CN108583179A - A kind of energy saving and environment friendly medical unmanned plane - Google Patents
A kind of energy saving and environment friendly medical unmanned plane Download PDFInfo
- Publication number
- CN108583179A CN108583179A CN201810275278.8A CN201810275278A CN108583179A CN 108583179 A CN108583179 A CN 108583179A CN 201810275278 A CN201810275278 A CN 201810275278A CN 108583179 A CN108583179 A CN 108583179A
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- Prior art keywords
- gear
- fuselage
- dead axle
- main shaft
- cylinder
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D55/00—Endless track vehicles
- B62D55/06—Endless track vehicles with tracks without ground wheels
- B62D55/075—Tracked vehicles for ascending or descending stairs, steep slopes or vertical surfaces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D55/00—Endless track vehicles
- B62D55/08—Endless track units; Parts thereof
- B62D55/18—Tracks
- B62D55/24—Tracks of continuously flexible type, e.g. rubber belts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D55/00—Endless track vehicles
- B62D55/08—Endless track units; Parts thereof
- B62D55/30—Track-tensioning means
-
- 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
- B64C11/02—Hub construction
- B64C11/04—Blade mountings
- B64C11/06—Blade mountings for variable-pitch blades
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- Engineering & Computer Science (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mixers Of The Rotary Stirring Type (AREA)
Abstract
The invention discloses a kind of energy saving and environment friendly medical unmanned planes, including fuselage, the fuselage is equipped with propeller set, the propeller set includes main shaft, adjustment axis, blade, the main axis is set on fuselage, the main shaft is hollow structure, it is arranged with adjustment axis in the main shaft, the main shaft madial wall upper edge is axially arranged with guide groove, the adjustment axis lateral wall is equipped with the gib block that sliding is matched with the guide groove in an axial direction, it is uniformly distributed on the main shaft lateral wall that there are three blade connecting rods, there are one blades for rotation connection respectively on each blade connecting rod, it is uniformly distributed on the lateral wall of the adjustment axis that there are three struts.The propeller set of the present invention drives the axial position of adjustment axis by the first cylinder by driving release handle, and to drive the second adjusting rod that the inclination angle of blade is adjusted, regulatory function is easy to use, simple in structure, and reliability is high, and service life is long.
Description
Technical field
The present invention relates to air vehicle technique fields, and in particular to a kind of energy saving and environment friendly medical unmanned plane.
Background technology
Currently, the structure for adjusting blade angle in the propeller set of unmanned helicopter, which exists, designs unreasonable, use
The problem of short life；Existing liquid medicine mixing device structure design is unreasonable, and liquid mixed effect is undesirable；It is existing that nobody is straight
Do not have the hub unit that can conveniently travel on land on the machine of liter, needs to improve.
Invention content
(1) technical problems to be solved
The technical problem to be solved in the present invention is to provide a kind of energy saving and environment friendly medical unmanned planes, to solve the prior art
Unmanned helicopter propeller set in adjust blade angle structure exist design it is unreasonable, service life is short to ask
Topic；Existing liquid medicine mixing device structure design is unreasonable, and liquid mixed effect is undesirable；Do not have on existing unmanned helicopter
The hub unit of land can conveniently be travelled on by having, the technical issues of needing to improve.
