CN110254718A - A kind of shooting aircraft - Google Patents
A kind of shooting aircraft Download PDFInfo
- Publication number
- CN110254718A CN110254718A CN201910594080.0A CN201910594080A CN110254718A CN 110254718 A CN110254718 A CN 110254718A CN 201910594080 A CN201910594080 A CN 201910594080A CN 110254718 A CN110254718 A CN 110254718A
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- Prior art keywords
- power
- aircraft
- shaft
- headstock
- symmetrical
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- 230000011664 signaling Effects 0.000 claims abstract description 15
- 230000005540 biological transmission Effects 0.000 claims description 7
- 230000003139 buffering effect Effects 0.000 claims description 7
- 210000003813 thumb Anatomy 0.000 claims description 7
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 5
- 210000000006 pectoral fin Anatomy 0.000 claims description 4
- 230000000630 rising effect Effects 0.000 claims description 3
- 230000001360 synchronised effect Effects 0.000 abstract description 2
- 230000007613 environmental effect Effects 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- 238000012935 Averaging Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
Classifications
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- 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
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Transmission Devices (AREA)
Abstract
It include headstock the invention discloses a kind of shooting aircraft, symmetrical direction case is equipped on the outside of the headstock left and right part, direction chamber is equipped in the direction case, the direction is intracavitary to be equipped with driven track component, wherein the driven track component is equipped with the outrigger shaft of left and right extension and is rotatably assorted with the headstock and connect, the direction is intracavitary to be equipped with reversing arrangement and is controlled by the driven track component, wherein, signaling switch component is equipped in the reversing arrangement, the signaling switch component controls the reversing arrangement, when aircraft being needed to turn to, signaling switch component opening makes the reversing arrangement connect generation lateral thrust realization aircraft with the driven track component to turn within the scope of most short radius；The configuration of the present invention is simple, it is easy to operate, circumference to lateral thrust realize the most turning of short radius range and Synchronous camera head rotation protection shooting picture it is steady.
Description
Technical field
The present invention relates to appliance technology of taking photo by plane, specially a kind of shooting aircraft.
Background technique
It takes photo by plane also known as aerophotography or aeroplane photography, refers to from aerial photographing earth landforms, top view is obtained, as photography
Except art, it is also employed for military affairs, transport development, hydraulic engineering, ecological Studies, urban planning etc..
Traditional aircraft has independent flight system and camera system independent control automatically controlled signal to realize linkage, still
The influence that high aerial signal reception will receive environmental change causes instruction execution insensitive.Aircraft on the market needs at this stage
It needs to turn on a large scale as aircraft when turning, it is sometimes relatively difficult to achieve in the city range shooting of some small spaces.And
And shooting picture when turning to can be because the steering of aircraft be unstable.Therefore a kind of energy small range steering and steady shot picture
Aircraft become current industry development inexorable trend, a kind of device that can solve the above problem that the present invention illustrates.
Summary of the invention
The purpose of the present invention is to provide a kind of shooting aircraft, can overcome defect in the prior art.
A kind of shooting aircraft includes headstock according to the present invention, and symmetrical side is equipped on the outside of the headstock left and right part
To case, direction chamber is equipped in the direction case, the direction is intracavitary to be equipped with driven track component, wherein the driven track component
It is connect equipped with controlling the outrigger shaft extended and being rotatably assorted with the headstock, the direction is intracavitary to be equipped with reversing arrangement and by institute
State the control of driven track component, wherein signaling switch component, the signaling switch component pair are equipped in the reversing arrangement
The reversing arrangement is controlled, and when aircraft being needed to turn to, the signaling switch component opening makes the reversing arrangement and institute
It states driven track component connection generation lateral thrust and realizes that aircraft turns within the scope of most short radius, pass through the auxiliary of reversing arrangement
Power-assist power drives the sporting flying of aircraft high-freedom degree, and power cavity is equipped in the headstock, is equipped with and prolongs in the power cavity
The flight system component for extending to top outer meets the power of aircraft rising, is equipped in the power cavity symmetrical dynamic
It power drive component and is connected by power with the flight system component, the power cavity bottom end is equipped with change over switch device, wherein institute
It states and is equipped with selection cam in change over switch device, the selection cam controls the power drive assem, and selection turns to
Direction allows the selection cam to abut with the power drive assem of side, and the headstock bottom outside is equipped with photographic device
And be connected by power with the change over switch device, shooting angle is maintained, buffering foot prop dress is equipped on the outside of the headstock left and right part
It sets, the buffer protection device in aircraft landing.
