CN108974379A - A kind of general aviation low-altitude monitor operation aircraft - Google Patents
A kind of general aviation low-altitude monitor operation aircraft Download PDFInfo
- Publication number
- CN108974379A CN108974379A CN201810524475.9A CN201810524475A CN108974379A CN 108974379 A CN108974379 A CN 108974379A CN 201810524475 A CN201810524475 A CN 201810524475A CN 108974379 A CN108974379 A CN 108974379A
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- fuselage
- fixedly connected
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- general aviation
- aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
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- 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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Mechanical Control Devices (AREA)
Abstract
The invention discloses a kind of general aviation low-altitude monitor operation aircraft, including fuselage, the lower surface of fuselage is fixedly connected there are four pedestal, and four pedestals are located at the four corners of fuselage lower surface, there are two horns for the upper surface setting of fuselage, and the surface of two horns is provided with propeller, the left and right sides of fuselage are clamped that there are two first bearings respectively, and two the second shafts are respectively sleeved in two first bearings.The general aviation low-altitude monitor operation aircraft, pass through the mutual cooperation between handle, the second shaft, threaded post, thread barrel, movable plate, gag lever post, telescopic device, crushing block, sliding slot and sliding block, to which monitor ontology is preferably fixed in aircraft, aircraft is prevented to shake and fall off in flight course, pass through tool again without staff to twist monitor ontology manually on board the aircraft, to facilitate the work of staff, the stability of monitor ontology is improved.
Description
Technical field
The present invention relates to vehicle technology field, specially a kind of general aviation low-altitude monitor operation aircraft.
Background technique
UAV referred to as " aircraft ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, or fully or intermittently automatically operated by car-mounted computer, aircraft presses application field, can divide
For it is military with it is civilian.Military aspect, aircraft are divided into reconnaissance plane and target drone.Civilian aspect, aircraft+industrial application are flight
Device has really just needed；It taking photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, supervising at present
The application in infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making and manufacture romance etc. field is controlled, greatly
The purposes of aircraft itself is expanded, developed country also in actively extension industrial application and develops vehicle technology.
Installing video camera additional on board the aircraft can be used to take photo by plane, and existing carry-on video camera is usually all work people
Threaded post is screwed on the fuselage of aircraft by member manually by tool, thus on board the aircraft by video camera installation, but it is this
Method is very troublesome, brings inconvenience to the work of staff, and aircraft can generate shaking in flight course, images
Machine can have an impact shooting effect since fixed effect is bad, or even can video camera be fallen off, and the angle of video camera is
Fixed, it can only be very inconvenient to operate by adjusting the angle of aircraft to adjust the angle of video camera.
Summary of the invention
(1) the technical issues of solving
In view of the deficiencies of the prior art, it the present invention provides a kind of general aviation low-altitude monitor operation aircraft, solves existing
Carry-on video camera to be usually all staff be screwed in threaded post on the fuselage of aircraft manually by tool, thus
On board the aircraft by video camera installation, but this method is very troublesome, brings inconvenience to the work of staff, and take the photograph
It fixes, can only be operated very not when the angle of camera by adjusting the angle of aircraft to adjust the angle of video camera
Convenient problem.
(2) technical solution
To achieve the above object, the invention provides the following technical scheme: a kind of general aviation low-altitude monitor operation aircraft, including
Fuselage, the lower surface of the fuselage is fixedly connected there are four pedestal, and four pedestals are located at the four corners of fuselage lower surface,
There are two horns for the upper surface setting of the fuselage, and the surface of two horns is provided with propeller, the left and right of the fuselage
Two sides are clamped respectively there are two first bearing, and two the second shafts are respectively sleeved in two first bearings, and two the
The mutually separate one end of two shafts is respectively fixedly connected with there are two handle, and the opposite end of two the second shafts respectively with two screw threads
Mutually separate one section of column is fixedly connected, and the surface of two threaded posts is threadedly coupled that there are two thread barrels, and two screw threads respectively
The opposite face of cylinder is fixedly connected with the left and right sides of two movable plates respectively, and fixation connects respectively for the lower surface of two movable plates
Sliding block there are two connecing, and two sliding blocks are slidably connected at respectively in two sliding slots, and two sliding slots are provided with the first fixed plate
Upper surface, the left side of the fuselage inner wall is fixedly connected by the first fixed plate with the right side of fuselage inner wall, and two
The opposite face of movable plate is respectively fixedly connected with there are two gag lever post, and the opposite end of two gag lever posts respectively with two the first grooves
The left and right sides of inner wall overlap, and two the first grooves are provided in first rotating shaft.
