CN108583872A - A kind of medical deliverance apparatus of energy conservation and environmental protection helicopter - Google Patents
A kind of medical deliverance apparatus of energy conservation and environmental protection helicopter Download PDFInfo
- Publication number
- CN108583872A CN108583872A CN201810272585.0A CN201810272585A CN108583872A CN 108583872 A CN108583872 A CN 108583872A CN 201810272585 A CN201810272585 A CN 201810272585A CN 108583872 A CN108583872 A CN 108583872A
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- CN
- China
- Prior art keywords
- fuselage
- cylinder
- gear
- main shaft
- wheel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
- B64C27/58—Transmitting means, e.g. interrelated with initiating means or means acting on blades
- B64C27/59—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01F—MIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
- B01F29/00—Mixers with rotating receptacles
- B01F29/60—Mixers with rotating receptacles rotating about a horizontal or inclined axis, e.g. drum mixers
- B01F29/62—Mixers with rotating receptacles rotating about a horizontal or inclined axis, e.g. drum mixers without bars, i.e. without mixing elements; characterised by the shape or cross section of the receptacle, e.g. of Y-, Z-, S- or X- shape; with cylindrical receptacles rotating about an axis at an angle to their longitudinal axis
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01F—MIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
- B01F31/00—Mixers with shaking, oscillating, or vibrating mechanisms
- B01F31/50—Mixers with shaking, oscillating, or vibrating mechanisms with a receptacle submitted to a combination of movements, i.e. at least one vibratory or oscillatory movement
-
- 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
- B62D55/084—Endless-track units or carriages mounted separably, adjustably or extensibly on vehicles, e.g. portable track units
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/38—Alighting gear characterised by elements which contact the ground or similar surface endless-track type
Abstract
The invention discloses a kind of medical deliverance apparatus of energy conservation and environmental protection helicopter, 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 second adjusting rod is equipped between the outer end and blade of the strut.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 field of medical technology, and in particular to a kind of medical deliverance apparatus of energy conservation and environmental protection helicopter.
Background technology
Currently, the structure for adjusting blade angle in the propeller set of helicopter, which exists, designs unreasonable, service life
Short problem；Existing medicine company mixing arrangement structure design is unreasonable, and liquid mixed effect is undesirable；On existing helicopter not
With the hub unit that can conveniently travel on land, need 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 medical deliverance apparatus of energy conservation and environmental protection helicopter, existing to solve
Unreasonable with the presence of the structure design for adjusting blade angle in the propeller set of the helicopter of technology, service life is short to ask
Topic；Existing medicine company mixing arrangement structure design is unreasonable, and liquid mixed effect is undesirable；Not having on existing helicopter can
The hub unit for conveniently travelling on land, 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：A kind of energy conservation and environmental protection helicopter is medical
Deliverance apparatus, including fuselage, the fuselage are equipped with propeller set, and the propeller set includes main shaft, adjustment axis, paddle
Leaf, the main axis are set on fuselage, and the main shaft is hollow structure, and adjustment axis, the master are arranged in the main shaft
Axis madial wall upper edge is axially arranged with guide groove, and the adjustment axis lateral wall is equipped with matches sliding with the guide groove in an axial direction
Gib block, it is uniformly distributed there are three blade connecting rod on the main shaft lateral wall, it is rotatably connected to one respectively on each blade connecting rod
A blade, uniformly distributed on the lateral wall of the adjustment axis there are three struts, and second is equipped between the outer end and blade of the strut and is adjusted
The both ends of pole, 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 set
There is 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 be slided relatively
Dynamic is installed in annular groove, and the other end of the release handle is rotatably connected to the driving end of one first cylinder, first gas
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 rotatablely equipped with first rotating shaft between first frame body and the second frame body, is arranged in the first rotating shaft
Can opposite sliding roller, be installed with second gear on described first rotating shaft one end, the second gear is engaged with third gear
Transmission, on the first frame body, the third gear drives its rotation by first motor for third gear rotational installation, and described the
The side of two gears is equipped with guide rod, and the guide rod is parallel in first rotating shaft, and the roller is equipped with guide sleeve, and the guide rod is slided
It is dynamic to be sheathed in guide sleeve, compression spring is arranged in the first rotating shaft, the compression spring is between second gear and roller, a disk
Edge be articulated on second frame body, the center of the disk, which is equipped with, to be perforated and is set in first rotating shaft, the roller
The upper one side adjacent with disk is equipped with butt junction, and mandril is threaded on second frame body for supporting the circle
Disk；
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 the first dead axle is fixed between corresponding two first oil compression rods,
It is fixed with a wheel hub on each first 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 can control the amplitude moved back and forth, mixed according to liquid
Needs come correspond to adjust；The wheel hub diameter changing device of the present invention can adjust the inclination angle of fuselage by driving oil compression rod, from
And 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 structure chart of the wheel hub diameter changing device of the present invention.
