavitary is rotatably provided with axle sleeve, and the sleeve outer surface is fixed
First pulley is installed, is equipped with perforative first threaded hole in left and right in the axle sleeve, the first threaded hole screw-internal thread fit has
The first threaded rod that left and right extends, the first threaded rod left distal end stretches into second cavity, in second cavity
The first threaded rod left distal end and second cavity in the second sliding shoe right end face of sliding setting be fixedly connected,
The first threaded rod right end is stretched into first sliding cavity and is fixedly connected with the first sliding shoe left end face,
It is equipped with the third transmission cavity extended to the right below second drive cavity, is equipped with what Open Side Down in the third transmission cavity roof
Second sliding cavity, what can be horizontally slipped in second sliding cavity is provided with the second sliding shoe, in the second sliding shoe end face
It is embedded with first motor, the first motor main shaft extends downwardly and bottom end outer surface be connected by power has first gear, institute
It states and is equipped with perforative second threaded hole in left and right in the second sliding shoe, the second threaded hole screw-internal thread fit is connected with left and right and extends
The second threaded rod, second threaded rod is extended into the left in second drive cavity, described in second drive cavity
Second threaded rod left distal end is connect with the second motor power being fixed in the end wall of the second drive cavity left side, described
The second screw thread rod outer surface in second drive cavity is fixedly connected with the second belt wheel, second belt wheel and the first band
Wheel is transmitted by belt and is connected, and the extended up and down is rotatably provided between the third transmission cavity and first sliding cavity
Two shafts, the second shaft top end extend up through the slot hole and stretch into first drive cavity, and described first passes
The second shaft top end outer surface of dynamic intracavitary is installed with the second bevel gear engaged with the first bevel gear,
Second shaft bottom extends down into the third transmission cavity and distal outer surface is installed with second gear, the machine
It is equipped with device of solar generating with it, the device of solar generating includes solar panels and accumulator.
2. a kind of efficient hybrid power driven management device according to claim 1, it is characterised in that：The fuselage bottom
Equipped with the 4th cavity that Open Side Down, between the 4th cavity and the third transmission cavity rotation be provided with the extended up and down
Three shafts, the third shaft upwardly extend top end and are rotationally connected in the third transmission cavity upper end wall, the third
The third shaft top end outer surface in transmission cavity be installed with the first gear be detached from cooperation and with it is described
The third gear of second gear engagement, the third shaft extend downwardly bottom end and are installed with turbofan, and the described 4th is empty
The permeability cell being evenly distributed in chamber end wall outside connection.
3. a kind of efficient hybrid power driven management device according to claim 1, it is characterised in that：Below the fuselage
Be provided with rotation seat, be equipped with upper and lower perforative 5th cavity in the rotation seat, the fuselage bottom extend downwardly stretch into it is described
5th cavity and end are rotatablely connected with the 5th cavity end wall, and the rotation seat upper surface is equipped with boss, outside the boss
Surface is equipped with external toothing, is rotatably provided with the 4th shaft extended up and down in the third transmission cavity lower end wall, and described the
The 4th shaft top end in three transmission cavities is installed with the 4th gear engaged with the first gear, and described
Four shafts extend downwardly bottom end and stretch out the external fuselage space, and the 4th shaft bottom end in the exterior space is fixed
The 5th gear engaged with the external toothing is installed.
4. a kind of efficient hybrid power driven management device according to claim 1, it is characterised in that：It is set in the ratchet
Cavity with teeth, the flute profile cavity wall is interior to be equipped with ratchet, and the flute profile intracavitary is rotatably provided with rotating disc, the rotating disc
The 5th shaft is fixedly connected in left end face, the 5th shaft outer surface, which is rotatably assorted, to be connected with and the ratchet engagement
Pawl is elasticly connected with spring between the pawl and the rotating disc.
5. a kind of efficient hybrid power driven management device according to claim 1, it is characterised in that：First sliding
The rotation of block outer surface is provided with pivoted housing, and the pivoted housing left distal end is rotationally connected in the first cavity left end face, described
The 6th shaft that left and right extends is equipped on the right side of third cavity in end wall, the 6th shaft left distal end stretches into the third cavity
Interior, the 6th shaft left distal end in the third cavity is fixedly connected with the rotating disc, and the 6th shaft is to the right
It extends through end wall on the right side of the third cavity and stretches into exterior space, the 6th shaft right end is solid in the exterior space
Surely it is connected with fan frame, the fan frame surrounding annular spread has the fan blades with the fan frame articulated connection, the fan blades left end face
It is interior to be equipped with sliding groove, it is equipped with slidable third sliding shoe in the sliding groove, the sliding shoe left end face is hingedly connected with
The push rod extended to the left, the push rod left distal end are articulated and connected with the pivoted housing.
6. a kind of efficient hybrid power driven management device according to claim 1, it is characterised in that：In the rotation seat
Annular spread has perforative flange hole up and down.
7. a kind of efficient hybrid power driven management device according to claim 1, it is characterised in that：The fuselage upper end
Solar panels are fixedly installed on face, roof is interior equipped with the accumulator powered for the motor on the fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810493900.2A CN108716474A (en) | 2018-05-22 | 2018-05-22 | A kind of efficient hybrid power driven management device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810493900.2A CN108716474A (en) | 2018-05-22 | 2018-05-22 | A kind of efficient hybrid power driven management device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108716474A true CN108716474A (en) | 2018-10-30 |
Family
ID=63900211
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810493900.2A Withdrawn CN108716474A (en) | 2018-05-22 | 2018-05-22 | A kind of efficient hybrid power driven management device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108716474A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110094349A (en) * | 2019-04-23 | 2019-08-06 | 天津盼香饰品有限公司 | One kind having humidification function usb desk fan |
| CN112572061A (en) * | 2020-12-21 | 2021-03-30 | 孔德杰 | Rubber composite pneumatic tire |
-
2018
- 2018-05-22 CN CN201810493900.2A patent/CN108716474A/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110094349A (en) * | 2019-04-23 | 2019-08-06 | 天津盼香饰品有限公司 | One kind having humidification function usb desk fan |
| CN110094349B (en) * | 2019-04-23 | 2020-04-10 | 温州市唐豪网络科技有限公司 | Desk fan with humidification function |
| CN112572061A (en) * | 2020-12-21 | 2021-03-30 | 孔德杰 | Rubber composite pneumatic tire |
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| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20181030 |
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| WW01 | Invention patent application withdrawn after publication |