CN105035300B - Unmanned plane suspension system - Google Patents
Unmanned plane suspension system Download PDFInfo
- Publication number
- CN105035300B CN105035300B CN201510533966.6A CN201510533966A CN105035300B CN 105035300 B CN105035300 B CN 105035300B CN 201510533966 A CN201510533966 A CN 201510533966A CN 105035300 B CN105035300 B CN 105035300B
- Authority
- CN
- China
- Prior art keywords
- frame
- control panel
- fixed mount
- shock absorber
- flight control
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 239000000725 suspension Substances 0.000 title claims abstract description 18
- 230000035939 shock Effects 0.000 claims abstract description 43
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims abstract description 41
- 239000006096 absorbing agent Substances 0.000 claims abstract description 40
- 239000000463 material Substances 0.000 claims abstract description 9
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims abstract description 7
- 239000000741 silica gel Substances 0.000 claims abstract description 7
- 229910002027 silica gel Inorganic materials 0.000 claims abstract description 7
- 238000009434 installation Methods 0.000 claims description 6
- 108091092878 Microsatellite Proteins 0.000 abstract description 2
- 230000003139 buffering effect Effects 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 238000013016 damping Methods 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Vibration Prevention Devices (AREA)
- Toys (AREA)
Abstract
A kind of unmanned plane suspension system, including the frame for installing propeller, and flight control panel fixed mount, it is characterized in that, being provided between the frame and flight control panel fixed mount is used to connect the frame and flight control panel fixed mount and the shock absorber strut with shock-absorbing function, the shock absorber strut is the hollow circular cylinder of silica gel material, shock absorber strut isolates the frame with flight control panel fixed mount, is also equipped with providing power for unmanned plane on the flight control panel fixed mount and has the battery of weight balance function.This unmanned plane suspension system, using the shock absorber strut connection frame and flight control panel fixed mount of silica gel material, buffering effect is excellent, using, as balancing weight, alleviating overall weight from charged pool, and suitable for the Small and micro-satellite to weight sensitive.
Description
Technical field
The present invention relates to a kind of shock absorbing apparatus, more particularly to a kind of unmanned plane shock absorbing apparatus.
Background technology
During existing large-scale unmanned plane shock-absorbing generally sponge is used for damping material, and iron block or lead enter
The shock-absorbing design of row counterweight, and SUAV then lacks shock-absorbing design, is directly consolidated frame and flight control system PCB
It is fixed.The suspension system of large-scale unmanned plane is not suitable for SUAV, and does shock-absorbing, counterweight in flight controller inside modules
Block can increase unmanned plane overall weight, therefore not be suitable for the MAV of weight sensitive.
The content of the invention
Small and micro-satellite is not suitable for it for existing unmanned plane suspension system, other balancing weights are added in inside to be increased
The problem of overall weight, the present invention proposes a kind of unmanned plane suspension system, and row buffering is entered by shock absorber strut, and will be self-contained
Battery as shock resistance block, not only shock-proof effect is good, and overall weight is also reduced.
To achieve these goals, technical scheme is as follows：
A kind of unmanned plane suspension system, including for installing the frame of propeller, and flight control panel fixed mount, it is described
Being provided between frame and flight control panel fixed mount is used to connect the frame with flight control panel fixed mount and with damping work(
The shock absorber strut of energy, the shock absorber strut isolates the frame with flight control panel fixed mount, and the shock absorber strut both ends are equipped with
Around the shock absorber strut external cylindrical surface neck of one week, it is equipped with the frame and flight control panel fixed mount on thickness direction
Through the frame and the hole clipping of flight control panel fixed mount, the shock absorber strut is consolidated with frame and shock absorber strut with flight control panel
Determine to be attached with hole clipping fastening by neck between frame.
Further, it is also equipped with providing power and with weight balance function for unmanned plane on the flight control panel fixed mount
Battery, there is not a segment distance contact interval to the battery surface with frame surface.
Further, the frame includes multiple propeller installation portions, and the multiple propeller installation portion is in regular hexagon
Stretch out, the frame main body is that the hole clipping in engraved structure, the frame is located at central rack.
Further, on the flight control panel fixed mount be used for install shock absorber strut hole clipping be arranged at flight control panel consolidate
Determine the stage casing edge of frame.
Further, the shock absorber strut is silica gel material.
Further, the shock absorber strut is hollow circular cylinder.
Further, the quantity of the shock absorber strut is 4.
Beneficial effect of the present invention：This unmanned plane suspension system, uses silica gel material between frame and flight control panel fixed mount
Battery is installed on flight control panel fixed mount and used as balancing weight as shock-absorbing part by the shock absorber strut of material so that
This unmanned plane suspension system has shockproof buffer effect good, the characteristics of overall weight is light.
