CN110001938A - A kind of support protection equipment for unmanned plane - Google Patents
A kind of support protection equipment for unmanned plane Download PDFInfo
- Publication number
- CN110001938A CN110001938A CN201910273598.4A CN201910273598A CN110001938A CN 110001938 A CN110001938 A CN 110001938A CN 201910273598 A CN201910273598 A CN 201910273598A CN 110001938 A CN110001938 A CN 110001938A
- Authority
- CN
- China
- Prior art keywords
- mounting base
- unmanned plane
- earth
- fixedly connected
- inclined plate
- 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.)
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Classifications
-
- 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
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The present invention relates to unmanned plane correlative technology fields, and disclose a kind of support protection equipment for unmanned plane, including mounting base, ontology is installed on the inside of mounting base, the bottom four corners of mounting base are fixedly connected to pillar, the bottom of four pillars is fixedly connected to hinged seat, the hinged ball of four hinged seat bottoms is fixedly connected to the inclined plate that contacts to earth, the plane of inclined plate of contacting to earth and the joining place on inclined-plane are connected with ball, the bottom four corners of mounting base offer through-hole, connecting spring is fixedly connected between hinged seat and the inclined-plane for the inclined plate that contacts to earth, the inside bottom rectangle of mounting base offers mounting groove.Equipment is protected in the support for being used for unmanned plane; the effective back stretch for preventing connecting spring from carrying out reset generation causes the secondary damage of ontology; the closing through slot part for contacting the air bag corresponding to inclined plate that contacts to earth on ground is expanded to gap section, and then effectively protects to the contact impact point part of unmanned plane.
Description
Technical field
The present invention relates to unmanned plane correlative technology field, equipment is protected in specially a kind of support for unmanned plane.
Background technique
With the development of society, science and technology is constantly progressive, unmanned plane using more and more extensive, unmanned plane universal so that
More and more people it is carried out using, but unmanned plane has certain uncontrollability in use, generate when unmanned plane therefore
For barrier when falling, the environment that falls is uncontrollable, and when unmanned plane falls is difficult stable landing, so that the landing stress shock point of unmanned plane
It is uncontrollable, easily cause the damage of components of drone body stress shock point to a certain extent, and the buffering of existing unmanned plane
Mechanism generally uses the buffering method of spring, and the rebound after spring or elastic mechanism landing easily causes the secondary damage of unmanned plane
Wound, it is therefore desirable to which the mechanism that one kind can protect stress shock point of the unmanned plane when falling reduces shock of a fall pair
The damage of unmanned plane.
Summary of the invention
The impact force for solving the problems, such as that stress shock point of the unmanned plane when falling is born easily causes unmanned plane to damage.
Equipment, including mounting base are protected in a kind of support for unmanned plane, are equipped with ontology on the inside of the mounting base, institute
The bottom four corners for stating mounting base are fixedly connected to pillar, and the bottom of four pillars is fixedly connected to hinged seat, and four hinged
The hinged ball of seat bottom is fixedly connected to the inclined plate that contacts to earth, and the plane of the inclined plate that contacts to earth and the joining place on inclined-plane are connected with
Ball, the bottom four corners of the mounting base offer through-hole, are fixedly connected between the hinged seat and the inclined-plane for the inclined plate that contacts to earth
There is connecting spring, the inside bottom rectangle of the mounting base offers mounting groove, and the inside bottom of four mounting grooves is solid
Dingan County is equipped with resilient mounting, passes through rope between the incline apex and corresponding resilient mounting of the inclined plate that contacts to earth described in four
It is fixedly connected, the side that four resilient mountings are connected with corresponding rope passes through pin shaft and is connected with activity
Hook is connected between the upper surface that the resilient mounting is mutually connected with movable hook by torsional spring, the inside bottom of the mounting base
Portion quadrangle is fixedly installed with positive stop hook, and the side that is bent in an arc shape of the positive stop hook is in contact with the bending side of movable hook, institute
The bottom surface quadrangle for stating ontology passes through flexible connector respectively and is connected with the top surface of four resilient mountings, the peace
The bottom middle position of dress seat is fixedly installed with helium tank, and the exhaust pipe of the helium tank runs through the bottom surface of mounting base and prolongs
The inside of mounting base is extended to, electrically-controlled valve is fixedly connected on the exhaust pipe of the helium tank, the bottom of the ontology is bonded with gas
The exhaust pipe end of capsule, the helium tank is fixedly connected with the air guide port of air bag, is opened up on the air bag there are four closing through slot,
Four closing through slots are arranged in a one-to-one correspondence with four resilient mountings respectively, and the right side of the mounting base is fixedly installed with
Control panel.