Preferably, the top of the first rotating shaft and the upper surface of the second groove inner wall overlap, second groove opens up
In the lower surface in fuselage inner wall, and the left and right sides of first rotating shaft are overlapped with the opposite face of two crushing blocks respectively, and two
The mutually separate one end of a crushing block passes through two telescopic devices respectively and is fixedly connected with the left and right sides of the second groove inner wall, and
The surface of first rotating shaft is socketed with fourth bearing, and fourth bearing is connected to the upper surface of the first fixed plate.
Preferably, the surface of the first rotating shaft is fixedly connected with gear, and the gear is engaged with ratch, the ratch
Right end is fixedly connected by electric pushrod with the left side of the first connecting plate, and the lower surface of first fixed plate connects by first
Fishplate bar is fixedly connected with the upper surface of the second fixed plate, and the left end of the ratch passes through the right side of the second telescopic rod and the second connecting plate
Side is fixedly connected, and the lower surface of first fixed plate connects by the way that the upper surface of the second connecting plate and the second fixed plate is fixed
It connects, and the upper surface of the second fixed plate is connected with 3rd bearing, and 3rd bearing is socketed in the outer surface of first rotating shaft, described
The surface of one shaft is socketed with second bearing, and second bearing is connected to the lower surface of fuselage.
Preferably, the front of the fuselage is fixedly connected with power supply, and the front of the power supply is fixedly connected with switch.
Preferably, the output end of the power supply is electrically connected with the input terminal of switch, and the output end and electric pushrod switched
Input terminal electrical connection, and switch model LW5D-16.
Preferably, the telescopic device includes the first telescopic rod and the spring for being socketed in the first telescopic rod surface, the machine
The left side of body inner wall is fixedly connected by the first telescopic rod and spring with the left side of crushing block.
Preferably, the fourth bearing and 3rd bearing are located above and below gear, the second bearing position
In the lower section of 3rd bearing.
Preferably, the size of first connecting plate and the second connecting plate is identical, and the first connecting plate and the second connecting plate
Shape be rectangle.
(3) beneficial effect
The present invention provides a kind of general aviation low-altitude monitor operation aircraft, have it is following the utility model has the advantages that
(1), the general aviation low-altitude monitor operation aircraft, by handle, the second shaft, threaded post, thread barrel, movable plate,
Mutual cooperation between gag lever post, the first groove, telescopic device, crushing block, sliding slot and sliding block rotates two by using personnel
Handle, handle drive the rotation of the second shaft, and the second shaft drives threaded post rotation, threaded post to drive movable plate to move by thread barrel
It is dynamic, while movable plate drives sliding slot to move in sliding block, movable plate drives gag lever post mobile, so that it is recessed that gag lever post is caught in first
In slot, the first telescopic rod drives crushing block mobile by spring, so that first rotating shaft is fixed on second simultaneously by two crushing blocks
In groove, so that monitor ontology is preferably fixed in aircraft, it is therefore prevented that aircraft shakes in flight course
With fall off, pass through again without staff tool by monitor ontology manually twist on board the aircraft, to facilitate work
The work for making personnel improves the stability of monitor ontology.
(2), the general aviation low-altitude monitor operation aircraft, passes through electric pushrod, ratch, gear, first rotating shaft, first
Mutual cooperation between connecting plate, the second connecting plate, second bearing and 3rd bearing is led to when needing to adjust monitor angle
Operation switch, electric pushrod work are crossed, electric pushrod drives ratch rotation, and ratch is engaged with gear, so that ratch band moving gear
Rotation, while ratch drives the second telescopic rod to shorten, the second telescopic rod is moved to the left, and gear drives first rotating shaft mobile, and first
Shaft drives the rotation of monitor ontology, and when needing to go back to, by Operation switch, electric pushrod drives ratch to reset, ratch band
Moving gear rotation, while ratch drives the elongation of the second telescopic rod, first rotating shaft drives the rotation of monitor ontology, to realize prison
Being adjusted for visual organ ontology angle, is convenient to use the operation of personnel, allows to adjust the angle of monitor ontology, facilitate
Observation to all angles.