(2) technical solution
In order to solve the above technical problems, the technical solution adopted in the present invention is：It is a kind of it is energy saving and environment friendly it is medical nobody
Machine, including fuselage, the fuselage are equipped with propeller set, and the propeller set includes main shaft, adjustment axis, blade, described
Main axis is set on fuselage, and the main shaft is hollow structure, and adjustment axis, the main shaft madial wall are arranged in the main shaft
Upper edge is axially arranged with guide groove, and the adjustment axis lateral wall is equipped with the gib block that sliding is matched with the guide groove in an axial direction,
Uniformly distributed on the main shaft lateral wall there are three blade connecting rods, are each rotatablely connected respectively on the blade connecting rod there are one blade,
Uniformly distributed on the lateral wall of the adjustment axis there are three struts, and the second adjusting rod, institute are equipped between the outer end and blade of the strut
The both ends for stating the second adjusting rod are that ball connects, and the main shaft lower end is equipped with driving gear, and the lower end of the adjustment axis is equipped with first
Annular groove, the fuselage, which also rotates, is equipped with a release handle, and one end of the release handle is equipped with guide post, and the guide post can opposite sliding
Be installed in first annular slot, the other end of the release handle is rotatably connected to the driving end of one first cylinder, described first
Cylinder is articulated on fuselage；
Liquid medicine mixing device is equipped in the fuselage, the liquid medicine mixing device includes the first frame body being fixed in fuselage
With the second frame body, it is installed with the first dead axle between first frame body and the second frame body, is arranged on first dead axle
Can opposite sliding roller, be fixed with partition board on first dead axle, the partition board is for being slidingly sealed the roller with will
Space in roller is separated into mixing chamber and gear cavity, and turning set is equipped with sleeve, one end of the sleeve on first dead axle
Portion is placed in gear cavity, and the other end is set on the outside of gear cavity, and the lateral wall of the sleeve is equipped with driving item, the driving
Item is arranged in an axially parallel mode along sleeve, and the outer end of the gear cavity is sheathed on the sleeve, the outer end of the gear cavity
It is equipped with driver slot, the driving item matches with driver slot, is fixedly provided with first bevel gear on first dead axle, and described the
One bevel gear is between partition board and sleeve, and the side wall of the sleeve is equipped with the second dead axle, and second dead axle and first are determined
Axis is perpendicular, is rotated on second dead axle and is equipped with second bevel gear, the first bevel gear and second bevel gear are meshed, institute
The eccentric position for stating second bevel gear is equipped with guide post, and the madial wall of the gear cavity is equipped with the second annular groove, described to lead
It is set in second annular groove to column sliding, the end being located on the sleeve outside gear cavity is installed with second gear, described
Second gear and third gear engaged transmission, the third gear rotational installation is on the second frame body, and the third gear is by the
One motor drives its rotation；
Solar power supply apparatus is additionally provided on the fuselage, the solar power supply apparatus includes the upright bar being set on fuselage
With the sliding rail being vertically arranged, the upright bar is equipped with cross bar, is slidably connected frame by sliding block on the sliding rail, the frame side
Wall is equipped with rack, and the cross bar outer end is equipped with first gear, and the first gear is meshed transmission with rack, first tooth
Wheel is driven by third motor to drive frame to move up and down, and mounting bracket is equipped in the frame, is set in the mounting bracket
There are horizontal air cylinder, the output end of the horizontal air cylinder to be equipped with connecting plate, oblique cylinder, the connecting plate are equipped with above the connecting plate
One end be hinged with solar panels, the solar panels are connected with accumulator, the output end phase of the solar panels and oblique cylinder
It is hinged.
The fuselage bottom is additionally provided with wheel hub diameter changing device, after the wheel hub diameter changing device is including two tension bands, two
Axle stand, two front-wheel pedestals being fixed on fuselage are connected by drive shaft turns between two front-wheel pedestals, described
Driving gear is installed in drive shaft, the both ends of the drive shaft are fixedly provided with two drive sprockets, two trailing wheel pedestals
Between be rotatedly connected by driven shaft, between the trailing wheel pedestal front-wheel pedestal corresponding with homonymy by the second oil pressure cylinder,
Second oil compression rod is connected, and the both ends of the driven shaft are fixedly provided with two mounting cylinders, and each mounting cylinder is uniform radially
It is equipped at intervals with six group of first oil pressure cylinder, there are two every group of the first oil pressure cylinder tools, and is corresponded in the axial direction of the mounting cylinder,
First oil pressure cylinder is equipped with the first oil compression rod, and third dead axle is fixed between corresponding two first oil compression rods,
It is fixed with a wheel hub on each third dead axle, the tension band inner ring is evenly equipped with strip, the wheel hub along its length
Peripheral surface on be evenly equipped with card slot, the strip for being embedded in card slot and drive sprocket, the tension band and outmost turns
Wheel hub is in contact transmission, and the end face of the wheel hub is equipped with the first limiting plate for limiting the tension band, the drive sprocket
End face be equipped with the second limiting plate for limiting the tension band, the length direction of each strip is equal with driven shaft
Row, second oil pressure cylinder are connected with the first oil pressure cylinder of its homonymy.