Fig. 7 is the part-structure figure of the wheel hub diameter changing device of the present invention.
Fig. 8 is the structure chart of wheel hub in the wheel hub diameter changing device invented.
Fig. 9 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 medical deliverance apparatus of energy conservation and environmental protection helicopter, including fuselage
100, the 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 is rotatably dispose on fuselage 100, and the main shaft 11 is hollow structure, and adjustment axis is arranged in the main shaft 11
12,11 madial wall upper edge of the main shaft is axially arranged with guide groove 111, and 12 lateral wall of the adjustment axis is equipped with is led with described in an axial direction
Match the gib block 121 of sliding to slot 111, uniformly distributed on 11 lateral wall of the main shaft there are three blade connecting rod 14, three blades
Connecting rod 14 is in the same plane, and there are one blade 13, the adjustment axis for rotation connection respectively on each blade connecting rod 14
Uniformly distributed on 12 lateral wall there are three struts 15, and three struts 15 are in the same plane, the outer end of the strut 15 and blade
The second adjusting rod 16 is equipped between 13, three struts 15 and three blades 13 correspond, and it is certain to be staggered in the vertical direction
Angle, such as can 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 driving gear 17 connects propeller motor (not shown) and is rotated to driving spindle 11, the lower end of the adjustment axis 12
Equipped with annular groove 122, the annular groove 122 is horizontally arranged, and the fuselage 100, which also rotates, is equipped with a release handle 18, institute
The middle part for stating release 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
Opposite sliding is installed in annular groove 122, and the other end of the release handle 18 is rotatably connected to the driving of one first cylinder 20
End, first cylinder 20 are articulated on fuselage 100.After propeller electric motor starting, adjustment axis rotation is driven by main shaft, with
The connected blade connecting rod of main shaft drives blade rotation, and to generate lift, the first cylinder is by driving release handle to be adjusted to drive
The axial position of axis, to drive the second adjusting rod that the inclination angle of blade is adjusted.
As shown in Figure 1 and Figure 5, liquid medicine mixing device 40 is equipped in the fuselage 100, the liquid medicine mixing device 40 includes
The first frame body 41 and the second frame body 42 being fixed in fuselage 100 rotate peace between first frame body, 41 and second frame body 42
Equipped with first rotating shaft 43, be arranged in the first rotating shaft 43 can opposite sliding roller 44, on 43 one end of the first rotating shaft
Be installed with second gear 45, the second gear 45 and 46 engaged transmission of third gear, the rotational installation of third gear 46 in
On first frame body 41, the third gear 46 drives its rotation, the side of the second gear 45 by first motor (not shown)
It is equipped with guide rod 47, the guide rod 47 is parallel in first rotating shaft 43, and the roller 44 is equipped with guide sleeve 48, and the guide rod 47 is slided
It is dynamic to be sheathed in guide sleeve 48, compression spring 49 is arranged in the first rotating shaft 43, the compression spring 49 is located at second gear 45 and roller
Between 43, the edge of a disk 401 is articulated on second frame body 42, and the center of the disk 401 is equipped with perforation 402 and wears
Be placed in first rotating shaft 43, the disk 401 between the second frame body 42 and roller 44, on the roller 44 with disk 401
Adjacent one side is equipped with butt junction 403, and mandril 404 is threaded on second frame body 42 for supporting the disk
401, the hinge joint for supporting point, the disk 401 and the second frame body 42 of the mandril 404 and disk 401 is with first rotating shaft 43
Centered on line it is symmetrical.It is used for powder charge liquid in roller, first motor is rotated after starting by the guide rod drive roller in second gear,
By adjusting the position of mandril, when disk adjustment is perpendicular as first rotating shaft, roller does not have in its axial direction in rotation
It moves back and forth, disk is adjusted to when tilting, roller can also move back and forth, and pass through in its axial direction in rotation
The angle of inclination of disk is adjusted, the amplitude moved back and forth is can control, is adjusted according to the needs of liquid mixing to correspond to, the liquid
Mixing arrangement can be such that liquid is sufficiently mixed.In order to improve the cleanliness factor in roller, guide sleeve can be done to length, one end of guide sleeve is complete
Guide rod is coated, the one end of guide sleeve in roller forms closed.