It may be preferred that the driven track component includes that intracavitary be rotatably assorted in the direction is connected with left and right extension and runs through
To the outrigger shaft in the power cavity, the track bevel gear intracavitary positioned at the direction, the rail are socketed on the outrigger shaft
Road bevel gear and the direction case side close to each other are fixedly connected with bracket, and the outrigger shaft is equipped with far from symmetrical centre point
Driven wheel of differential, the outrigger shaft are equipped with the linkage structure being located in the power cavity, optimize linkage structure.
It may be preferred that the linkage structure includes connecting shaft block, it is equipped with rotation slot in the connecting shaft block, is set in the connecting shaft block
The useful locking slot being connected with the rotation slot, drives the only work in demand of different components.
It may be preferred that the reversing arrangement includes that direction chamber top inner wall is rotatably assorted the change for being connected with and extending up and down
To axis, the turning axis be equipped with positioned at direction case top end face deflecting paddle, the turning axis be equipped with with it is described
The commutation bevel gear of the ratcheting connection of driven wheel of differential, the turning axis are equipped with the switching for being located at the commutation bevel gear upper end
Case, the a-b box is interior to be equipped with switching chamber, and the switching is intracavitary to be slidably connected with the active being socketed with the turning axis
Pushing block, active pushing block lower end and switching bottom of chamber end press are connected with recovery spring, and the switching bottom of chamber end inner wall is sliding
Dynamic to be connected with symmetrical slip pipe, the slip pipe is equipped with the driven pushing block for the connection that offsets with the active pushing block,
The slip pipe is equipped with the loop orbit plate with the ratcheting connection of the driven wheel of differential, is generated lateral thrust help and is turned to.
It may be preferred that the signaling switch component includes that direction case top inner wall is embedded with hydraulic press, it is described hydraulic
Machine lower end end has been connected by power hydraulic push rod, is equipped in the direction case and is located at the turning axis close to the limit at symmetrical centre end
Position sliding block, the position limiting slide block is interior to be equipped with sliding rail chamber, and the direction case is fixedly connected with torque on the inner wall of symmetrical centre end
Axis is rotatably assorted on the torque axis and is connected with driving lever, and the driving lever is equipped with the card slot of opening upwards, the driving lever with it is described
The press of direction case side close to each other is connected with torsion spring, and the sliding rail is intracavitary to be slidably connected with push rod, the push rod with
The a-b box sliding connection, the push rod offset with the active pushing block and connect, and store power and wait being detached from and restore to repeat to make
With.
It may be preferred that the flight system component includes that power cavity top inner wall is fixedly connected with lifting motor, institute
It states lifting motor and is connected by power the drive shaft extended up and down, drive shaft lower end end is equipped with driving bevel gear, the drive
Moving axis is equipped with the concave positioned at the driving bevel gear upper end, and drive shaft upper end end, which is equipped with, is located at the headstock
The rotating block of upper end end face is rotatably assorted on the rotating block and is connected with centrosymmetric shaft, and the shaft is far from symmetrical
Heart end is equipped with propeller, and power cavity top inner wall is slidably connected with pull rod, the pull rod lower end and the concave
Offset connection, and the pull rod upper end is fixedly connected with the propeller, increase aircraft.
It may be preferred that the power drive assem includes that the power cavity rear end inner wall is fixedly connected with axle bed, the axis
It is rotatably assorted on seat and is connected with the driving shaft that left and right extends, the driving shaft is fixedly connected with linkage knot far from symmetrical centre end
Structure, the driving shaft right end is equipped with the drive bevel gear with the ratcheting connection of the driving bevel gear, in described power cavity or so
It is fixedly connected with symmetrical swing rod on wall, the cunning supporting plate extended up and down, the sliding supporting plate are slidably connected on the swing rod
Upper end, which is rotatably assorted, is connected with interlocking bar, and the interlocking bar is equipped with the lock for being located at and being connected by power in the linkage structure and therewith
Bar, power communication conversion.