Brief description of the drawings
Fig. 1 is overall structure diagram of the invention；
Fig. 2 is main view dimensional structure diagram of the invention；
Fig. 3 is framework accessory structural representation of the invention；
Fig. 4 is shock absorber strut design of part schematic diagram of the invention；
Fig. 5 is flight control panel fixed mount part schematic diagram of the invention.
In accompanying drawing, it is as follows that each label represents list of parts：Frame 1, shock absorber strut 2, flight control panel fixed mount 3, battery 4,
Propeller installation portion 11, neck 21, hole clipping 22.
Embodiment
The present invention is further described in detail below by specific embodiment and with reference to accompanying drawing.
Unmanned plane suspension system as shown in Figure 1 and Figure 2, including consolidate for installing the frame 1 of propeller, flight control panel
Determine frame 3, multiple shock absorber struts 2 are provided between the frame 1 and flight control panel fixed mount 3, as shown in figure 4, the shock absorber strut 2 is
The hollow circular cylinder of silica gel material, the quantity of shock absorber strut 2 is 4, and 6, or other quantity, such design are alternatively certainly
So that shock absorber strut 2 has good damping effect, the both ends of shock absorber strut 2, which are equipped with, surround 2 external cylindrical surface of shock absorber strut one week
Neck 21；As shown in Fig. 3, Fig. 5, the main body of frame 1 is engraved structure, so that the overall weight of frame 1 is lighter, frame
1 is provided with multiple propeller installation portions 11, and the multiple propeller installation portion 11 stretches out in regular hexagon shape, the frame
1 middle part is provided with multiple hole clippings 22 matched with neck 21 on shock absorber strut 2, and described one end of shock absorber strut 2 is fastened and connected with frame 1；
The flight control panel fixed mount 3 is also engraved structure, and edge matches provided with the multiple and neck 21 of shock absorber strut 2 in the middle
Hole clipping 22, the other end of shock absorber strut 2 is fastened and connected with flight control panel fixed mount 3, and the frame 1 and flight control panel are fixed
Hole clipping 22 runs through the frame 1 and flight control panel fixed mount 3 in a thickness direction on frame 3, and the shock absorber strut 2 is by the machine
Frame 1 is isolated with flight control panel fixed mount 3, and retains certain interval between the flight control panel fixed mount 3 and frame 1
（About 1mm）So that control panel fixed mount 3 can freedom and flexibility movement so as to absorbing vibrations, while so that unmanned plane landed
Flight control panel fixed mount 3 has enough buffer distances in journey.
It is also equipped with providing power for unmanned plane on the flight control panel fixed mount 3 and there is the battery of weight balance function
4, there is not a segment distance contact interval to the lower surface of battery 4 with frame surface so that control panel fixed mount 3 being capable of freedom and flexibility
Movement is so as to absorb vibrations, while also ensuring that battery 4 does not collide frame 1 in unmanned plane descent.
This unmanned plane suspension system, is carried out frame 1 and flight control panel fixed mount 3 using the shock absorber strut 2 of silica gel material
Every sky connection, the battery carried is installed on to flight control panel fixed mount 3 and used as balancing weight so that this unmanned plane shock-absorbing system
System for traditional suspension system, overall weight light the characteristics of good with shock-proof effect, and suitable for microminiature nobody
Machine, applicability is high.
Claims (5)
1. a kind of unmanned plane suspension system, including for installing the frame (1) of propeller, and flight control panel fixed mount (3),
Characterized in that, being provided between the frame (1) and flight control panel fixed mount (3) is used to be connected the frame (1) and flight
Control panel fixed mount (3) and the shock absorber strut (2) with shock-absorbing function, the shock absorber strut (2) control the frame (1) with flight
Plate fixed mount (3) is isolated, and shock absorber strut (2) both ends are equipped with around the shock absorber strut external cylindrical surface neck of one week
(21), it is equipped with the frame (1) and flight control panel fixed mount (3) on thickness direction through the frame (1) and flight
The hole clipping (22) of control panel fixed mount (3), the shock absorber strut (2) is fixed with frame (1) and shock absorber strut (2) with flight control panel
It is fastened and connected between frame (3) by neck (21) with hole clipping (22)；
It is also equipped with providing power for unmanned plane on the flight control panel fixed mount (3) and there is the battery (4) of weight balance function,
There is not a segment distance on battery (4) surface in contact interval with frame (1) surface；The frame (1) is pacified including multiple propellers
Dress portion (11), the multiple propeller installation portion (11) stretches out in regular hexagon, and frame (1) main body is hollow out knot
Hole clipping (22) on structure, the frame (1) is located at central rack.