(3), the general aviation low-altitude monitor operation aircraft, by setting telescopic device, sliding slot, sliding block, first bearing,
Second bearing, 3rd bearing, fourth bearing, the first connecting plate and the second connecting plate, the first telescopic rod are driven by spring and are squeezed
Block is mobile, so that first rotating shaft is fixed in the second groove by two crushing blocks simultaneously, it can be preferably solid by monitor ontology
It is scheduled in aircraft, by setting sliding slot and sliding block, so that the second shaft drives thread barrel mobile by threaded post, thread barrel is logical
Crossing movable plate drives gag lever post mobile, while movable plate band movable slider moves in sliding slot, improves the stability of device, avoids
When moving there is a situation where Catons for movable plate, greatly improve the fluency of device, by the way that first bearing is arranged, so that
Rotating handles, it is more stable that handle drives the second shaft that can rotate in fuselage, and structure of the invention is compact, and design is closed
Reason, it is practical.
Detailed description of the invention
Fig. 1 is the schematic diagram of the section structure that the present invention faces；
Fig. 2 is the structural schematic diagram of the portion A of the present invention amplification；
Fig. 3 is the structural schematic diagram that the present invention faces.
In figure: 1 fuselage, 2 propellers, 3 horns, 4 telescopic devices, 41 first telescopic rods, 42 springs, 5 crushing blocks, 6 first
Shaft, 7 first grooves, 8 gag lever posts, 9 movable plates, 10 threaded barrels, 11 threaded posts, 12 handles, 13 first bearings, 14 second turns
Axis, 15 sliding slots, 16 sliding blocks, 17 first connecting plates, 18 electric pushrods, 19 second fixed plates, 20 monitor ontologies, 21 second axis
It holds, 22 3rd bearings, 23 gears, 24 ratch, 25 second connecting plates, 26 second telescopic rods, 27 first fixed plates, 28 the 4th axis
It holds, 29 power supplys, 30 switches, 31 second grooves, 32 pedestals.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
As shown in Figure 1-3, the present invention provides a kind of technical solution: a kind of general aviation low-altitude monitor operation aircraft, packet
Include fuselage 1, the lower surface of fuselage 1 is fixedly connected with that there are four pedestals 32, and four pedestals 32 are located at the four of 1 lower surface of fuselage
At angle, the front of fuselage 1 is fixedly connected with power supply 29, and the front of power supply 29 is fixedly connected with switch 30, the output end of power supply 29
It is electrically connected with the input terminal of switch 30, and the output end of switch 30 is electrically connected with the input terminal of electric pushrod 18, and switch 30
Model LW5D-16, by the way that switch 30 is arranged, so that staff is more convenient to the control of 18 working condition of electric pushrod,
There are two horns 3 for the upper surface setting of fuselage 1, and the surface of two horns 3 is provided with propeller 2, the left and right sides of fuselage 1
Face is clamped respectively there are two first bearing 13, by the way that first bearing 13 is arranged, so that handle 12 drives the second shaft 14 in fuselage 1
The more stable smoothness of interior rotation, avoiding handle 12, there is a situation where Catons in rotation, and divide in two first bearings 13
Tao Jie not be there are two the second shaft 14, and two mutually separate one end of the second shaft 14 are respectively fixedly connected with there are two handle 12,
And the opposite end of two the second shafts 14 is fixedly connected with mutually separate one section of two threaded posts 11 respectively, and two threaded posts 11
Surface be threadedly coupled respectively there are two thread barrel 10, rotate two handles 12 by using personnel, handle 12 drives second turn
Axis 14 rotates, and the second shaft 14 drives the rotation of threaded post 11, threaded post 11 to drive movable plate 9 mobile by thread barrel 10, simultaneously
Movable plate 9 drives sliding slot 15 to move in sliding block 16, and movable plate 9 drives gag lever post 8 mobile, so that gag lever post 8 is caught in first
In groove 7, and the opposite face of two thread barrels 10 is fixedly connected with the left and right sides of two movable plates 9 respectively, and two work
The lower surface of movable plate 9 is respectively fixedly connected with there are two sliding block 16, and two sliding blocks 16 are slidably connected in two sliding slots 15 respectively,
By setting sliding slot 15 and sliding block 16, so that the second shaft 14 drives thread barrel 10 mobile by threaded post 11, thread barrel 10 is logical
It crosses movable plate 9 and drives the movement of gag lever post 8, while movable plate 9 moves in sliding slot 15 with movable slider 16, improves the stabilization of device