It may be preferred that the change over switch device includes that power cavity bottom end inner wall is provided with reversing motor, the commutation electricity
Machine top is connected by power the transmission shaft extended up and down, and the transmission shaft is equipped with active thumb wheel, power cavity bottom end inner wall
Be rotatably assorted the fluted roller shaft for being connected with and extending up and down, and the fluted roller shaft is equipped with the slot for the connection that offsets with the active thumb wheel
Wheel, the fluted roller shaft are equipped with position and the sheave upper end and the connection that offsets with the sliding supporting plate selection cam, the slot
Wheel shaft is equipped with the photographic device positioned at the headstock bottom outside, and driving turns to.
It may be preferred that the photographic device includes being rotatably assorted to be connected with shot box on the fluted roller shaft, the shot box
Interior to be equipped with open slot, the fluted roller shaft is equipped with the turntable being located in the open slot, and the turntable lower end is rotatably assorted connection
There is hanger axis, sliding rail is equipped in hanger axis lower end, camera is slidably connected on the sliding rail, is set on the turntable
There is the push rod positioned at hanger axis left end, keeps the direction of camera lens.
It may be preferred that the buffering leg means include that the headstock or so end face is fixedly connected with symmetrical foot
, it is hingedly connected with hydraulic foot lever on the pedestal, the hydraulic foot lever lower end is hingedly connected with flippers, and the hydraulic foot lever is remote
It is equipped with limited block from symmetrical centre end end face, is slidably connected with limit plate, the limit plate and institute on the hydraulic foot lever
Limited block to be stated to offset connection, the limit plate is equipped with extended cavity up and down, and the fluted roller shaft is located in the extended cavity,
Aircraft stabilization is parked in ground.
The beneficial effects of the present invention are: structure of the invention is simple, easy to operate, the power source band gone up and down by aircraft
The operation of dynamic transfer, and turned around by being realized within the scope of most short radius sideways against power on circumference, it turns to simultaneously
Device is connected with camera adjustment, and direction remains unchanged when realizing turning, guarantees that shooting picture is flat when aircraft is turned
Stability realizes that aircraft lifting makes to protect aircraft not destroyed using buffer unit, extends the service life of device, while benefit
Change climb efficiency and the driving capability for improving flight with the impeller included angle in flight active force, optimizes the flight of aircraft
Path and using energy source, compound current market environmental protection, efficient requirement.
Detailed description of the invention
The present invention is described in detail by following specific embodiments and drawings for ease of explanation,.
Fig. 1 is a kind of overall structure diagram of shooting aircraft of the invention；
Fig. 2 is the schematic cross-section of " A-A " of Fig. 1；
Fig. 3 is the schematic cross-section of " B-B " of Fig. 1；
Fig. 4 is the enlarged structure schematic diagram of " C " of Fig. 1.
Specific embodiment
Below with reference to Fig. 1-Fig. 4, the present invention is described in detail, for sake of convenience, now provides to hereafter described orientation
As follows: hereafter described front-rear direction up and down is consistent with the front-rear direction up and down of Fig. 1 projection relation itself.