Preferably, the connection relationship between the control panel and electrically-controlled valve and ontology is to be electrically connected, the control
Panel uses wireless signal receiver.
Preferably, the rope uses micro-elasticity rope, and four ropes extend through corresponding through-hole.
Preferably, the resilient mounting and flexible connector are all made of 65Mn spring steel material, and movable hook uses
60sicr spring steel material, the positive stop hook use 304 stainless steel materials.
Preferably, it is contacted between the side wall of the ontology and the inner sidewall of mounting base by the way that rubber strip is soft, the ontology
There are gaps between bottom and the inside bottom of mounting base.
Preferably, the original state of the connecting spring is confined state, and the connecting spring is oblique with the inclined plate that contacts to earth
Face is to be mutually connected vertically.
Preferably, the helium tank uses high pressure helium gas cylinder, stores helium liquid in helium tank.
Compared with prior art:
(1), support protection equipment for being used for unmanned plane, by the way that mounting base, ontology, the inclined plate that contacts to earth, ball, connecting spring is arranged
It cooperates with rope, when the device is in use, unmanned plane lands under runaway condition, and four below mounting base contact to earth inclined plate
Planar section contacts ground first, one or more contact ground in four inclined plates that contact to earth, so that impact force at contact passes through touching
Ground inclined plate is transmitted, and the impact force for the inclined plate that contacts to earth makes the hinged ball carry out activity of hinged seat, so that the inclined plate and hinged of contacting to earth
Seat between angle change, and connecting spring contacted to earth inclined plate inclined-plane carry out recovery stretch, effectively to mounting base
The impact force that contact impact point is born is buffered, and the inclined plate that contacts to earth pull corresponding connection rope to resilient mounting into
Row pulls, and resilient mounting is connected rope and is pulled, and resilient mounting is pulled deformation and bends downward, elasticity installation
The torsional spring for being connected part between part and movable hook is resiliently bent, so that the bottom of movable hook activity to positive stop hook is hooked on,
Also flexible connector is pulled to bend downward while resilient mounting is pulled down, the impact force effectively born to ontology
It is buffered, the back stretch for effectively preventing connecting spring from reset generation causes the secondary damage of ontology, to reach
To the purpose protected at unmanned plane contact impact point.
(2), the support protection equipment for being used for unmanned plane, passes through setting control panel, electrically-controlled valve, helium tank and air bag phase
Mutually cooperation after unmanned plane is out of control, carries out wireless transmission signal to control panel by wireless control terminal when the device is in use
Start electrically-controlled valve, so that the high-pressure helium in helium tank imports the inner cavity of air bag by exhaust pipe, so that air bag is in high-pressure helium
Importing under expanded, and after one or more contact ground in four inclined plates that contact to earth are impacted, positive stop hook will
Movable hook is caught on, so that flexible connector is also bent and limited by elasticity, so that the closing through slot part of air bag exists
The importing of high-pressure helium extends under expanding to gap section, so that the closing of the air bag corresponding to inclined plate that contacts to earth on contact ground
Through slot part is expanded to gap section, and then effectively protects to the contact impact point part of unmanned plane.
(3), support protection equipment for being used for unmanned plane, by the way that contact to earth inclined plate and ball mutual cooperation is arranged, in equipment
In use, one or more contact ground in four inclined plates that contact to earth, when the planar section for the inclined plate that contacts to earth is by excessive impact
After power, ball is contacted with ground, so that ball is rolled on the ground, prevents the shock of a fall power that unmanned plane is excessive
The inclined plate that causes to contact to earth rubs on the ground, causes excessive vibration damage equipment component, protects to reach to unmanned plane
The purpose of shield.
Detailed description of the invention
Fig. 1 is schematic structural view of the invention；
Fig. 2 is structure enlargement diagram at A in Fig. 1；
Fig. 3 is air bag schematic top plan view of the present invention；
Fig. 4 is resilient mounting of the present invention and movable hook connection schematic diagram；
Fig. 5 is positive stop hook schematic diagram of the present invention；
Fig. 6 is flexible connector schematic diagram of the present invention.
