CN208233380U - A kind of support plate applied to unmanned plane - Google Patents
A kind of support plate applied to unmanned plane Download PDFInfo
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- CN208233380U CN208233380U CN201820135120.6U CN201820135120U CN208233380U CN 208233380 U CN208233380 U CN 208233380U CN 201820135120 U CN201820135120 U CN 201820135120U CN 208233380 U CN208233380 U CN 208233380U
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- unmanned plane
- support plate
- support frame
- host
- plate
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Abstract
The utility model discloses a kind of support plates applied to unmanned plane, its structure includes unmanned machine host, image headstock, camera, support frame, support plate, host cap, fixed screw, flight support frame, electric motor, shaft, mounting head, propeller, fixed screw, damper, camera shooting headstock insertion is installed on unmanned machine host, camera and the camera shooting same axle center of headstock, support plate is equipped with inside support frame, fixed screw is threadedly coupled with host cap, flight support frame is mutually welded with unmanned machine host, shaft and the same axle center of electric motor, a kind of support plate applied to unmanned plane of the utility model, structure is equipped with damper, when unmanned plane drops to ground, vibration is passed to the piston spring above vibration damper plate first and carries out preliminary damping by rubber base, vibration is transferred again to spring by moving up vibration damper plate with piston valve again Secondary shock-absorbing is carried out, the jerk power on when unmanned plane lands and ground is greatly reduced, ensure that unmanned plane is hardly damaged.
Description
Technical field
The utility model is a kind of support plate applied to unmanned plane, belongs to air vehicle technique field.
Background technique
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, without cockpit on machine, but the equipment such as automatic pilot, presetting apparatus, signal pickup assembly are installed,
On ground, naval vessels or machine tool remote control station personnel are by equipment such as radars, are tracked, positioned to it, is remotely controlled, telemetering and number pass
It is defeated, it can take off as conventional airplane under wireless remotecontrol or be launched with booster rocket, can also be taken to by machine tool in the air
Launch flight.
Prior art discloses application No. is a kind of 201520614418.1 support plates applied to unmanned plane, including
Pillar, the first plate, the second plate and elastic parts, the support plate applied to unmanned plane is by connecting holder and unmanned plane flexibility
It connects, but the support plate damping effect of the prior art unmanned plane is bad, when unmanned plane landing and the impact force on ground is larger,
It is easily damaged unmanned plane.
Utility model content
In view of the deficienciess of the prior art, the utility model aim is to provide a kind of support plate applied to unmanned plane,
Bad with the support plate damping effect for solving prior art unmanned plane, when unmanned plane landing and the impact force on ground is larger, holds
The problem of unmanned plane easy to damage.
To achieve the goals above, the utility model is achieved through the following technical solutions: a kind of be applied to nobody
The support plate of machine, structure include unmanned machine host, camera shooting headstock, camera, support frame, support plate, host cap, fixed spiral shell
Silk, flight support frame, electric motor, shaft, mounting head, propeller, fixed screw, damper, the camera shooting headstock insertion peace
Loaded on unmanned machine host, the camera and the camera shooting same axle center of headstock, support frame as described above inside is equipped with support plate, described solid
Determine screw to be threadedly coupled with host cap, the flight support frame is mutually welded with unmanned machine host, and the shaft and electric motor are same
One axle center, the mounting head are integrated with propeller, and the fixed screw is connect with shaft thread, the support plate bottom
End fit with damper top, the damper include fixed plate, protective shell, spring, piston tube, piston spring, piston valve,
Strut, vibration damper plate, rubber base, the protective shell top are mutually welded with fixed plate bottom end, and the spring insertion is installed on fixed plate
On, the piston tube top fits with fixed plate bottom end, and piston spring, the piston valve and work are equipped with inside the piston tube
Plug manages same axle center, is equipped with strut below the piston valve, and the strut is mutually welded with vibration damper plate, the rubber base insertion installation
In on protective shell.
Further, support frame as described above is mutually welded with unmanned machine host, and the host cap insertion is installed on unmanned machine host
On.
Further, the electric motor insertion is installed on flight support frame, and the mounting head insertion is installed on shaft
On.
Further, the fixed plate insertion is installed in support plate.
Further, the support plate is long 18CM, wide 18CM, the cuboid of high 2.5CM.
Further, the support plate is stainless steel material, light weight, long service life.
Further, the host cap is aluminum alloy material, and hardness is high, is unlikely to deform.