A kind of shooting aircraft includes headstock 11 according to the present invention, is equipped on the outside of 11 left and right part of headstock symmetrical
Direction case 23, be equipped with direction chamber 24 in the direction case 23, driven track component be equipped in the direction chamber 24, wherein described
Driven track component is equipped with the outrigger shaft 34 that left and right extends and is rotatably assorted with the headstock 11 and connect, in the direction chamber 24
It is controlled equipped with reversing arrangement and by the driven track component, wherein signaling switch component is equipped in the reversing arrangement,
The signaling switch component controls the reversing arrangement, and when aircraft being needed to turn to, the signaling switch component is opened
So that the reversing arrangement is connect generation lateral thrust with the driven track component and realizes that aircraft turns within the scope of most short radius
To by the sporting flying of the auxiliary power drive aircraft high-freedom degree of reversing arrangement, the headstock 11 is interior to be equipped with power
Chamber 17, the power cavity 17 is interior to be equipped with the flight system component for extending to top outer, meets the power of aircraft rising, described
It is equipped with symmetrical power drive assem in power cavity 17 and is connected by power with the flight system component, the power cavity 17
Bottom end is equipped with change over switch device, wherein selection cam 48, described 48 pairs of institutes of selection cam are equipped in the change over switch device
It states power drive assem to be controlled, selects steering direction that the selection cam 48 and the power drive assem of side is allowed to support
It connecing, 11 bottom outside of headstock is equipped with photographic device and is connected by power with the change over switch device, shooting angle is maintained,
Buffering leg means are equipped on the outside of 11 left and right part of headstock, the buffer protection device in aircraft landing.
Valuably, the driven track component includes being rotatably assorted to be connected with left and right extension and run through in the direction chamber 24
To the outrigger shaft 34 in the power cavity 17, the track bevel gear in the direction chamber 24 is socketed on the outrigger shaft 34
57, the track bevel gear 57 is fixedly connected with bracket 56 with the direction case 23 side close to each other, sets on the outrigger shaft 34
There is the driven wheel of differential 58 of separate symmetrical centre point, the outrigger shaft 34 is equipped with the linkage knot being located in the power cavity 17
Structure.
Valuably, the linkage structure includes connecting shaft block 72, is equipped with rotation slot 66, the connecting shaft block in the connecting shaft block 72
It is equipped in 72 with the locking slot 64 being connected with the rotation slot 66.
Valuably, the reversing arrangement includes that the 24 top inner wall of direction chamber is rotatably assorted the change for being connected with and extending up and down
To axis 22, the turning axis 22 is equipped with the deflecting paddle 21 positioned at the 23 top end face of direction case, sets in the turning axis 22
The useful commutation bevel gear 33 with the ratcheting connection of the driven wheel of differential 58, the turning axis 22, which is equipped with, is located at commutation cone
The a-b box 26 of 33 upper end of gear, the a-b box 26 is interior to be equipped with switching chamber 27, is slidably connected in the switching chamber 27
With the active pushing block 28 being socketed with the turning axis 22,28 lower end of active pushing block and 27 bottom end of switching chamber press are connected
Have and restore spring 30, the 27 bottom end inner wall of switching chamber is slidably connected with symmetrical slip pipe 31, on the slip pipe 31
Equipped with the driven pushing block 29 with the connection that offsets with the active pushing block 28, the slip pipe 31 be equipped with with the driven wheel of differential
The loop orbit plate 32 of 58 ratcheting connections.
Valuably, the signaling switch component includes that the 23 top inner wall of direction case is embedded with hydraulic press 70, the liquid
70 lower end end of press has been connected by power hydraulic push rod 71, is equipped in the direction case 23 and is located at the turning axis 22 close to symmetrical
The position limiting slide block 20 of center-side, the position limiting slide block 20 is interior to be equipped with sliding rail chamber 62, and the direction case 23 is in symmetrical centre end
It is fixedly connected with torque axis 18 on wall, is rotatably assorted on the torque axis 18 and is connected with driving lever 59, the driving lever 59 is equipped with and opens
The upward card slot 61 of mouth, the driving lever 59 are connected with torsion spring 19, the cunning with the press of the direction case 23 side close to each other
Push rod 25 is slidably connected in rail chamber 62, the push rod 25 is slidably connected with the a-b box 26, the push rod 25
It offsets and connect with the active pushing block 28.