2. unmanned plane suspension system according to claim 1, it is characterised in that on the flight control panel fixed mount (3)
The stage casing edge of flight control panel fixed mount (3) is arranged at for installing the hole clipping (22) of shock absorber strut (2).
3. unmanned plane suspension system according to claim 1, it is characterised in that the shock absorber strut (2) is silica gel material.
4. unmanned plane suspension system according to claim 1, it is characterised in that the shock absorber strut (2) is hollow circular cylinder.
5. unmanned plane suspension system according to claim 1, it is characterised in that the quantity of the shock absorber strut (2) is 4.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510533966.6A CN105035300B (en) | 2015-08-27 | 2015-08-27 | Unmanned plane suspension system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510533966.6A CN105035300B (en) | 2015-08-27 | 2015-08-27 | Unmanned plane suspension system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105035300A CN105035300A (en) | 2015-11-11 |
| CN105035300B true CN105035300B (en) | 2017-09-19 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510533966.6A Active CN105035300B (en) | 2015-08-27 | 2015-08-27 | Unmanned plane suspension system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105035300B (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107074376B (en) * | 2016-05-26 | 2019-02-26 | 深圳市大疆创新科技有限公司 | The mounting device and unmanned vehicle of motion sensor |
| CN107264767A (en) * | 2017-06-02 | 2017-10-20 | 上海交通大学 | A kind of rotor wing unmanned aerial vehicle of Novel lightweight six |
| CN107352039A (en) * | 2017-07-18 | 2017-11-17 | 歌尔股份有限公司 | Unmanned plane and its shooting shock buffering mechanism |
| CN108710348B (en) * | 2018-05-14 | 2024-03-26 | 西安工业大学 | Unmanned aerial vehicle crowd control system and unmanned aerial vehicle equipment thereof |
Citations (8)
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|---|---|---|---|---|
| CN203854854U (en) * | 2014-05-29 | 2014-10-01 | 金陵科技学院 | Rotary wing type unmanned plane with damping landing gear |
| CN204184578U (en) * | 2014-10-14 | 2015-03-04 | 广东电网公司江门供电局 | A kind of charged aircraft device of unmanned plane searching line defct and hidden danger |
| CN204236774U (en) * | 2014-11-25 | 2015-04-01 | 南京机电职业技术学院 | Rotary wind type unmanned plane is used in a kind of transport |
| CN204250368U (en) * | 2014-11-14 | 2015-04-08 | 北华航天工业学院 | A kind of mini quadrotor of Intelligent aerial photography |
| CN204279940U (en) * | 2014-11-05 | 2015-04-22 | 成都盛世普益科技有限公司 | A kind of many rotor wing unmanned aerial vehicles device |
| CN204527660U (en) * | 2015-02-13 | 2015-08-05 | 湖北大秀天域科技发展有限公司 | Many rotor wing unmanned aerial vehicles |
| CN204527625U (en) * | 2015-02-13 | 2015-08-05 | 湖北大秀天域科技发展有限公司 | Multifunctional individual unmanned plane |
| CN205059989U (en) * | 2015-08-27 | 2016-03-02 | 深圳市恩孚电子科技有限公司 | Unmanned aerial vehicle system of moving away to avoid possible earthquakes |
-
2015
- 2015-08-27 CN CN201510533966.6A patent/CN105035300B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203854854U (en) * | 2014-05-29 | 2014-10-01 | 金陵科技学院 | Rotary wing type unmanned plane with damping landing gear |
| CN204184578U (en) * | 2014-10-14 | 2015-03-04 | 广东电网公司江门供电局 | A kind of charged aircraft device of unmanned plane searching line defct and hidden danger |
| CN204279940U (en) * | 2014-11-05 | 2015-04-22 | 成都盛世普益科技有限公司 | A kind of many rotor wing unmanned aerial vehicles device |
| CN204250368U (en) * | 2014-11-14 | 2015-04-08 | 北华航天工业学院 | A kind of mini quadrotor of Intelligent aerial photography |
| CN204236774U (en) * | 2014-11-25 | 2015-04-01 | 南京机电职业技术学院 | Rotary wind type unmanned plane is used in a kind of transport |
| CN204527660U (en) * | 2015-02-13 | 2015-08-05 | 湖北大秀天域科技发展有限公司 | Many rotor wing unmanned aerial vehicles |
| CN204527625U (en) * | 2015-02-13 | 2015-08-05 | 湖北大秀天域科技发展有限公司 | Multifunctional individual unmanned plane |
| CN205059989U (en) * | 2015-08-27 | 2016-03-02 | 深圳市恩孚电子科技有限公司 | Unmanned aerial vehicle system of moving away to avoid possible earthquakes |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105035300A (en) | 2015-11-11 |
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