Property, avoiding movable plate 9, there is a situation where Catons when moving, greatly improve the fluency of device, it is therefore prevented that movable plate
9, the rotation of gag lever post 8 and thread barrel 10 plays the role of limit, and two sliding slots 15 are provided with the first fixed plate 27
The left side of upper surface, 1 inner wall of fuselage is fixedly connected by the first fixed plate 1 with the right side of 1 inner wall of fuselage, and two activities
The opposite face of plate 9 is respectively fixedly connected with there are two gag lever post 8, and the opposite end of two gag lever posts 8 respectively with two the first grooves 7
The left and right sides of inner wall overlap, and two the first grooves 7 are provided in first rotating shaft 6, by the way that the first groove 7 is arranged, so that
First rotating shaft 6 can drive monitor ontology 20 to carry out left and right adjusting, realize the angle adjustable of monitor ontology 20, and first
The top of shaft 6 and the upper surface of 31 inner wall of the second groove overlap, and the second groove 31 is provided with the lower surface of 1 inner wall of fuselage, and
The left and right sides of first rotating shaft 6 are overlapped with the opposite face of two crushing blocks 5 respectively, by the way that crushing block 5, and crushing block 5 is arranged
Shape be it is arc-shaped, first rotating shaft 6 is fixed in the second groove 31 by two arc-shaped crushing blocks 5, so that first
Shaft 6 can rotate in the second groove 31, and first rotating shaft 6 will not fall off out of second groove 31, and two 5 phases of crushing block
Separate one end passes through two telescopic devices 4 respectively and is fixedly connected with the left and right sides of 31 inner wall of the second groove, telescopic device 4
Including the first telescopic rod 41 and the spring 42 for being socketed in 41 surface of the first telescopic rod, the left side of 1 inner wall of fuselage is stretched by first
Contracting bar 41 and spring 42 are fixedly connected with the left side of crushing block 5, and by the way that telescopic device 4 is arranged, the first telescopic rod 41 passes through bullet
Spring 42 drives crushing block 5 mobile, so that first rotating shaft 6 is fixed in the second groove 31 by two crushing blocks 5 simultaneously, thus will prison
Visual organ ontology 20 is preferably fixed in aircraft, it is therefore prevented that aircraft shakes in flight course so that monitor ontology
20 fall off, and allow the more stable rotation of first rotating shaft 6, and first rotating shaft when adjusting the position of monitor ontology 20
6 surface is socketed with fourth bearing 28, by setting second bearing 21 and 3rd bearing 22, so that first rotating shaft 6 drives monitoring
When device ontology 20 rotates, the more smooth stabilization that first rotating shaft 6 can rotate in aircraft avoids the feelings for Caton occur
Condition, fourth bearing 28 and 3rd bearing 22 are located above and below gear 23, and second bearing 21 is located at 3rd bearing 22
Lower section, and fourth bearing 28 is connected to the upper surface of the first fixed plate 27, and the surface of first rotating shaft 6 is fixedly connected with gear
23, gear 23 is engaged with ratch 24, and the right end of ratch 24 connects by the way that the left side of electric pushrod 18 and the first connecting plate 17 is fixed
It connects, the first connecting plate 17 is identical with the size of the second connecting plate 25, and the shape of the first connecting plate 17 and the second connecting plate 25 is equal
Lower surface for rectangle, the first fixed plate 27 is fixedly connected by the first connecting plate 17 with the upper surface of the second fixed plate 19, is led to
Setting ratch 24 is crossed, electric pushrod 18 works, and electric pushrod 18 drives ratch 24 mobile, and ratch 24 is engaged with gear 23, so that
Ratch 24 is rotated with moving gear 23, while ratch 24 drives the second telescopic rod 26 to shorten, and the second telescopic rod 26 is moved to the left, gear
23 drive first rotating shaft 6 to rotate, and first rotating shaft 6 drives monitor ontology 20 to rotate, and the left end of ratch 24 passes through the second telescopic rod
26 are fixedly connected with the right side of the second connecting plate 25, and the lower surface of the first fixed plate 27 is solid by the second connecting plate 25 and second
The upper surface of fixed board 19 is fixedly connected, and the upper surface of the second fixed plate 19 is connected with 3rd bearing 22, and 22 sets of 3rd bearing
It connects in the outer surface of first rotating shaft 6, the surface of first rotating shaft 6 is socketed with second bearing 21, and second bearing 21 is connected to fuselage 1
Lower surface.