Valuably, the flight system component includes that the 17 top inner wall of power cavity is fixedly connected with lifting motor 12,
The lifting motor 12 is connected by power the drive shaft 15 extended up and down, and the 15 lower end end of drive shaft is equipped with driving bevel gear
54, the drive shaft 15 is equipped with the concave 55 positioned at 54 upper end of driving bevel gear, the 15 upper end end of drive shaft
Equipped with the rotating block 16 for being located at the 11 upper end end face of headstock, being rotatably assorted on the rotating block 16, it is centrosymmetric to be connected with
Shaft 14, the shaft 14 are equipped with propeller 10,17 top inner wall of the power cavity sliding connection far from symmetrical centre end
There is pull rod 13,13 lower end of pull rod offsets with the concave 55 to be connect, and 13 upper end of pull rod and the propeller 10 are solid
Fixed connection.
Valuably, the power drive assem includes that the 17 rear end inner wall of power cavity is fixedly connected with axle bed, the axis
It is rotatably assorted on seat and is connected with the driving shaft 67 that left and right extends, the driving shaft 67 is fixedly connected with linkage far from symmetrical centre end
Structure, 67 right end of driving shaft are equipped with the drive bevel gear 68 with the ratcheting connection of the driving bevel gear 54, the power
It is fixedly connected with symmetrical swing rod 69 on 17 or so inner wall of chamber, the sliding branch extended up and down is slidably connected on the swing rod 69
Plate 60, sliding 60 upper end of supporting plate, which is rotatably assorted, is connected with interlocking bar 40, and the interlocking bar 40, which is equipped with, is located at linkage knot
The locking bar 65 being connected by power in structure and therewith.
Valuably, the change over switch device includes that 17 bottom end inner wall of power cavity is provided with reversing motor 37, the commutation
37 top of motor is connected by power the transmission shaft 36 extended up and down, and the transmission shaft 36 is equipped with active thumb wheel 35, the power
17 bottom end inner wall of chamber is rotatably assorted the fluted roller shaft 46 for being connected with and extending up and down, and the fluted roller shaft 46 is equipped with to be dialled with the active
The sheave 47 that wheel 35 offsets connection, the fluted roller shaft 46 be equipped with position and 47 upper end of sheave and with sliding 60 phase of supporting plate
Selection cam 48 to connection, the fluted roller shaft 46 are equipped with the photographic device positioned at 11 bottom outside of headstock.
Valuably, the photographic device includes being rotatably assorted to be connected with shot box 44 on the fluted roller shaft 46, the photography
It is equipped with open slot 41 in case 44, the fluted roller shaft 46 is equipped with the turntable 45 being located in the open slot 41, under the turntable 45
End, which is rotatably assorted, is connected with hanger axis 38, and sliding rail 39, the company of being slidably matched on the sliding rail 39 are equipped in 38 lower end of hanger axis
It is connected to camera 42, the turntable 45 is equipped with the push rod 43 positioned at 38 left end of hanger axis.
Valuably, the buffering leg means include that 11 or so the end face of headstock is fixedly connected with symmetrical pedestal
53, hydraulic foot lever 50 is hingedly connected on the pedestal 53, and hydraulic 50 lower end of foot lever is hingedly connected with flippers 49, the liquid
Presser bar 50 is equipped with limited block 51 far from symmetrical centre end end face, is slidably connected with limit plate on the hydraulic foot lever 50
52, the limit plate 52 offsets with the limited block 51 and connect, and the limit plate 52 is equipped with extended cavity 63 up and down, institute
Fluted roller shaft 46 is stated to be located in the extended cavity 63.
In the initial state, the locking bar 65 is located in the rotation slot 66 a kind of shooting aircraft of the invention, described
Do not offset connection between selection cam 48 and the sliding supporting plate 60, and the hydraulic press 70 closes 71 contraction state of hydraulic push rod
And the push rod 25 is disconnected with the card slot 61, the direction case 23 is placed in the same direction with the headstock 11, the lifting
Motor 12 and the reversing motor 37 are in closed state, and all parts are in off working state.