As shown in Fig. 1, Fig. 6 to Fig. 8,100 bottom of the fuselage is additionally provided with wheel hub diameter changing device 50, the wheel hub reducing dress
Set 50 include two tension band 51, two trailing wheel pedestals 52, two front-wheel pedestals 53 being fixed on fuselage 100, described in two
It is rotatedly connected by drive shaft 54 between front-wheel pedestal 53, driving gear 55, the sliding tooth is installed in the drive shaft 54
Wheel 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
A drive sprocket 56 is rotatedly connected by driven shaft 57 between two trailing wheel pedestals 52, the trailing wheel pedestal 52 and homonymy
It is connected by the second oil pressure cylinder 58, the second oil compression rod 59 between corresponding front-wheel pedestal 53, before the second oil compression rod 59 is fixed on
On axle stand 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 installations
Cylinder 64, uniform intervals are equipped with six group of first oil pressure cylinder 60, every group of the first oil pressure cylinder 60 tool to each mounting cylinder 64 radially
There are two, and corresponded in the axial direction of the mounting cylinder 64, first oil pressure cylinder 60 is equipped with the first oil compression rod 61, right
It is fixed with the first dead axle 62 between two first oil compression rods 61 answered, one is fixed on each first dead axle 62
Wheel hub 63,51 inner ring of the tension band are evenly equipped with strip 511, card slot are evenly equipped on the peripheral surface of the wheel hub 63 along its length
631, the strip 511 is for being embedded in card slot 631 and drive sprocket 56,63 phase of wheel hub of the tension band 51 and outmost turns
The end face of Contact Transmission, the wheel hub 63 is equipped with the first limiting plate 632 for limiting the tension band 51, the drive sprocket
56 end face is equipped with the second limiting plate 561 for limiting the tension band 51, the length direction of each strip 511 with from
Moving axis 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, 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 water
Level state, 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 are straight
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 traveling
When descending so that the outermost loop diameter that six wheel hubs are surrounded is less than drive sprocket diameter so that descending is offset in fuselage hypsokinesis
The gradient.Tension band is made of flexible material, can remain tensile force with the adjustment of wheel hub.
As shown in Fig. 1 and Fig. 9, solar power supply apparatus 70, the solar power supply apparatus are additionally provided on the fuselage 100
70 include the upright bar 71 being set on fuselage 100 and the sliding rail 72 being vertically arranged, and the upright bar 71 is equipped with cross bar 73, the sliding rail
It is slidably connected frame 75 by sliding block 74 on 72,75 side wall of the frame is equipped with rack 76, and 73 outer end of the cross bar is equipped with the
One gear 77, the first gear 77 are meshed transmission with rack 76, and the first gear 77 is driven by third motor is (not shown)
Dynamic that mounting bracket 78 is equipped in the frame 75 to drive frame 75 to move up and down, the mounting bracket 78 is equipped with level
The output end of 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, the company
One end of fishplate bar 80 is hinged with solar panels 82, and the solar panels 82 are connected with accumulator 83, the solar panels 82 with tiltedly
The output end of 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 medical deliverance apparatus of energy conservation and environmental protection helicopter, including fuselage, which is characterized in that the fuselage is equipped with spiral
Paddle device, the propeller set include 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, outside the adjustment axis
Side wall is equipped with matches the gib block of sliding with the guide groove in an axial direction, and uniformly distributed on the main shaft lateral wall there are three blades to connect
Bar, rotation connection is there are one blade respectively on each blade connecting rod, and uniformly distributed on the lateral wall of the adjustment axis there are three branch
Bar is equipped with the second adjusting rod between the outer end and blade of the strut, the both ends of second adjusting rod are that ball connects, the master
Axis lower end is equipped with driving gear, and the lower end of the adjustment axis is equipped with annular groove, and the fuselage, which also rotates, is equipped with a release handle, described
One end of release handle is equipped with guide post, and what the guide post opposite can slide is installed in annular groove, and the other end of the release handle turns