(3) advantageous effect
The present invention is compared to the prior art, has the advantages that：
The propeller set of the present invention drives the axial position of adjustment axis by the first cylinder by driving release handle, from
And driving the second adjusting rod that the inclination angle of blade is adjusted, regulatory function is easy to use, simple in structure, and reliability is high, uses
Long lifespan；The liquid medicine mixing device of the present invention can be such that liquid is sufficiently mixed, and prevent deposited phenomenon；The wheel hub reducing of the present invention
Device can be by driving oil compression rod adjust the inclination angle of fuselage, to achieve the purpose that adaptation to the ground.
Description of the drawings
Fig. 1 is the layout of the present invention.
Fig. 2 is the stereogram one of the propeller set of the present invention.
Fig. 3 is the stereogram two of the propeller set of the present invention.
Fig. 4 is the structural exploded view of the propeller set of the present invention.
Fig. 5 is the structure chart of the liquid medicine mixing device of the present invention.
Fig. 6 is the part-structure figure one of the liquid medicine mixing device of the present invention.
Fig. 7 is the part-structure figure two of the liquid medicine mixing device of the present invention.
Fig. 8 is the part-structure figure three of the liquid medicine mixing device of the present invention.
Fig. 9 is the enlarged drawing in the portions A in Fig. 8.
Figure 10 is the structure chart of the wheel hub diameter changing device of the present invention.
Figure 11 is the part-structure figure of the wheel hub diameter changing device of the present invention.
Figure 12 is the structure chart of wheel hub in the wheel hub diameter changing device invented.
Figure 13 is the structure chart of the solar power supply apparatus of the present invention.
Specific implementation mode
With reference to the accompanying drawings and embodiments, the specific implementation mode of the present invention is described in further detail.Implement below
Example is not limited to the scope of the present invention for illustrating the present invention.
As shown in Figures 1 to 4, the present invention provides a kind of energy saving and environment friendly medical unmanned plane, including fuselage 100, described
Fuselage 100 is equipped with propeller set 10, and the propeller set 10 includes main shaft 11, adjustment axis 12, blade 13, the main shaft
11 are rotatably dispose on fuselage 100, and the main shaft 11 is hollow structure, and adjustment axis 12, the master are arranged in the main shaft 11
11 madial wall upper edge of axis is axially arranged with guide groove 111, and 12 lateral wall of the adjustment axis is equipped with and 111 phase of the guide groove in an axial direction
Coordinate the gib block 121 of sliding, is evenly distributed on 11 lateral wall of the main shaft there are three blade connecting rod 14, three blade connecting rods 14 are located at
On same plane, there are one blade 13, the lateral walls of the adjustment axis 12 for rotation connection respectively on each blade connecting rod 14
Above uniformly distributed there are three struts 15, and three struts 15 are in the same plane, are equipped between the outer end and blade 13 of the strut 15
Second adjusting rod 16, three struts 15 and three blades 13 correspond, and the certain angle that is staggered in the vertical direction, such as can
To be 5 °, the both ends of second adjusting rod 16 are that ball connects, and 11 lower end of the main shaft is equipped with driving gear 17, the sliding tooth
17 connection propeller motor (not shown) of wheel rotates to driving spindle 11, and the lower end of the adjustment axis 12 is equipped with first annular slot
122, the first annular slot 122 is horizontally arranged, and the fuselage 100, which also rotates, is equipped with a release handle 18, the adjusting
The middle part of handle 18 is rotationally connected on fuselage 100, and one end of the release handle 18 is equipped with guide post 19, and the guide post 19 can be slided relatively
Dynamic is installed in first annular slot 122, and the other end of the release handle 18 is rotatably connected to the driving end of one first cylinder 20,
First cylinder 20 is articulated on fuselage 100.After propeller electric motor starting, adjustment axis rotation is driven by main shaft, with master
The connected blade connecting rod of axis drives blade rotation, and to generate lift, the first cylinder drives adjustment axis by driving release handle
Axial position, to drive the second adjusting rod the inclination angle of blade is adjusted.