In figure: 1 mounting base, 2 ontologies, 3 pillars, 4 hinged seats, 5 contact to earth inclined plate, 6 balls, 7 through-holes, 8 connecting springs, 9 peace
Tankage, 10 resilient mountings, 11 ropes, 12 pin shafts, 13 movable hooks, 14 torsional springs, 15 positive stop hooks, 16 flexible connectors, 17 helium
Bottle, 18 electrically-controlled valves, 19 air bags, 20 closing through slots, 21 control panels.
Specific embodiment
As shown in figures 1 to 6, the present invention provides a kind of technical solution: a kind of support protection equipment for unmanned plane, including
Mounting base 1, the inside of mounting base 1 are equipped with ontology 2, soft by rubber strip between the side wall of ontology 2 and the inner sidewall of mounting base 1
Contact, there are gap between the bottom of ontology 2 and the inside bottom of mounting base 1, the bottom four corners of mounting base 1 are fixedly connected to
Pillar 3, the bottom of four pillars 3 are fixedly connected to hinged seat 4, and the hinged ball of four 4 bottoms of hinged seat is fixedly connected to
Contact to earth inclined plate 5, and the plane of inclined plate 5 of contacting to earth and the joining place on inclined-plane are connected with ball 6, and the bottom four corners of mounting base 1 are opened
Equipped with through-hole 7, connecting spring 8, the original state of connecting spring 8 are fixedly connected between hinged seat 4 and the inclined-plane for the inclined plate 5 that contacts to earth
For confined state, the inclined-plane of connecting spring 8 and the inclined plate 5 that contacts to earth is to be mutually connected vertically, and the inside bottom rectangle of mounting base 1 is opened
Equipped with mounting groove 9, the inside bottom of four mounting grooves 9 is fixedly installed with resilient mounting 10, the inclined-plane of four inclined plates 5 that contact to earth
It is fixedly connected between top and corresponding resilient mounting 10 by rope 11, rope 11 uses micro-elasticity rope, four ropes
Rope 11 extends through corresponding through-hole 7, and the side that four resilient mountings 10 are connected with corresponding rope 11 passes through pin
Axis 12 is connected with movable hook 13, is connected between the upper surface that resilient mounting 10 is connected with 13 phase of movable hook by torsional spring 14
It connects, the inside bottom quadrangle of mounting base 1 is fixedly installed with positive stop hook 15, and positive stop hook 15 is bent in an arc shape side and movable hook 13
Bending side be in contact, the bottom surface quadrangle of ontology 2 passes through flexible connector 16 and four resilient mountings 10 respectively
Top surface is connected, and resilient mounting 10 and flexible connector 16 are all made of 65Mn spring steel material, and movable hook 13 uses
60sicr spring steel material, positive stop hook 15 use 304 stainless steel materials, and the bottom middle position of mounting base 1 is fixedly installed with helium
Gas cylinder 17, helium tank 17 use high pressure helium gas cylinder, helium liquid are stored in helium tank 17, the exhaust pipe of helium tank 17 is through peace
It fills the bottom surface of seat 1 and extends to the inside of mounting base 1, be fixedly connected with electrically-controlled valve 18 on the exhaust pipe of helium tank 17, this
The bottom of body 2 is bonded with air bag 19, and the exhaust pipe end of helium tank 17 is fixedly connected with the air guide port of air bag 19, opens on air bag 19
If four closing through slots 20 are arranged in a one-to-one correspondence with four resilient mountings 10 respectively, mounting base 1 there are four through slot 20 is closed
Right side is fixedly installed with control panel 21, and the connection relationship between control panel 21 and electrically-controlled valve 18 and ontology 2 is electrical property
Connection, control panel 21 use wireless signal receiver.
