CN106218876A - A kind of aerial photography device with shockproof function - Google Patents
A kind of aerial photography device with shockproof function Download PDFInfo
- Publication number
- CN106218876A CN106218876A CN201610706103.9A CN201610706103A CN106218876A CN 106218876 A CN106218876 A CN 106218876A CN 201610706103 A CN201610706103 A CN 201610706103A CN 106218876 A CN106218876 A CN 106218876A
- Authority
- CN
- China
- Prior art keywords
- foot rest
- bracing frame
- straight tube
- fixed
- guard rail
- 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.)
- Pending
Links
- 238000013016 damping Methods 0.000 claims abstract description 42
- 229920001971 elastomer Polymers 0.000 claims description 8
- 239000005060 rubber Substances 0.000 claims description 8
- 239000000463 material Substances 0.000 claims description 6
- 230000006378 damage Effects 0.000 abstract description 7
- 210000003128 head Anatomy 0.000 description 9
- 230000006835 compression Effects 0.000 description 4
- 238000007906 compression Methods 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000009514 concussion Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000000523 sample Substances 0.000 description 2
- 229920003051 synthetic elastomer Polymers 0.000 description 2
- 239000005061 synthetic rubber Substances 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 244000043261 Hevea brasiliensis Species 0.000 description 1
- 239000005062 Polybutadiene Substances 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 241000607479 Yersinia pestis Species 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- MTAZNLWOLGHBHU-UHFFFAOYSA-N butadiene-styrene rubber Chemical compound C=CC=C.C=CC1=CC=CC=C1 MTAZNLWOLGHBHU-UHFFFAOYSA-N 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000002372 labelling Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000004899 motility Effects 0.000 description 1
- 229920003052 natural elastomer Polymers 0.000 description 1
- 229920001194 natural rubber Polymers 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 229920002857 polybutadiene Polymers 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 239000002341 toxic gas Substances 0.000 description 1
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
- B64C25/62—Spring shock-absorbers; Springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Vibration Prevention Devices (AREA)
Abstract
The invention discloses a kind of aerial photography device with shockproof function, including aircraft body, connecting on aircraft body has two to land foot rest, and each foot rest that lands includes that two support straight tubes and a bracing frame, are provided with a damping spring between each support straight tube and bracing frame；One end of described damping spring is fixed with supporting straight tube, and the other end is fixed with bracing frame；Being additionally provided with damping straight tube inside damping spring, one end of damping straight tube is fixed with bracing frame, and the other end is placed in inside support straight tube；Also including that extends a foot rest on foot rest each landing, described prolongation foot rest is fixed on bracing frame by two buckles；Landing at two and be additionally provided with a guard rail between foot rest, the two ends of guard rail are connected with two bracing frames landed on foot rest respectively.Advantages of the present invention: solve land vibrations bring photographic head, The Cloud Terrace and land foot rest easily collide with damage problem.
Description
Technical field
The present invention relates to minute vehicle field, relate in particular to a kind of aerial photography device with shockproof function.
Background technology
Minute vehicle receives much attention owing to having special purposes.One important application is military surveillance, is equipped with
To soldier class, carry out enemy's situation scouting and supervision.Can be additionally used in war danger estimation, target search, communication relay, monitoring chemistry,
Nuclear or biological weapons, scouts interior of building situation.It is applicable to the multiple war environment such as city, jungle.Because it is easy to take
Band, simple to operate, advantage that safety is good, can equip in a large number in army.In non-military field, it is configured with respective sensor
Minute vehicle can be used to search disaster survivor, toxic gas or chemical substance source, eliminate crop pests etc..In reality
In the life of border, the minute vehicle with photography function uses the most universal, but this minute vehicle land foot rest one
As be made up of rigid, hard plastics or rustless steel, material is harder, the most wear-resisting, yielding, when landing, lands foot rest, photographic head
Very big with the concussion impact that The Cloud Terrace is subject to, damage of easily being collided with.Even if landing on smooth ground, always can exist and taking the photograph
The unclear problem of picture shot when landing as head.
Summary of the invention
It is an object of the invention to provide a kind of aerial photography device with shockproof function, solve existing minute vehicle and falling
Ground time, the foot rest that lands be easily subject to impact and damage, and land foot rest be weak to mill problem；Solve existing minute vehicle
When falling on uneven ground, the photographic head of minute vehicle and The Cloud Terrace easily collide with damage, and the picture of shooting is because being shaken
Dynamic and ambiguous problem.