When being worked using a kind of shooting aircraft of the invention, starts the lifting motor 12 and drive the drive shaft 15
The rotating block 16, the driving bevel gear 54 and the concave 55 are rotated, the rotating block 16 rotates institute by shaft 14
Propeller 10 is stated, while the concave 55 pulls the level angle of the propeller 10 to change by the pull rod 13, flow-disturbing
Flight, starts the reversing motor 37 and the transmission shaft 36 is driven to rotate the active thumb wheel 35, the active when needing to turn to
Thumb wheel 35 stirs the sheave 47 by the connection that offsets, and the sheave 47 drives the selection cam 48 by the fluted roller shaft 46
It is rotated with the turntable 45, one of those offsets and connect with cunning supporting plate 60 described in the end of left and right for the selection cam 48 rotation, logical
It crosses interlocking bar 40 to promote the locking bar 65 in the locking slot 64, the driving bevel gear 54 passes through described in ratcheting connection drive
Drive bevel gear 68, the drive bevel gear 68 drive the connecting shaft block 72 by driving shaft 67, and the connecting shaft block 72 passes through institute
State locking bar 65, the interlocking bar 40 drives the outrigger shaft 34 to rotate the driven wheel of differential 58, the driven wheel of differential 58
The commutation bevel gear 33 is driven to rotate by ratcheting connection, the commutation bevel gear 33 appeals turning axis 22 by Europe and rotates institute
State a-b box 26 and the deflecting paddle 21, the rotation of deflecting paddle 21 generates lateral thrust, due to the hydraulic press 70 with it is described
37 Electricity Federation synchronous averaging of reversing motor pushes the push rod 25 to slide in the card slot 61 by the hydraulic push rod 71, and described
Push rod 25 pushes the driven pushing block 29 by the active pushing block 28, the driven pushing block 29 by beat up slip pipe 31 push it is described
Loop orbit plate 32 and the track bevel gear 57 it is ratcheting connection and along rotation, steering of the push rod 25 by the a-b box 26
Power is slided in the sliding rail chamber 62, the elastic force of the savings of torsion spring 19 torsion is made by the driving lever 59 rotation, together
Shi Suoshu turntable 45 is stirred the camera 42 and slided on the sliding rail 39 by the push rod 43 guarantees shooting direction.
A kind of shooting aircraft of the invention closes the hydraulic press 70 and the reversing motor 37 after power cut-off,
The power output of the lifting motor 12 is reduced to zero, is slowly reduced aircraft, while the flippers 49 contacts ground and passes through
The buffering of hydraulic foot lever 50 is simultaneously come to a complete stop by the extended cavity 63 limitation.
The beneficial effects of the present invention are: structure of the invention is simple, easy to operate, the power source band gone up and down by aircraft
The operation of dynamic transfer, and turned around by being realized within the scope of most short radius sideways against power on circumference, it turns to simultaneously
Device is connected with camera adjustment, and direction remains unchanged when realizing turning, guarantees that shooting picture is flat when aircraft is turned
Stability realizes that aircraft lifting makes to protect aircraft not destroyed using buffer unit, extends the service life of device, while benefit
Change climb efficiency and the driving capability for improving flight with the impeller included angle in flight active force, optimizes the flight of aircraft
Path and using energy source, compound current market environmental protection, efficient requirement.
In the above manner, those skilled in the art can be made within the scope of the invention according to operating mode it is various
Change.
Claims (10)
1. a kind of shooting aircraft includes headstock, symmetrical direction case, feature are equipped on the outside of the headstock left and right part
It is: is equipped with direction chamber in the direction case, the direction is intracavitary is equipped with driven track component, wherein the driven track component
It is connect equipped with controlling the outrigger shaft extended and being rotatably assorted with the headstock, the direction is intracavitary to be equipped with reversing arrangement and by institute
State the control of driven track component, wherein signaling switch component, the signaling switch component pair are equipped in the reversing arrangement
The reversing arrangement is controlled, and when aircraft being needed to turn to, the signaling switch component opening makes the reversing arrangement and institute
It states driven track component connection generation lateral thrust and realizes that aircraft turns within the scope of most short radius, pass through the auxiliary of reversing arrangement
Power-assist power drives the sporting flying of aircraft high-freedom degree, and power cavity is equipped in the headstock, is equipped with and prolongs in the power cavity
The flight system component for extending to top outer meets the power of aircraft rising, is equipped in the power cavity symmetrical dynamic
It power drive component and is connected by power with the flight system component, the power cavity bottom end is equipped with change over switch device, wherein institute
It states and is equipped with selection cam in change over switch device, the selection cam controls the power drive assem, and selection turns to
Direction allows the selection cam to abut with the power drive assem of side, and the headstock bottom outside is equipped with photographic device
And be connected by power with the change over switch device, shooting angle is maintained, buffering foot prop dress is equipped on the outside of the headstock left and right part
It sets, the buffer protection device in aircraft landing.