Beneficial effect
A kind of support plate applied to unmanned plane of the utility model, structure is equipped with damper, when unmanned plane drops to ground
When face, vibration is passed to the piston spring above vibration damper plate first and carries out preliminary damping by rubber base, then by moving up with piston valve
Vibration is transferred again to spring and carries out secondary shock-absorbing by vibration damper plate, greatly reduces the jerk on when unmanned plane lands and ground
Power ensure that unmanned plane is hardly damaged.
Detailed description of the invention
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model
Sign, objects and advantages will become more apparent upon:
Fig. 1 is a kind of structural schematic diagram of the support plate applied to unmanned plane of the utility model；
Fig. 2 is the cross section structure schematic diagram of the utility model damper.
In figure: unmanned machine host -1, camera -3, support frame -4, support plate -5, host cap -6, is fixed camera shooting headstock -2
Screw -7, flight support frame -8, electric motor -9, shaft -10, mounting head -11, propeller -12, fixed screw -13, damping
Device -14, fixed plate -1401, protective shell -1402, spring -1403, piston tube -1404, piston spring -1405, piston valve -
1406, strut -1407, vibration damper plate -1408, rubber base -1409.
Specific embodiment
To be easy to understand the technical means, creative features, achievement of purpose, and effectiveness of the utility model, below
In conjunction with specific embodiment, the utility model is further described.
Fig. 1, Fig. 2 are please referred to, the utility model provides a kind of support plate technical solution applied to unmanned plane: its structure packet
Include unmanned machine host 1, camera shooting headstock 2, camera 3, support frame 4, support plate 5, host cap 6, fixed screw 7, flight support frame
8, electric motor 9, shaft 10, mounting head 11, propeller 12, fixed screw 13, damper 14, the insertion of camera shooting headstock 2 peace
Loaded on unmanned machine host 1, the camera 3 and the camera shooting same axle center of headstock 2 are equipped with support plate 5 inside support frame as described above 4,
The fixed screw 7 is threadedly coupled with host cap 6, and the flight support frame 8 is welded with unmanned 1 phase of machine host, the shaft 10
With the same axle center of electric motor 9, the mounting head 11 is integrated with propeller 12, the fixed screw 13 and shaft 10
It is threadedly coupled, 5 bottom end of support plate fits with 14 top of damper, and the damper 14 includes fixed plate 1401, protection
Shell 1402, spring 1403, piston tube 1404, piston spring 1405, piston valve 1406, strut 1407, vibration damper plate 1408, rubber base
1409,1402 top of protective shell is mutually welded with 1401 bottom end of fixed plate, and the insertion of spring 1403 is installed on fixed plate
On 1401,1404 top of piston tube fits with 1401 bottom end of fixed plate, and piston bullet is equipped with inside the piston tube 1404
Spring 1405, the piston valve 1406 and the same axle center of piston tube 1404 are equipped with strut 1407 below the piston valve 1406, described
Strut 1407 and 1408 phase of vibration damper plate are welded, and the insertion of rubber base 1409 is installed on protective shell 1402, support frame as described above 4 with
Unmanned 1 phase of machine host welding, the insertion of host cap 6 are installed on unmanned machine host 1, and the insertion of electric motor 9 is installed on
On flight support frame 8, the insertion of mounting head 11 is installed in shaft 10, and the insertion of fixed plate 1401 is installed on support plate 5
On, the support plate 5 be long 18CM, wide 18CM, the cuboid of high 2.5CM, the support plate 5 be stainless steel material, light weight,
Long service life, the host cap 6 are aluminum alloy material, and hardness is high, is unlikely to deform.
Camera 3 described in this patent is also known as camera computer, computer eye, electronic eyes etc., is a kind of video input apparatus,
Widely applied to video conference, tele-medicine and real time monitoring etc., common people can also be each other by camera
Image, the talk for having sound and communication are carried out in network, in addition, people can also be used for the number of current various prevalences
Image, sound processing etc., the spring 1403 is a kind of using the elastic machine components come work, zero made of elastic material
Deformation occurs under external force for part, restores to the original state again after removing external force, also makees " spring ", be generally made of spring steel, spring
The complicated multiplicity of type mainly have helical spring, scroll spring, flat spring, heterotypic spring etc. by shape point.
Rotate in use, controlling the electric motor 9 on unmanned machine host 1 by unmanned aerial vehicle (UAV) control device, so that spiral shell
The rotation rotation of paddle 12 is flown to sky with unmanned plane and is taken photo by plane using camera 3, when unmanned plane drops to ground, rubber base
Vibration is passed to the piston spring 1405 of the top of vibration damper plate 1408 first by 1409 carries out preliminary damping, then by with piston valve 1406
It moves up vibration damper plate 1408 and vibration is transferred again to the progress secondary shock-absorbing of spring 1403, greatly reduce when unmanned plane lands and ground
The impact force in face, it is not easy to damage unmanned plane.