The present invention is achieved through the following technical solutions:
A kind of aerial photography device with shockproof function, including aircraft body, connects on aircraft body and has two to land foot rest,
Each foot rest that lands includes that two support straight tube and a bracing frame, are provided with two slotted eyes, often on each bracing frame (3)
A damping spring it is provided with between individual support straight tube and bracing frame；One end of described damping spring is fixed, separately with supporting straight tube
One end is fixed with bracing frame；Being additionally provided with damping straight tube inside damping spring, one end of damping straight tube is fixed with bracing frame, separately
One end is placed in inside support straight tube；Also including that extends a foot rest on foot rest each landing, described prolongation foot rest passes through two
Buckle is fixed on bracing frame；Landing at two and be additionally provided with a guard rail between foot rest, the two ends of guard rail are respectively with two
The individual bracing frame landed on foot rest connects；Described guard rail be one by the bar pad having certain thickness rubber to make, anti-
The two ends of guardrail are provided with groove, the notch size of groove and the shaft diameter matches of bracing frame；Each groove also sets up
Having two circular holes, the diameter of described circular hole is equal with the diameter of slotted eye on bracing frame, uses screw bolt and nut to coordinate
Guard rail is fixed on bracing frame by the mode connected.
Further, arranging a damping straight tube inside damping spring, one end of damping straight tube is fixed with bracing frame, subtracts
One end and the bracing frame of shake straight tube are fixing has been a supporting role, it is to avoid damping spring bending shifts, and causes landing foot rest
Deformation.Additionally the other end of damping straight tube be placed in support straight tube inside, when designing simultaneously, it is desirable to damping straight tube not with support straight tube
Being connected and also have a certain distance with supporting straight tube, such damping straight tube can move along with the compression of damping spring and past
Support straight tube is internal mobile.Flight controller has constant weight, so flight controller is when landing, is positioned on flight controller
The foot rest that lands can produce an active force over the ground, meanwhile, landing foot rest also can be by the opposition on ground.Because being subject to
To the opposition on ground, the damping spring on foot rest that lands will be produced a thrust by compression, and damping spring produces
The opposition on thrust and ground can be cancelled out each other, meanwhile, be placed in support one end of the damping straight tube within straight tube can be along with
The compression of damping spring and more probe into inside support straight tube.The damping spring and the damping straight tube that arrange on foot rest solve existing
Minute vehicle when landing, the foot rest that lands be easily subject to impact and damage, and land foot rest be weak to mill problem.
Also include that extends a foot rest on foot rest each landing, one prolongation foot rest is fixed on by two buckles
Add on support and land the height of foot rest, both can ensure that the original-pack foot rest that lands was not dirty, and be not scraped off, fall can be reduced again
The probability that camera lens when falling, The Cloud Terrace are injured.
Landing at two and arrange a guard rail between foot rest, guard rail is had certain thickness rubber blanket to make by one,
For example with synthetic rubber.The top view of guard rail is a rectangle, and the width of guard rail can be with more slightly wider, as far as possible will shooting
Head base and The Cloud Terrace surround, and when falling rough local time, the effect of camera head protecting can be more preferably.The two ends of guard rail are recessed
Groove, groove has two apertures, is stuck on bracing frame by groove, and bolt passes aperture, uses nut by guard rail and bracing frame
Fix.
Being additionally provided with the connecting hole of an annular on each support straight tube, the foot rest that lands is threaded connection part and passes
Connecting hole is fixed with aircraft body.Further, foot rest is landed for convenience supporting the connecting hole arranging annular on straight tube
It is threaded connection fixing with aircraft body, uses threaded connector to have spirit through connecting hole such connection fixed form
Activity, the foot rest that lands can take off at any time, does not occupies, it is simple to transport.
Described prolongation foot rest uses abrasion-resistive hard quality of rubber materials to make.Further, abrasion-resistive hard quality of rubber materials system is used
The prolongation foot rest become can be more resistant to mill, and service life is longer.Here butadiene-styrene rubber or butadiene rubber can be used.