In use, rotating two handles 12 by using personnel, handle 12 drives the rotation of the second shaft 14, the second shaft 14
The rotation of threaded post 11, threaded post 11 is driven to drive movable plate 9 mobile by thread barrel 10, while movable plate 9 drives sliding slot 15 to exist
It is moved in sliding block 16, movable plate 9 drives gag lever post 8 mobile, to gag lever post 8 is caught in the first groove 7, the first telescopic rod 41
Drive crushing block 5 mobile by spring 42, so that first rotating shaft 6 is fixed in the second groove 31 by two crushing blocks 5 simultaneously, from
And monitor ontology 20 is preferably fixed in aircraft, when needing to adjust monitor angle, pass through Operation switch 30, electricity
Dynamic push rod 18 works, and electric pushrod 18 drives ratch 24 mobile, and ratch 24 is engaged with gear 23, so that ratch 24 is with moving gear 23
Rotation, while ratch 24 drives the second telescopic rod 26 to shorten, the second telescopic rod 26 is moved to the left, and gear 23 drives first rotating shaft 6
Rotation, first rotating shaft 6 drives monitor ontology 20 to rotate, and when needing to go back to, by Operation switch 30, electric pushrod 18 is driven
Ratch 24 resets, and ratch 24 is rotated with moving gear 23, while ratch 24 drives the elongation of the second telescopic rod 26, and first rotating shaft 6 drives
Monitor ontology 20 rotates, to realize the adjustable of 20 angle of monitor ontology, turns off the switch 30 after usage.
Can to sum up obtain, the general aviation low-altitude monitor operation aircraft, by handle 12, the second shaft 14, threaded post 11,
It is mutual between thread barrel 10, movable plate 9, gag lever post 8, the first groove 7, telescopic device 4, crushing block 5, sliding slot 15 and sliding block 16
Cooperation rotates two handles 12 by using personnel, and handle 12 drives the rotation of the second shaft 14, and the second shaft 14 drives threaded post
11 rotations, threaded post 11 drive movable plate 9 mobile by thread barrel 10, while movable plate 9 drives sliding slot 15 to move in sliding block 16
Dynamic, it is mobile that movable plate 9 drives gag lever post 8, so that gag lever post 8 is caught in the first groove 7, the first telescopic rod 41 passes through spring 42
Drive crushing block 5 mobile, so that first rotating shaft 6 is fixed in the second groove 31 by two crushing blocks 5 simultaneously, thus by monitor
Ontology 20 is preferably fixed in aircraft, it is therefore prevented that and aircraft shakes and falls off in flight course, without
Staff passes through tool again and twists monitor ontology 20 on board the aircraft manually, to facilitate the work of staff, mentions
The high stability of monitor ontology 20.
Meanwhile the general aviation low-altitude monitor operation aircraft, pass through electric pushrod 18, ratch 24,23, first turns of gear
Mutual cooperation between axis 6, the first connecting plate 17, the second connecting plate 25, second bearing 21 and 3rd bearing 22, when needing to adjust
When monitor angle, by Operation switch 30, electric pushrod 18 works, and electric pushrod 18 drives ratch 24 mobile, ratch 24 with
Gear 23 engages, so that ratch 24 is rotated with moving gear 23, while ratch 24 drives the second telescopic rod 26 to shorten, the second telescopic rod
26 are moved to the left, and gear 23 drives first rotating shaft 6 to rotate, and first rotating shaft 6 drives monitor ontology 20 to rotate, when needs are gone back to
When, by Operation switch 30, electric pushrod 18 drives ratch 24 to reset, and ratch 24 is rotated with moving gear 23, while 24 band of ratch
Dynamic second telescopic rod 26 elongation, first rotating shaft 6 drives monitor ontology 20 to rotate, to realize 20 angle of monitor ontology
It is adjustable, it is convenient to use the operation of personnel, allows to adjust the angle of monitor ontology 20, facilitates to all angles
Observation.