The utility model solve prior art unmanned plane support plate damping effect it is bad, when unmanned plane landing when and ground
Impact force it is larger, the problem of being easily damaged unmanned plane, the utility model is combined with each other by above-mentioned component, and structure is equipped with
Damper, when unmanned plane drops to ground, vibration is passed to the piston spring above vibration damper plate first and carried out just by rubber base
Damping is walked, then vibration is transferred again to spring progress secondary shock-absorbing by moving up vibration damper plate with piston valve, greatly reduces nobody
Machine land when and ground jerk power, ensure that unmanned plane is hardly damaged.
The basic principles and main features of the present invention and the advantages of the present invention have been shown and described above, for
For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this
In the case where the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute
Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent elements of the claims
All changes are embraced therein.It should not treat any reference in the claims as limiting related right
It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiments being understood that.
Claims (5)
1. a kind of support plate applied to unmanned plane, it is characterised in that: its structure includes unmanned machine host (1), camera shooting headstock
(2), camera (3), support frame (4), support plate (5), host cap (6), fixed screw (7), flight support frame (8), electronic horse
Up to (9), shaft (10), mounting head (11), propeller (12), fixed screw (13), damper (14), the camera shooting headstock (2)
Insertion is installed on unmanned machine host (1), the camera (3) and camera shooting headstock (2) same axle center, in support frame as described above (4)
Portion is equipped with support plate (5), and the fixed screw (7) is threadedly coupled with host cap (6), the flight support frame (8) and unmanned plane
Host (1) mutually welds, the shaft (10) and electric motor (9) same axle center, and the mounting head (11) is with propeller (12)
Integral structure, the fixed screw (13) are threadedly coupled with shaft (10), and support plate (5) bottom end and damper (14) are pushed up
End fits, the damper (14) include fixed plate (1401), protective shell (1402), spring (1403), piston tube (1404),
Piston spring (1405), piston valve (1406), strut (1407), vibration damper plate (1408), rubber base (1409), the protective shell
(1402) top is mutually welded with fixed plate (1401) bottom end, and spring (1403) insertion is installed on fixed plate (1401), institute
It states piston tube (1404) top to fit with fixed plate (1401) bottom end, piston spring is equipped with inside the piston tube (1404)
(1405), the piston valve (1406) and piston tube (1404) same axle center, piston valve (1406) lower section are equipped with strut
(1407), the strut (1407) is mutually welded with vibration damper plate (1408), and rubber base (1409) insertion is installed on protective shell
(1402) on.
2. a kind of support plate applied to unmanned plane according to claim 1, it is characterised in that: support frame as described above (4) with
Unmanned machine host (1) is mutually welded, and host cap (6) insertion is installed on unmanned machine host (1).
3. a kind of support plate applied to unmanned plane according to claim 1, it is characterised in that: the electric motor (9)
Insertion is installed on flight support frame (8), and mounting head (11) insertion is installed on shaft (10).
4. a kind of support plate applied to unmanned plane according to claim 1, it is characterised in that: the fixed plate (1401)
Insertion is installed on support plate (5).
5. a kind of support plate applied to unmanned plane according to claim 1, it is characterised in that: the support plate (5) is
Long 18CM, wide 18CM, the cuboid of high 2.5CM.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820135120.6U CN208233380U (en) | 2018-01-26 | 2018-01-26 | A kind of support plate applied to unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820135120.6U CN208233380U (en) | 2018-01-26 | 2018-01-26 | A kind of support plate applied to unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208233380U true CN208233380U (en) | 2018-12-14 |
Family
ID=64578600
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820135120.6U Active CN208233380U (en) | 2018-01-26 | 2018-01-26 | A kind of support plate applied to unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208233380U (en) |
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2018
- 2018-01-26 CN CN201820135120.6U patent/CN208233380U/en active Active
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| GR01 | Patent grant | ||
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| CP03 | Change of name, title or address |
Address after: No. 76-45, Shenbei Road, Shenbei New District, Shenyang City, Liaoning Province 110000 Patentee after: Liaoning Dazhuang UAV Technology Co.,Ltd. Address before: 110122 No. 76-43, Shenbei Road, Shenbei New District, Shenyang City, Liaoning Province (Gate A) Patentee before: LIAONING ZHUANGLONG UNMANNED AERIAL VEHICLE TECHNOLOGY Co.,Ltd. |