The present invention compared with prior art, has such advantages as and beneficial effect:
1, a kind of aerial photography device with shockproof function of the present invention, solves existing minute vehicle when landing, and lands foot rest
Be easily subject to impact and damage, and land foot rest be weak to mill problem；
2, a kind of aerial photography device with shockproof function of the present invention, solves existing minute vehicle and falls on uneven ground
Time, the photographic head of minute vehicle and The Cloud Terrace easily collide with damage, and meanwhile, the picture of shooting also can obscure not because being given a shock
Clear problem；
3, a kind of aerial photography device with shockproof function of the present invention, the foot rest that lands can take off at any time, has motility, not occupy-place
Put, it is simple to transport.
Accompanying drawing explanation
Accompanying drawing described herein is used for providing being further appreciated by the embodiment of the present invention, constitutes of the application
Point, it is not intended that the restriction to the embodiment of the present invention.In the accompanying drawings:
Fig. 1 is the structural representation of the present invention；
Fig. 2 is that the present invention lands the structural representation of foot rest；
Fig. 3 is the structural representation of guard rail of the present invention.
Labelling in accompanying drawing and the component names of correspondence:
1-aircraft body, 2-supports straight tube, 3-bracing frame, 4-damping spring, 5-damping straight tube, and 6-extends foot rest, 7-card
Button, 8-connecting hole, 9-guard rail, 10-groove, 11-circular hole.
Detailed description of the invention
For making the object, technical solutions and advantages of the present invention clearer, below in conjunction with embodiment and accompanying drawing, to this
Invention is described in further detail, and the exemplary embodiment of the present invention and explanation thereof are only used for explaining the present invention, do not make
For limitation of the invention.
Embodiment 1:
A kind of aerial photography device with shockproof function as shown in Figure 1, Figure 2, Figure 3 shows, including aircraft body 1, at aircraft body 1
Upper connection has two to land foot rest, it is characterised in that each foot rest that lands includes that two support straight tubes 2 and a bracing frame 3,
It is provided with two slotted eyes on each bracing frame 3, between each support straight tube 2 and bracing frame 3, is provided with a damping spring 4；
One end of described damping spring 4 is fixed with supporting straight tube 2, and the other end is fixed with bracing frame 3；Also set up inside damping spring 4
Having damping straight tube 5, one end of damping straight tube 5 to fix with bracing frame 3, it is internal that the other end is placed in support straight tube 2；At each landing leg
Also including on frame that extends a foot rest 6, described prolongation foot rest 6 is fixed on bracing frame 3 by two buckles 7；Land at two
Being additionally provided with a guard rail 9 between foot rest, the two ends of guard rail 9 are connected with two bracing frames landed on foot rest 3 respectively；Institute
State guard rail 9 to be one and be provided with groove 10 at the two ends of guard rail 9 by the bar pad having certain thickness rubber to make, recessed
The notch size of groove 10 and the shaft diameter matches of bracing frame 3；Each groove 10 is additionally provided with two circular holes 11, described circle
The diameter in hole 11 is equal with the diameter of slotted eye on bracing frame 3, and the mode using screw bolt and nut to be connected will be anti-
Guardrail 9 is fixed on bracing frame 3.Being additionally provided with the connecting hole 8 of an annular on each support straight tube 2, the foot rest that lands leads to
Cross threaded connector to fix through connecting hole with aircraft body 1.Described prolongation foot rest 6 uses abrasion-resistive hard quality of rubber materials system
Become.
The design principle of a kind of aerial photography device with shockproof function: flight controller has constant weight, so flight control
Device processed is when landing, and the foot rest that lands being positioned on flight controller can produce an active force over the ground, meanwhile, lands foot rest also
Can be by the opposition on ground.Because by the opposition on ground, the damping spring 4 landed on foot rest will be pressed
Contracting produces a thrust, and the thrust of damping spring 4 generation can be cancelled out each other with the opposition on ground, meanwhile, is placed in support
It is internal that one end of damping straight tube 5 within straight tube 2 can more probe into support straight tube 2 along with the compression of damping spring 4.At landing leg
The damping spring 4 arranged on frame and damping straight tube 5 solve existing minute vehicle and are easily subject to concussion when landing, and cause
The float of shooting is unclear, and lands foot rest and be easily subject to impact and the problem damaged.