Meanwhile the general aviation low-altitude monitor operation aircraft, pass through setting telescopic device 4, sliding slot 15, sliding block 16, the
One bearing 13, second bearing 21,3rd bearing 22, fourth bearing 28, the first connecting plate 17 and the second connecting plate 25, first is flexible
Bar 41 drives crushing block 5 mobile by spring 42, so that first rotating shaft 6 is fixed on the second groove 31 simultaneously by two crushing blocks 5
It is interior, monitor ontology 20 can be preferably fixed in aircraft, by setting sliding slot 15 and sliding block 16, so that the second shaft
14 drive thread barrel 10 mobile by threaded post 11, and thread barrel 10 drives gag lever post 8 mobile by movable plate 9, while movable plate 9
Band movable slider 16 moves in sliding slot 15, improves the stability of device, avoids the feelings that Caton occurs when moving for movable plate 9
Condition greatly improves the fluency of device, and by the way that first bearing 13 is arranged, so that rotating handles 12, handle 12 drives second
Shaft 14 can rotate more stable in fuselage 1, and structure of the invention is compact, and design is rationally, practical.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (8)
1. the lower surface of a kind of general aviation low-altitude monitor operation aircraft, including fuselage (1), the fuselage (1) is fixedly connected
There are four pedestal (32), and four pedestals (32) are located at the four corners of fuselage (1) lower surface, it is characterised in that: the machine
There are two horn (3) for the upper surface setting of body (1), and the surface of two horns (3) is provided with propeller (2), the fuselage
(1) left and right sides are clamped respectively there are two first bearing (13), and are respectively sleeved on two in two first bearings (13)
Second shaft (14), and two mutually separate one end of the second shaft (14) are respectively fixedly connected with there are two handle (12), and two
The opposite end of second shaft (14) is fixedly connected with mutually separate one section of two threaded posts (11) respectively, and two threaded posts (11)
Surface be threadedly coupled respectively there are two thread barrel (10), and the opposite face of two thread barrels (10) respectively with two movable plates
(9) left and right sides are fixedly connected, and the lower surface of two movable plates (9) is respectively fixedly connected with there are two sliding block (16), and
Two sliding block difference (16) are slidably connected in two sliding slots (15), and two sliding slots (15) are provided with the first fixed plate (27)
Upper surface, the left side of fuselage (1) inner wall connects by the way that the first fixed plate (1) and the right side of fuselage (1) inner wall are fixed
It connects, and the opposite face of two movable plates (9) is respectively fixedly connected with there are two gag lever post (8), and the opposite end of two gag lever posts (8)
It is overlapped respectively with the left and right sides of two the first groove (7) inner walls, and two the first grooves (7) are provided with first rotating shaft (6)
On.
2. a kind of general aviation low-altitude monitor operation aircraft according to claim 1, it is characterised in that: described first turn
The top of axis (6) and the upper surface of the second groove (31) inner wall overlap, second groove (31) is provided in fuselage (1)
The lower surface of wall, and the left and right sides of first rotating shaft (6) are overlapped with the opposite face of two crushing blocks (5) respectively, and two are squeezed
The mutually separate one end of briquetting (5) passes through two telescopic devices (4) respectively and the left and right sides of the second groove (31) inner wall are fixed
Connection, and the surface of first rotating shaft (6) is socketed with fourth bearing (28), and fourth bearing (28) is connected to the first fixed plate (27)
Upper surface.