As shown in Fig. 1 and Fig. 5 to Fig. 9, liquid medicine mixing device 40, the liquid medicine mixing device are equipped in the fuselage 100
40 include being fixed on the first frame bodies 41 and the second frame body 42 in fuselage 100, between first frame body, 41 and second frame body 42
It is installed with the first dead axle 43, the roller 44 that can be slided relatively, first dead axle 43 are arranged on first dead axle 43
On be fixed with partition board 45, the partition board 45 is for being slidingly sealed the roller 44 so that the space in roller 44 is separated into mixing
Chamber 441 and gear cavity 442, the mixing chamber 441 are equipped with medicine containing opening 443, and turning set is equipped with sleeve on first dead axle 43
46, the one end of the sleeve 46 is placed in gear cavity 442, and the other end is set to 442 outside of gear cavity, the sleeve 46
Lateral wall is equipped with driving item 461, driving being arranged in an axially parallel mode along sleeve 46 of item 461, the outer end of the gear cavity 442
Portion is sheathed on the sleeve 46, and the outer end of the gear cavity 442 is equipped with driver slot 443, the driving item 461 and driving
Slot 443 matches, and first bevel gear 47 is fixedly provided on first dead axle 43, and the first bevel gear 47 is located at 45 He of partition board
Between sleeve 46, the side wall of the sleeve 46 is equipped with the second dead axle 462, and second dead axle 462 hangs down with 43 phase of the first dead axle
Directly, rotation is equipped with second bevel gear 48 on second dead axle 462, and the first bevel gear 47 is mutually nibbled with second bevel gear 48
It closes, the eccentric position of the second bevel gear 48 is equipped with guide post 481, and the madial wall of the gear cavity 442 is equipped with second
Annular groove 444, second annular groove 444 and the first dead axle 43 are coaxial, and the sliding of the guide post 481 is set to second ring
The end being located in shape slot 444, on the sleeve 46 outside gear cavity 442 is installed with second gear 49, the second gear 49 with
The engaged transmission of third gear 491, the rotational installation of third gear 491 is on the second frame body 42, and the third gear 491 is by the
One motor (not shown) drives its rotation.It is used for powder charge liquid in roller, band moving sleeve rotates after first motor starts, due to roller
Gear cavity driver slot with driving item match, sleeve drive roller rotate synchronously, roller rotation after drive second bevel gear
Movement, since sleeve is in the axial direction without displacement, the movement only rotated, second bevel gear is remained nibbles with first bevel gear
It closes, the guide post of the eccentric position in second bevel gear is moved back and forth in the axial direction by the second annular groove driving drum,
Therefore roller rotates, and the straight reciprocating motion in axial direction occurs, and liquid can be made to be sufficiently mixed uniformly, improves mixing effect
Fruit prevents deposited phenomenon.
As shown in Fig. 1, Figure 10 to Figure 12,100 bottom of the fuselage is additionally provided with wheel hub diameter changing device 50, the wheel hub reducing
Device 50 include two tension band 51, two trailing wheel pedestals 52, two front-wheel pedestals 53 being fixed on fuselage 100, two institutes
It states and is rotatedly connected by drive shaft 54 between front-wheel pedestal 53, driving gear 55, the driving are installed in the drive shaft 54
Gear 55 is connected on driving motor (not shown) to drive drive shaft 54 to rotate, and the both ends of the drive shaft 54 are fixedly provided with
Two drive sprockets 56 are rotatedly connected by driven shaft 57 between two trailing wheel pedestals 52, the trailing wheel pedestal 52 with it is same
Connected by the second oil pressure cylinder 58, the second oil compression rod 59 between the corresponding front-wheel pedestal 53 in side, the second oil compression rod 59 is fixed on
On front-wheel pedestal 53, the second oil pressure cylinder 58 is fixed on trailing wheel pedestal 52, and the both ends of the driven shaft 57 are fixedly provided with two peaces
Fitted tube 64, uniform intervals are equipped with six group of first oil pressure cylinder 60, every group of first oil pressure cylinder 60 to each mounting cylinder 64 radially
There are two tools, and is corresponded in the axial direction of the mounting cylinder 64, and first oil pressure cylinder 60 is equipped with the first oil compression rod 61,
It is fixed with third dead axle 62 between corresponding two first oil compression rods 61, is fixed on each third dead axle 62
One wheel hub 63,51 inner ring of the tension band are evenly equipped with strip 511, card are evenly equipped on the peripheral surface of the wheel hub 63 along its length
Slot 631, the strip 511 is for being embedded in card slot 631 and drive sprocket 56, the wheel hub 63 of the tension band 51 and outmost turns
Be in contact transmission, and the end face of the wheel hub 63 is equipped with the first limiting plate 632 for limiting the tension band 51, the drive chain
The end face of wheel 56 is equipped with the second limiting plate 561 for limiting the tension band 51, the length direction of each strip 511 with
Driven shaft 57 is parallel, and second oil pressure cylinder 58 is connected with the first oil pressure cylinder 60 of its homonymy.When fuselage travels on level land
When upper, the outermost loop diameter that the second oil compression rod of start makes six wheel hubs be surrounded is identical with drive sprocket, you can fuselage is made to keep
Horizontality, in order to travel；When travelling on upward slope, the second oil compression rod is adjusted so that the outmost turns that six wheel hubs are surrounded
Diameter is more than drive sprocket diameter so that fuselage leans forward, and offsets the gradient of upward slope so that fuselage travels more steady；Work as row
It sails when descending so that the outermost loop diameter that six wheel hubs are surrounded is less than drive sprocket diameter so that fuselage hypsokinesis, under counteracting
The gradient on slope.Tension band is made of flexible material, can remain tensile force with the adjustment of wheel hub.