2. a kind of shooting aircraft as described in claim 1, wherein the driven track component includes intracavitary turn of the direction
It moves and is connected with the outrigger shaft that left and right extends and is through in the power cavity, be socketed on the outrigger shaft positioned at the side
To intracavitary track bevel gear, the track bevel gear and the direction case side close to each other are fixedly connected with bracket, described to prolong
It stretches axis and is equipped with the driven wheel of differential far from symmetrical centre point, the outrigger shaft is equipped with the linkage knot being located in the power cavity
Structure.
3. such as a kind of shooting aircraft of claim 2, it is characterised in that: the linkage structure includes connecting shaft block, the connecting shaft block
It is interior to be equipped with rotation slot, it is equipped in the connecting shaft block with the locking slot being connected with the rotation slot.
4. a kind of shooting aircraft as described in claim 1, it is characterised in that: the reversing arrangement includes direction chamber top
End inner wall is rotatably assorted the turning axis for being connected with and extending up and down, and the turning axis is equipped with positioned at direction case top end face
Deflecting paddle, the turning axis are equipped with the commutation bevel gear with the ratcheting connection of the driven wheel of differential, set in the turning axis
There is the a-b box for being located at the commutation bevel gear upper end, switching chamber is equipped in the a-b box, the switching is intracavitary to be slidably matched
The useful active pushing block with turning axis socket is connected, active pushing block lower end is connected with switching bottom of chamber end press
Restore spring, switching bottom of chamber end inner wall is slidably connected with symmetrical slip pipe, the slip pipe equipped with with institute
It states active pushing block to offset the driven pushing block of connection, the slip pipe is equipped with the loop orbit with the ratcheting connection of the driven wheel of differential
Plate.
5. a kind of shooting aircraft as described in claim 1, it is characterised in that: the signaling switch component includes the direction
Case top inner wall is embedded with hydraulic press, and hydraulic press lower end end has been connected by power hydraulic push rod, has been equipped in the direction case
Sliding rail chamber is equipped in the position limiting slide block at symmetrical centre end, the position limiting slide block positioned at the turning axis, the direction case leans on
It is fixedly connected with torque axis on the inner wall of nearly symmetrical centre end, is rotatably assorted on the torque axis and is connected with driving lever, on the driving lever
Card slot equipped with opening upwards, the driving lever and direction case side press close to each other are connected with torsion spring, the sliding rail
Intracavitary to be slidably connected with push rod, the push rod and the a-b box are slidably connected, and the push rod is pushed away with the active
Block offsets connection.
6. a kind of shooting aircraft as described in claim 1, it is characterised in that: the flight system component includes the power
Chamber top inner wall is fixedly connected with lifting motor, and the lifting motor is connected by power the drive shaft extended up and down, the driving
Axis lower end end is equipped with driving bevel gear, and the drive shaft is equipped with the concave positioned at the driving bevel gear upper end, described
Drive shaft upper end end is equipped with the rotating block positioned at headstock upper end end face, is rotatably assorted in being connected on the rotating block
The symmetrical shaft of the heart, the shaft are equipped with propeller, the sliding connection of power cavity top inner wall far from symmetrical centre end
There is pull rod, the pull rod lower end offsets with the concave to be connect, and the pull rod upper end is fixedly connected with the propeller.