Also include that extends a foot rest 6 on foot rest each landing, by two buckles 7, a prolongation foot rest 6 is fixed
Bracing frame 3 adds and lands the height of foot rest, both can ensure that the original-pack foot rest that lands was not dirty, and be not scraped off, again can
The probability that when reducing landing, camera lens, The Cloud Terrace are injured.Additionally extending foot rest 6 uses natural rubber material to make, and more resistant to mill, uses the longevity
Order longer.
Landing at two and arrange a guard rail 9 between foot rest, guard rail 9 uses synthetic rubber to make.When falling in injustice
The local time in of sliding, there are this guard rail 9, photographic head and The Cloud Terrace can avoid colliding with below photographic head, photographic head and The Cloud Terrace
A good protection can be obtained.
Above-described detailed description of the invention, has been carried out the purpose of the present invention, technical scheme and beneficial effect further
Describe in detail, be it should be understood that the detailed description of the invention that the foregoing is only the present invention, be not intended to limit the present invention
Protection domain, all within the spirit and principles in the present invention, any modification, equivalent substitution and improvement etc. done, all should comprise
Within protection scope of the present invention.
Claims (3)
1., with an aerial photography device for shockproof function, including aircraft body (1), there are two in the upper connection of aircraft body (1)
Land foot rest, it is characterised in that each foot rest that lands includes that two support straight tube (2) and a bracing frame (3), in each support
It is provided with two slotted eyes on frame (3), between each support straight tube (2) and bracing frame (3), is provided with a damping spring (4)；
One end of described damping spring (4) is fixed with supporting straight tube (2), and the other end is fixed with bracing frame (3)；In damping spring (4)
Portion is additionally provided with damping straight tube (5), and one end of damping straight tube (5) is fixed with bracing frame (3), and the other end is placed in support straight tube (2)
Internal；Also including that extends a foot rest (6) on foot rest each landing, described prolongation foot rest (6) is fixed by two buckles (7)
On bracing frame (3)；Landing at two and be additionally provided with a guard rail (9) between foot rest, the two ends of guard rail (9) are respectively with two
The individual bracing frame (3) landed on foot rest connects；Described guard rail (9) be one by the bar shaped having certain thickness rubber to make
Pad, is provided with the shaft diameter of groove (10), the notch size of groove (10) and bracing frame (3) at the two ends of guard rail (9)
Join；Each groove (10) is additionally provided with two circular holes (11), the diameter of described circular hole (11) groove upper with bracing frame (3)
The diameter in hole is equal, and guard rail (9) is fixed on bracing frame (3) by the mode using screw bolt and nut to be connected.
A kind of aerial photography device with shockproof function the most according to claim 1, it is characterised in that at each support straight tube
(2) being additionally provided with the connecting hole (8) of an annular on, the foot rest that lands is threaded connection part through connecting hole and aircraft machine
Body (1) is fixed.
A kind of aerial photography device with shockproof function the most according to claim 1, it is characterised in that described prolongation foot rest (6)
Abrasion-resistive hard quality of rubber materials is used to make.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610706103.9A CN106218876A (en) | 2016-08-23 | 2016-08-23 | A kind of aerial photography device with shockproof function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610706103.9A CN106218876A (en) | 2016-08-23 | 2016-08-23 | A kind of aerial photography device with shockproof function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106218876A true CN106218876A (en) | 2016-12-14 |
Family
ID=57552941