As shown in Fig. 1 and Figure 13, solar power supply apparatus 70, the solar powered dress are additionally provided on the fuselage 100
It includes the upright bar 71 being set on fuselage 100 and the sliding rail 72 being vertically arranged to set 70, and the upright bar 71 is equipped with cross bar 73, the cunning
It is slidably connected frame 75 by sliding block 74 on rail 72,75 side wall of the frame is equipped with rack 76, and 73 outer end of the cross bar is equipped with
First gear 77, the first gear 77 are meshed transmission with rack 76, and the first gear 77 is by third motor (not shown)
Driving is equipped with mounting bracket 78 to drive frame 75 to move up and down in the frame 75, the mounting bracket 78 is equipped with water
The output end of flat cylinder 79, the horizontal air cylinder 79 is equipped with connecting plate 80, and 80 top of the connecting plate is equipped with oblique cylinder 81, described
One end of connecting plate 80 is hinged with solar panels 82, and the solar panels 82 are connected with accumulator 83, the solar panels 82 with
The output end of oblique cylinder 81 is hinged.On sunny daytime, start third motor, first gear band carry-over bar is to make on frame
It rises, oblique cylinder makes solar panels convert suitable lighting angle, and then receive the sun with making solar panels maximum area in east
Can, and solar energy is stored into accumulator, can be used for powering, when wind and rain day, solar panels can be accommodated in frame, from
Wind and rain is invaded, and service life is increased, and has the feature of environmental protection.
The above is only a preferred embodiment of the present invention, it is noted that for the ordinary skill people of the art
For member, without departing from the technical principles of the invention, several improvements and modifications can also be made, these improvements and modifications
Also it should be regarded as protection scope of the present invention.
Claims (2)
1. a kind of energy saving and environment friendly medical unmanned plane, including fuselage, which is characterized in that the fuselage is filled equipped with propeller
It sets, the propeller set includes main shaft, adjustment axis, blade, and the main axis is set on fuselage, and the main shaft is hollow
Structure is arranged with adjustment axis in the main shaft, and the main shaft madial wall upper edge is axially arranged with guide groove, the adjustment axis lateral wall
It is equipped with the gib block for matching sliding with the guide groove in an axial direction, is evenly distributed on the main shaft lateral wall there are three blade connecting rod,
Rotation connection is uniformly distributed there are three strut on the lateral wall of the adjustment axis there are one blade respectively on each blade connecting rod,
The second adjusting rod is equipped between the outer end and blade of the strut, the both ends of second adjusting rod are that ball connects, the main shaft
Lower end is equipped with driving gear, and the lower end of the adjustment axis is equipped with first annular slot, and the fuselage, which also rotates, is equipped with a release handle, institute
The one end for stating release handle is equipped with guide post, the guide post can opposite sliding be installed in first annular slot, the release handle it is another
One end is rotatably connected to the driving end of one first cylinder, and first cylinder is articulated on fuselage；
It is equipped with liquid medicine mixing device in the fuselage, the liquid medicine mixing device includes the first frame body being fixed in fuselage and the
Two frame bodies are installed with the first dead axle between first frame body and the second frame body, being arranged on first dead axle can phase
To the roller of sliding, it is fixed with partition board on first dead axle, the partition board is for being slidingly sealed the roller with by roller
Interior space is separated into mixing chamber and gear cavity, and turning set is equipped with sleeve on first dead axle, and the one end of the sleeve holds
It is placed in gear cavity, the other end is set on the outside of gear cavity, and the lateral wall of the sleeve is equipped with driving item, the driving item edge
Sleeve is arranged in an axially parallel mode, and the outer end of the gear cavity is sheathed on the sleeve, is set on the outer end of the gear cavity
There are driver slot, the driving item to be matched with driver slot, first bevel gear, first cone are fixedly provided on first dead axle
For gear between partition board and sleeve, the side wall of the sleeve is equipped with the second dead axle, second dead axle and the first dead axle phase