The dynamic driving end for being connected with one first cylinder, first cylinder are 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 rotatablely equipped with first rotating shaft between first frame body and the second frame body, being arranged in the first rotating shaft can phase
To the roller of sliding, second gear, the second gear and third gear engaged transmission are installed on described first rotating shaft one end,
In on the first frame body, the third gear drives its rotation, second tooth by first motor for the third gear rotational installation
The side of wheel is equipped with guide rod, and the guide rod is parallel in first rotating shaft, and the roller is equipped with guide sleeve, the guide rod sliding sleeve
In guide sleeve, compression spring is arranged in the first rotating shaft, the compression spring is between second gear and roller, the side of a disk
Edge is articulated on second frame body, and the center of the disk, which is equipped with, to be perforated and be set in first rotating shaft, on the roller with
The adjacent one side of disk is equipped with butt junction, and mandril is threaded on second frame body for supporting the disk；
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. the medical deliverance apparatus of energy conservation and environmental protection helicopter according to claim 1, which is characterized in that the fuselage bottom
It is additionally provided with wheel hub diameter changing device, the wheel hub diameter changing device includes two tension bands, two trailing wheel pedestals, is fixed on fuselage
Two front-wheel pedestals are connected between two front-wheel pedestals by drive shaft turns, sliding tooth are installed in the drive shaft
Wheel, the both ends of the drive shaft are fixedly provided with two drive sprockets, and phase is rotated by driven shaft between two trailing wheel pedestals
Even, be connected by the second oil pressure cylinder, the second oil compression rod between the trailing wheel pedestal front-wheel pedestal corresponding with homonymy, it is described from
The both ends of moving axis are fixedly provided with two mounting cylinders, and uniform intervals are equipped with six group of first oil pressure to each mounting cylinder radially
Cylinder, there are two every group of the first oil pressure cylinder tools, and is corresponded in the axial direction of the mounting cylinder, and first oil pressure cylinder is equipped with
First oil compression rod is fixed with the first dead axle between corresponding two first oil compression rods, solid on each first dead axle
Surely it is equipped with a wheel hub, the tension band inner ring is evenly equipped with strip, card slot is evenly equipped on the peripheral surface of the wheel hub along its length,
The strip 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 wheel
The end face of hub is equipped with the first limiting plate and is equipped with the second limiting plate for limiting the tension band, the end face of the drive sprocket
For limiting the tension band, the length direction of each strip is parallel with driven shaft, and second oil pressure cylinder is same with it
First oil pressure cylinder of side is connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810272585.0A CN108583872A (en) | 2018-03-29 | 2018-03-29 | A kind of medical deliverance apparatus of energy conservation and environmental protection helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810272585.0A CN108583872A (en) | 2018-03-29 | 2018-03-29 | A kind of medical deliverance apparatus of energy conservation and environmental protection helicopter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108583872A true CN108583872A (en) | 2018-09-28 |
Family
ID=63624887
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810272585.0A Pending CN108583872A (en) | 2018-03-29 | 2018-03-29 | A kind of medical deliverance apparatus of energy conservation and environmental protection helicopter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108583872A (en) |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105035251A (en) * | 2015-08-31 | 2015-11-11 | 青岛科技大学 | Stepless speed change device and application thereof |
| CN205554597U (en) * | 2016-04-15 | 2016-09-07 | 徐挺 | Intelligence pesticide sprays helicopter |
-
2018
- 2018-03-29 CN CN201810272585.0A patent/CN108583872A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105035251A (en) * | 2015-08-31 | 2015-11-11 | 青岛科技大学 | Stepless speed change device and application thereof |
| CN205554597U (en) * | 2016-04-15 | 2016-09-07 | 徐挺 | Intelligence pesticide sprays helicopter |
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| PB01 | Publication | ||
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Application publication date: 20180928 |
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| RJ01 | Rejection of invention patent application after publication |