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610706103.9A Pending CN106218876A (en) | 2016-08-23 | 2016-08-23 | A kind of aerial photography device with shockproof function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106218876A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109050914A (en) * | 2018-08-09 | 2018-12-21 | 广州华夏职业学院 | Unmanned plane support device is sent in a kind of take-away with charge free |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204197280U (en) * | 2014-11-12 | 2015-03-11 | 成都好飞机器人科技有限公司 | A kind of elasticity alighting gear of depopulated helicopter |
| CN205076031U (en) * | 2015-09-07 | 2016-03-09 | 天津市天舞科技有限公司 | Helicopter cage undercarriage that adaptive capacity to environment is stronger |
| CN105438451A (en) * | 2015-11-30 | 2016-03-30 | 无锡觅睿恪科技有限公司 | Elastic protective underframe of unmanned aerial vehicle |
| CN205150253U (en) * | 2015-11-26 | 2016-04-13 | 江西天祥通用航空股份有限公司 | Novel helicopter joins externally pesticide spraying machine |
| CN205327398U (en) * | 2015-12-27 | 2016-06-22 | 北京航空航天大学 | Small -size many rotor crafts shock attenuation undercarriage |
| CN105857615A (en) * | 2016-05-16 | 2016-08-17 | 苏州金建达智能科技有限公司 | Unmanned aerial vehicle with object transportation function of robot |
| CN206107591U (en) * | 2016-08-23 | 2017-04-19 | 成都翼高九天科技有限公司 | Modified flying device that takes photo by plane |
-
2016
- 2016-08-23 CN CN201610706103.9A patent/CN106218876A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204197280U (en) * | 2014-11-12 | 2015-03-11 | 成都好飞机器人科技有限公司 | A kind of elasticity alighting gear of depopulated helicopter |
| CN205076031U (en) * | 2015-09-07 | 2016-03-09 | 天津市天舞科技有限公司 | Helicopter cage undercarriage that adaptive capacity to environment is stronger |
| CN205150253U (en) * | 2015-11-26 | 2016-04-13 | 江西天祥通用航空股份有限公司 | Novel helicopter joins externally pesticide spraying machine |
| CN105438451A (en) * | 2015-11-30 | 2016-03-30 | 无锡觅睿恪科技有限公司 | Elastic protective underframe of unmanned aerial vehicle |
| CN205327398U (en) * | 2015-12-27 | 2016-06-22 | 北京航空航天大学 | Small -size many rotor crafts shock attenuation undercarriage |
| CN105857615A (en) * | 2016-05-16 | 2016-08-17 | 苏州金建达智能科技有限公司 | Unmanned aerial vehicle with object transportation function of robot |
| CN206107591U (en) * | 2016-08-23 | 2017-04-19 | 成都翼高九天科技有限公司 | Modified flying device that takes photo by plane |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109050914A (en) * | 2018-08-09 | 2018-12-21 | 广州华夏职业学院 | Unmanned plane support device is sent in a kind of take-away with charge free |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104527979B (en) | Space base teargas bullet automatic feeder | |
| CN106081077A (en) | A kind of can the shockproof flight instruments of multiple-effect of flying for long time | |
| KR101858009B1 (en) | Drone for inspecting bridge | |
| CN207050575U (en) | Unmanned plane carry catches net rifle in the air | |
| CN206107591U (en) | Modified flying device that takes photo by plane | |
| CN211223849U (en) | Combined type unmanned aerial vehicle vibration damping mount | |
| CN106218876A (en) | A kind of aerial photography device with shockproof function | |
| CN110979643A (en) | Landing gear and unmanned aerial vehicle | |
| CN205971819U (en) | Prevent to fall to ground flight controller who vibrates | |
| CN212423449U (en) | Unmanned aerial vehicle rises and falls with stabilizer blade structure with shock-absorbing function | |
| KR101891693B1 (en) | Dron with the radial pattern arrangement of outside frame | |
| CN203681878U (en) | Damping device of multi-lens aerial photography stabilized platform | |
| CN211996147U (en) | Automatic high-altitude water inlet separating device | |
| CN106275396A (en) | A kind of flight detector with shock-absorbing function | |
| CN206087284U (en) | Miniature aircraft of modified four -axis | |
| KR102002952B1 (en) | A device for damage protection for a drone | |
| CN206087275U (en) | But jar -proof flying device of solar energy power supply multiple -effect | |
| CN212125520U (en) | Unmanned aerial vehicle aerial photographing device for monitoring forest fire | |
| CN210734506U (en) | Be applied to glass curtain wall remote sensing and detect's unmanned aerial vehicle | |
| CN210555562U (en) | Unmanned aerial vehicle shock attenuation undercarriage | |
| CN210882619U (en) | Fire control unmanned aerial vehicle | |
| CN205589470U (en) | Unmanned aerial vehicle | |
| CN208344532U (en) | A kind of parachuting type unmanned plane recyclable device | |
| CN207658086U (en) | A kind of unmanned plane image collecting device | |
| CN106275397A (en) | A kind of can the minute vehicle of automatic power |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161214 |