Vertically, rotation is equipped with second bevel gear on second dead axle, and the first bevel gear and second bevel gear be meshed, and described the
The eccentric position of two bevel gears is equipped with guide post, and the madial wall of the gear cavity is equipped with the second annular groove, the guide post
Sliding is set in second annular groove, and the end being located on the sleeve outside gear cavity is installed with second gear, and described second
Gear and third gear engaged transmission, the third gear rotational installation is on the second frame body, and the third gear is by the first electricity
Machine drives its rotation；
Solar power supply apparatus is additionally provided on the fuselage, the solar power supply apparatus includes the upright bar being set on fuselage and erects
The sliding rail being directly arranged, the upright bar are equipped with cross bar, are slidably connected frame by sliding block on the sliding rail, on the frame side wall
Equipped with rack, the cross bar outer end is equipped with first gear, and the first gear is meshed transmission with rack, the first gear by
Third motor drives to drive frame to move up and down, and mounting bracket is equipped in the frame, and the mounting bracket is equipped with water
Flat cylinder, the output end of the horizontal air cylinder are equipped with connecting plate, are equipped with oblique cylinder above the connecting plate, and the one of the connecting plate
End is hinged with solar panels, and the solar panels are connected with accumulator, and the output end of the solar panels and oblique cylinder is hinged.
2. energy saving and environment friendly medical unmanned plane according to claim 1, which is characterized in that the fuselage bottom is additionally provided with
Wheel hub diameter changing device, the wheel hub diameter changing device includes two tension bands, two trailing wheel pedestals, be fixed on two on fuselage before
Axle stand is connected between two front-wheel pedestals by drive shaft turns, driving gear is installed in the drive shaft, described
The both ends of drive shaft are fixedly provided with two drive sprockets, are rotatedly connected by driven shaft between two trailing wheel pedestals, described
It is connected by the second oil pressure cylinder, the second oil compression rod between trailing wheel pedestal front-wheel pedestal corresponding with homonymy, the driven shaft
Both ends are fixedly provided with two mounting cylinders, and uniform intervals are equipped with six group of first oil pressure cylinder to each mounting cylinder radially, every group
There are two first oil pressure cylinder tools, and is corresponded in the axial direction of the mounting cylinder, and first oil pressure cylinder is equipped with the first oil
Compression bar is fixed with third dead axle between corresponding two first oil compression rods, is fixed on each third dead axle
One wheel hub, the tension band inner ring are evenly equipped with strip along its length, and card slot, the card are evenly equipped on the peripheral surface of the wheel hub
Item is for being embedded in card slot and drive sprocket, and the tension band is in contact transmission with the wheel hub of outmost turns, the end of the wheel hub
Face is equipped with the first limiting plate and is equipped with the second limiting plate for limiting for limiting the tension band, the end face of the drive sprocket
The length direction of the position tension band, each strip is parallel with driven shaft, and the of second oil pressure cylinder and its homonymy
One oil pressure cylinder is connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810275278.8A CN108583179A (en) | 2018-03-30 | 2018-03-30 | A kind of energy saving and environment friendly medical unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810275278.8A CN108583179A (en) | 2018-03-30 | 2018-03-30 | A kind of energy saving and environment friendly medical unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108583179A true CN108583179A (en) | 2018-09-28 |
Family
ID=63623975
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810275278.8A Withdrawn CN108583179A (en) | 2018-03-30 | 2018-03-30 | A kind of energy saving and environment friendly medical unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108583179A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110619832A (en) * | 2019-11-13 | 2019-12-27 | 徐州乐泰机电科技有限公司 | Novel propeller structure |
-
2018
- 2018-03-30 CN CN201810275278.8A patent/CN108583179A/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110619832A (en) * | 2019-11-13 | 2019-12-27 | 徐州乐泰机电科技有限公司 | Novel propeller structure |
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