7. a kind of shooting aircraft as described in claim 1, it is characterised in that: the power drive assem includes the power
Cavity rear end inner wall is fixedly connected with axle bed, is rotatably assorted on the axle bed and is connected with the driving shaft that left and right extends, the driving shaft
Be fixedly connected with linkage structure far from symmetrical centre end, the driving shaft right end be equipped with with the ratcheting connection of the driving bevel gear
Drive bevel gear, be fixedly connected with symmetrical swing rod on described power cavity or so inner wall, be slidably connected on the swing rod
There is the cunning supporting plate extended up and down, the sliding supporting plate upper end, which is rotatably assorted, is connected with interlocking bar, and the interlocking bar, which is equipped with, is located at institute
State the locking bar being connected by power in linkage structure and therewith.
8. a kind of shooting aircraft as described in claim 1, it is characterised in that: the change over switch device includes power cavity bottom
End inner wall is provided with reversing motor, and the reversing motor top is connected by power the transmission shaft extended up and down, on the transmission shaft
Equipped with active thumb wheel, power cavity bottom end inner wall is rotatably assorted the fluted roller shaft for being connected with and extending up and down, sets on the fluted roller shaft
The sheave of the useful connection that offsets with the active thumb wheel, the fluted roller shaft be equipped with position and the sheave upper end and with the cunning
Supporting plate offsets the selection cam of connection, and the fluted roller shaft is equipped with the photographic device positioned at the headstock bottom outside.
9. a kind of shooting aircraft as claimed in claim 8, it is characterised in that: the photographic device includes on the fluted roller shaft
It is rotatably assorted and is connected with shot box, open slot is equipped in the shot box, the fluted roller shaft, which is equipped with, to be located in the open slot
Turntable, the turntable lower end, which is rotatably assorted, is connected with hanger axis, and sliding rail is equipped in hanger axis lower end, sliding on the sliding rail
Dynamic to be connected with camera, the turntable is equipped with the push rod positioned at hanger axis left end.
10. a kind of shooting aircraft as described in claim 1, it is characterised in that: the buffering leg means include described dynamic
Power case or so end face is fixedly connected with symmetrical pedestal, and hydraulic foot lever, the hydraulic foot lever are hingedly connected on the pedestal
Lower end is hingedly connected with flippers, and the hydraulic foot lever is equipped with limited block far from symmetrical centre end end face, slides on the hydraulic foot lever
Dynamic to be connected with limit plate, the limit plate offsets with the limited block and connect, and the limit plate is equipped with up and down
Extended cavity, the fluted roller shaft are located in the extended cavity.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910594080.0A CN110254718A (en) | 2019-07-03 | 2019-07-03 | A kind of shooting aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910594080.0A CN110254718A (en) | 2019-07-03 | 2019-07-03 | A kind of shooting aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110254718A true CN110254718A (en) | 2019-09-20 |
Family
ID=67924127
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910594080.0A Withdrawn CN110254718A (en) | 2019-07-03 | 2019-07-03 | A kind of shooting aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110254718A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112381974A (en) * | 2020-11-16 | 2021-02-19 | 成都中科大旗软件股份有限公司 | Stadium passenger flow early warning system |
| CN112918675A (en) * | 2021-03-15 | 2021-06-08 | 杭州翰昌电子商务有限公司 | Unmanned aerial vehicle for water quality monitoring of maintaining dynamic balance |
| CN113298070A (en) * | 2021-06-25 | 2021-08-24 | 安徽机电职业技术学院 | Target recognition device for industrial robot |
-
2019
- 2019-07-03 CN CN201910594080.0A patent/CN110254718A/en not_active Withdrawn
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112381974A (en) * | 2020-11-16 | 2021-02-19 | 成都中科大旗软件股份有限公司 | Stadium passenger flow early warning system |
| CN112918675A (en) * | 2021-03-15 | 2021-06-08 | 杭州翰昌电子商务有限公司 | Unmanned aerial vehicle for water quality monitoring of maintaining dynamic balance |
| CN113298070A (en) * | 2021-06-25 | 2021-08-24 | 安徽机电职业技术学院 | Target recognition device for industrial robot |
| CN113298070B (en) * | 2021-06-25 | 2022-04-01 | 安徽机电职业技术学院 | Target recognition device for industrial robot |
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Application publication date: 20190920 |
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| WW01 | Invention patent application withdrawn after publication |