When the device is in use, when the device is in use, after unmanned plane is out of control, by wireless control terminal to control panel 21
It carries out wireless transmission signal and starts electrically-controlled valve 18, so that the high-pressure helium in helium tank 17 imports the interior of air bag 19 by exhaust pipe
Chamber, so that air bag 19 is expanded under the importing of high-pressure helium, unmanned plane lands under runaway condition, 1 lower section of mounting base
The planar section of four inclined plates 5 that contact to earth contacts ground first, one or more contact ground in four inclined plates 5 that contact to earth, so that
Impact force at contact is transmitted by the inclined plate 5 that contacts to earth, and the impact force for the inclined plate 5 that contacts to earth makes the hinged ball carry out activity of hinged seat 4,
So that the angle to contact to earth between inclined plate 5 and hinged seat 4 changes, and connecting spring 8 is replied by the inclined-plane for the inclined plate 5 that contacts to earth
Stretch, the impact force effectively born to the contact impact point of mounting base 1 buffers, and the inclined plate 5 that contacts to earth pull it is corresponding
Connection rope 11 resilient mounting 10 is pulled, and resilient mounting 10 is connected rope 11 and is pulled, and elastic
Installation part 10 is pulled deformation and bends downward, and the torsional spring 14 that part is connected between resilient mounting 10 and movable hook 13 is curved by elasticity
Song is also drawn while resilient mounting 10 is pulled down so that 13 activity of movable hook is hooked on to the bottom of positive stop hook 15
Dynamic elasticity connector 16 is bent downward, and the impact force effectively born to ontology 2 buffers, and effectively prevents connecting spring
8 back stretch for carrying out reset generation cause the secondary damage of ontology 2, and positive stop hook 15 catches on movable hook 13, so that bullet
Property connector 16 also by elasticity bend and limited so that air bag 19 closing 20 part of through slot high-pressure helium importing expand
Fill it is lower to gap section extend so that contact ground the air bag 19 corresponding to inclined plate 5 that contacts to earth 20 part of closing through slot to
Gap section is expanded, and then effectively protects to the contact impact point part of unmanned plane.
Claims (7)
1. equipment, including mounting base (1) are protected in a kind of support for unmanned plane, it is characterised in that: the mounting base (1) it is interior
Side is equipped with ontology (2), and the bottom four corners of the mounting base (1) are fixedly connected to pillar (3), the bottom of four pillars (3)
It is fixedly connected to hinged seat (4), the hinged ball of four hinged seat (4) bottoms is fixedly connected to the inclined plate that contacts to earth (5), the touching
The plane of ground inclined plate (5) and the joining place on inclined-plane are connected with ball (6), and the bottom four corners of the mounting base (1) open up
Have through-hole (7), is fixedly connected with connecting spring (8), the installation between the hinged seat (4) and the inclined-plane of the inclined plate that contacts to earth (5)
The inside bottom rectangle of seat (1) offers mounting groove (9), and the inside bottom of four mounting grooves (9) is fixedly installed with bullet
Property installation part (10), passes through rope between the incline apex and corresponding resilient mounting (10) of the inclined plate (5) that contacts to earth described in four
Rope (11) is fixedly connected, and the side that four resilient mountings (10) are connected with corresponding rope (11) passes through pin shaft
(12) it is connected with movable hook (13), passes through between the upper surface that the resilient mounting (10) is mutually connected with movable hook (13)
Torsional spring (14) is connected, and the inside bottom quadrangle of the mounting base (1) is fixedly installed with positive stop hook (15), the positive stop hook
(15) the side that is bent in an arc shape is in contact with the bending side of movable hook (13), the bottom surface quadrangle difference of the ontology (2)
It is connected by flexible connector (16) with the top surface of four resilient mountings (10), in the bottom of the mounting base (1)
Between position be fixedly installed with helium tank (17), the exhaust pipe of the helium tank (17) through mounting base (1) bottom surface and prolong
The inside of mounting base (1) is extended to, is fixedly connected with electrically-controlled valve (18) on the exhaust pipe of the helium tank (17), the ontology (2)
Bottom be bonded with air bag (19), the exhaust pipe end of the helium tank (17) is fixedly connected with the air guide port of air bag (19), institute
State opened up on air bag (19) there are four close through slot (20), four closing through slots (20) respectively with four resilient mountings
(10) it is arranged in a one-to-one correspondence, the right side of the mounting base (1) is fixedly installed with control panel (21).
2. equipment is protected in a kind of support for unmanned plane according to claim 1, it is characterised in that: the control panel
(21) connection relationship between electrically-controlled valve (18) and ontology (2) is to be electrically connected, and the control panel (21) is using wireless
Signal receiver.
3. equipment is protected in a kind of support for unmanned plane according to claim 1, it is characterised in that: the rope (11)
Using micro-elasticity rope, four ropes (11) extend through corresponding through-hole (7).