3. a kind of general aviation low-altitude monitor operation aircraft according to claim 1, it is characterised in that: described first turn
The surface of axis (6) is fixedly connected with gear (23), and the gear (23) is engaged with ratch (24), and the right end of the ratch (24) is logical
It crosses electric pushrod (18) to be fixedly connected with the left side of the first connecting plate (17), the lower surface of first fixed plate (27) passes through
First connecting plate (17) is fixedly connected with the upper surface of the second fixed plate (19), and the left end of the ratch (24) is flexible by second
Bar (26) is fixedly connected with the right side of the second connecting plate (25), and the lower surface of first fixed plate (27) passes through the second connection
Plate (25) is fixedly connected with the upper surface of the second fixed plate (19), and the upper surface of the second fixed plate (19) is connected with 3rd bearing
(22), and 3rd bearing (22) is socketed in the outer surfaces of first rotating shaft (6), and the surface of the first rotating shaft (6) is socketed with second
Bearing (21), and second bearing (21) is connected to the lower surface of fuselage (1).
4. a kind of general aviation low-altitude monitor operation aircraft according to claim 1, it is characterised in that: the fuselage
(1) front is fixedly connected with power supply (29), and the front of the power supply (29) is fixedly connected with switch (30).
5. a kind of general aviation low-altitude monitor operation aircraft according to claim 4, it is characterised in that: the power supply
(29) output end is electrically connected with the input terminal of switch (30), and switchs the output end of (30) and the input terminal of electric pushrod (18)
Electrical connection, and switch the model LW5D-16 of (30).
6. a kind of general aviation low-altitude monitor operation aircraft according to claim 2, it is characterised in that: the flexible dress
(4) are set to include the first telescopic rod (41) and be socketed in the spring (42) on the first telescopic rod (41) surface, fuselage (1) inner wall
Left side is fixedly connected by the first telescopic rod (41) and spring (42) with the left side of crushing block (5).
7. a kind of general aviation low-altitude monitor operation aircraft according to claim 3, it is characterised in that: the 4th axis
It holds (28) and 3rd bearing (22) is located above and below gear (23), the second bearing (21) is located at 3rd bearing
(22) lower section.
8. a kind of general aviation low-altitude monitor operation aircraft according to claim 1, it is characterised in that: described first connects
Fishplate bar (17) is identical with the size of the second connecting plate (25), and the first connecting plate (17) and the shape of the second connecting plate (25) are
Rectangle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810524475.9A CN108974379A (en) | 2018-05-28 | 2018-05-28 | A kind of general aviation low-altitude monitor operation aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810524475.9A CN108974379A (en) | 2018-05-28 | 2018-05-28 | A kind of general aviation low-altitude monitor operation aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108974379A true CN108974379A (en) | 2018-12-11 |
Family
ID=64542146
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810524475.9A Pending CN108974379A (en) | 2018-05-28 | 2018-05-28 | A kind of general aviation low-altitude monitor operation aircraft |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112550747A (en) * | 2021-01-19 | 2021-03-26 | 广西光谱空间信息科技有限公司 | Self-locking anti-drop low-altitude flight unmanned aerial vehicle integrating aerial photography instrument and radar device |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN206456568U (en) * | 2016-12-21 | 2017-09-01 | 赵普 | A kind of environmental monitoring unmanned plane |
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| CN207374691U (en) * | 2017-11-03 | 2018-05-18 | 杭州鼎翼智能科技有限公司 | A kind of unmanned plane camera fixing device |
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| CN206456568U (en) * | 2016-12-21 | 2017-09-01 | 赵普 | A kind of environmental monitoring unmanned plane |
| CN206813338U (en) * | 2017-05-06 | 2017-12-29 | 北京速测信息科技有限公司 | Disk coal instrument is installed on the fixing device on unmanned plane |
| CN207292460U (en) * | 2017-05-24 | 2018-05-01 | 重庆洪吉航空遥感技术研究院有限公司 | A kind of airborne camera head fixing device of air remote sensing |
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| CN207347956U (en) * | 2017-08-31 | 2018-05-11 | 广东清泉建设工程有限公司 | A kind of town road alarming device |
| CN207374691U (en) * | 2017-11-03 | 2018-05-18 | 杭州鼎翼智能科技有限公司 | A kind of unmanned plane camera fixing device |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN112550747A (en) * | 2021-01-19 | 2021-03-26 | 广西光谱空间信息科技有限公司 | Self-locking anti-drop low-altitude flight unmanned aerial vehicle integrating aerial photography instrument and radar device |
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