4. equipment is protected in a kind of support for unmanned plane according to claim 1, it is characterised in that: the elasticity installation
Part (10) and flexible connector (16) are all made of 65Mn spring steel material, and movable hook (13) uses 60sicr spring steel material, institute
Positive stop hook (15) are stated using 304 stainless steel materials.
5. equipment is protected in a kind of support for unmanned plane according to claim 1, it is characterised in that: the ontology (2)
Side wall and mounting base (1) inner sidewall between by the soft contact of rubber strip, the bottom of the ontology (2) and mounting base (1)
There are gaps between inside bottom.
6. equipment is protected in a kind of support for unmanned plane according to claim 1, it is characterised in that: the connecting spring
(8) original state is confined state, and the inclined-plane of the connecting spring (8) and the inclined plate that contacts to earth (5) is is mutually connected vertically.
7. equipment is protected in a kind of support for unmanned plane according to claim 1, it is characterised in that: the helium tank
(17) high pressure helium gas cylinder is used, stores helium liquid in helium tank (17).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910273598.4A CN110001938A (en) | 2019-04-06 | 2019-04-06 | A kind of support protection equipment for unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910273598.4A CN110001938A (en) | 2019-04-06 | 2019-04-06 | A kind of support protection equipment for unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110001938A true CN110001938A (en) | 2019-07-12 |
Family
ID=67170115
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910273598.4A Withdrawn CN110001938A (en) | 2019-04-06 | 2019-04-06 | A kind of support protection equipment for unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110001938A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110697033A (en) * | 2019-10-28 | 2020-01-17 | 罗嘉宇 | Many rotor unmanned aerial vehicle undercarriage |
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| CN207257975U (en) * | 2017-07-31 | 2018-04-20 | 河南豫乾技术转移中心有限公司 | Unmanned plane elasticity chassis |
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| CN108454835A (en) * | 2017-02-20 | 2018-08-28 | 深圳光启空间技术有限公司 | Undercarriage and aircraft |
| CN108557056A (en) * | 2018-04-03 | 2018-09-21 | 芜湖超科机电设备有限公司 | A kind of unmanned plane used for geological prospecting of taking photo by plane |
| CN108820192A (en) * | 2018-06-13 | 2018-11-16 | 郑州秉同立智电子科技有限公司 | A kind of unmanned plane buffering stand being conveniently replaceable |
| CN108891614A (en) * | 2018-06-28 | 2018-11-27 | 芜湖新尚捷智能信息科技有限公司 | A kind of air bag auxiliary unmanned plane protective device |
| CN109263865A (en) * | 2018-10-08 | 2019-01-25 | 东阳市天齐科技有限公司 | The movable undercarriage of multi-rotor unmanned aerial vehicle |
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2019
- 2019-04-06 CN CN201910273598.4A patent/CN110001938A/en not_active Withdrawn
Patent Citations (9)
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|---|---|---|---|---|
| US20170267335A1 (en) * | 2016-03-21 | 2017-09-21 | Safran Landing Systems | Lockable wheel actuator disengagement system on an aircraft landing gear |
| CN206141851U (en) * | 2016-10-08 | 2017-05-03 | 无锡飞天侠科技有限公司 | Real time imaging unmanned aerial vehicle camera device collides receiving mechanism |
| CN108454835A (en) * | 2017-02-20 | 2018-08-28 | 深圳光启空间技术有限公司 | Undercarriage and aircraft |
| CN207257975U (en) * | 2017-07-31 | 2018-04-20 | 河南豫乾技术转移中心有限公司 | Unmanned plane elasticity chassis |
| CN108116687A (en) * | 2017-12-20 | 2018-06-05 | 郑州康晓科技有限公司 | Unmanned plane accidental falling deceleration damping device |
| CN108557056A (en) * | 2018-04-03 | 2018-09-21 | 芜湖超科机电设备有限公司 | A kind of unmanned plane used for geological prospecting of taking photo by plane |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110697033A (en) * | 2019-10-28 | 2020-01-17 | 罗嘉宇 | Many rotor unmanned aerial vehicle undercarriage |
| CN110697033B (en) * | 2019-10-28 | 2020-06-09 | 陕西嘉创飞航无人机科技有限公司 | Many rotor unmanned aerial vehicle undercarriage |
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| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190712 |
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| WW01 | Invention patent application withdrawn after publication |