CN110341945A - A kind of Collapsible support for unmanned plane - Google Patents
A kind of Collapsible support for unmanned plane Download PDFInfo
- Publication number
- CN110341945A CN110341945A CN201910709195.XA CN201910709195A CN110341945A CN 110341945 A CN110341945 A CN 110341945A CN 201910709195 A CN201910709195 A CN 201910709195A CN 110341945 A CN110341945 A CN 110341945A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- support frame
- bottom plate
- cross bar
- telescopic rod
- 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
- 229910000831 Steel Inorganic materials 0.000 claims description 8
- 239000010959 steel Substances 0.000 claims description 8
- 239000000853 adhesive Substances 0.000 claims description 5
- 230000001070 adhesive effect Effects 0.000 claims description 5
- 239000003292 glue Substances 0.000 claims description 5
- 230000003139 buffering effect Effects 0.000 claims description 3
- 239000006260 foam Substances 0.000 claims description 3
- 238000003466 welding Methods 0.000 claims description 3
- 230000005855 radiation Effects 0.000 claims 1
- 238000000034 method Methods 0.000 description 5
- 238000013016 damping Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- UPLPHRJJTCUQAY-WIRWPRASSA-N 2,3-thioepoxy madol Chemical compound C([C@@H]1CC2)[C@@H]3S[C@@H]3C[C@]1(C)[C@@H]1[C@@H]2[C@@H]2CC[C@](C)(O)[C@@]2(C)CC1 UPLPHRJJTCUQAY-WIRWPRASSA-N 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 235000013399 edible fruits Nutrition 0.000 description 2
- 230000017525 heat dissipation Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 239000003381 stabilizer Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/04—Arrangement or disposition on aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
-
- 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
- B64C25/54—Floats
- B64C25/56—Floats inflatable
-
- 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
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/08—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
-
- 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
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of Collapsible supports for unmanned plane, including cross bar, connecting rod, support frame and radiator fan, cross bar is equipped with two side by side, two connecting rods are welded between two cross bars in parallel, the bottom of cross bar is connected with bottom plate by spring, bottom plate is airbag structure, telescopic rod there are four being set on cross bar, the top of telescopic rod is fixed on the support frame, telescopic rod is equipped with telescoping switch, it is opened up above support frame fluted, the bottom of groove is equipped with buffer layer, several buffer springs are fixed in buffer layer, opening is offered on support frame and buffer layer, the bottom of support frame is equipped with radiator fan, the side of support frame is equipped with fan swicth, cell jar is additionally provided in support frame, cell jar is embedded with battery.The present invention effectively reduces the impact force generated when UAV Landing, protects to unmanned plane, and support frame reduces unmanned plane during flying resistance convenient for being folded in unmanned plane during flying.
Description
Technical field
The present invention relates to air vehicle technique field, specially a kind of Collapsible support for unmanned plane.
Background technique
Unmanned plane press application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.The people
With aspect, unmanned plane+industrial application is that unmanned plane has really just needed；At present take photo by plane, agricultural, plant protection, self-timer, express transportation,
Disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture wave
The application in unrestrained etc. field, has greatly expanded the purposes of unmanned plane itself, developed country also actively extension industrial application with
Develop unmanned air vehicle technique.
The support frame of existing unmanned plane is inconvenient for use, is easy since support frame is longer so that unmanned plane during flying is inconvenient,
It is easy when flight in small space so that unmanned plane damages, and biggish support frame is easy gas-flow resistance when increase flight, it is inconvenient
In unmanned plane stabilized flight, in addition unmanned plane can generate strong impact, traditional unmanned plane support frame damping effect when landing
Fruit is poor.
Summary of the invention
The purpose of the present invention is to provide a kind of Collapsible supports for unmanned plane, to solve in above-mentioned background technique
The problem of proposition.
In order to solve the above technical problem, the present invention provides following technical solutions:
A kind of Collapsible support for unmanned plane, including cross bar, connecting rod, support frame and radiator fan, the cross
Bar is equipped with two side by side, is welded with two connecting rods between two cross bars in parallel, fixed between the cross bar and connecting rod
There is steel wire, the bottom of the cross bar is connected with bottom plate by spring, and the bottom plate is airbag structure, and the side of bottom plate is fixed
It is provided with valve cock, is connected in the valve cock and bottom plate, the bottom of the bottom plate is additionally provided with cushion, and the cross bar is equipped with
Four telescopic rods, the top of the telescopic rod is fixed on the support frame, and the telescopic rod is equipped with telescoping switch, support frame as described above
Top open up fluted, the bottom of the groove is equipped with buffer layer, is fixed with several buffer springs in the buffer layer, described
Opening is offered on support frame and buffer layer, the bottom of support frame as described above is equipped with radiator fan, the side of support frame as described above
Equipped with fan swicth, cell jar is additionally provided in support frame as described above, the cell jar is embedded with battery, the telescoping switch
It is electrically connected with battery, and is provided with PLC controller on telescoping switch, the PLC controller connects with unmanned aerial vehicle (UAV) control end
It connects.
In order to further increase a kind of use function of Collapsible support for unmanned plane, gone back in the buffer layer equal
It is even to be equipped with foam.
In order to further increase a kind of use function of Collapsible support for unmanned plane, the telescopic rod includes set
Pipe and support column, offer screw hole on casing, with being arranged with holding screw in screw hole.
In order to further increase a kind of use function of Collapsible support for unmanned plane, the radiator fan and wind
Fan switch is electrically connected, and the fan swicth and battery are electrically connected.
In order to further increase a kind of use function of Collapsible support for unmanned plane, the spring is at least arranged
Four groups, the spring is fixedly connected on cross bar and bottom plate by welding.
In order to further increase a kind of use function of Collapsible support for unmanned plane, the cushion is thickness
Rubber pad not less than 5mm, the cushion are adhered to bottom plate by adhesive glue fixation.
Compared with prior art, the beneficial effects obtained by the present invention are as follows being: the present invention is placed on by setting groove, unmanned plane
The inside is more stable, will not slide easily, by the way that buffer layer is arranged, when unmanned plane is placed in groove, can reduce vibration, subtract
The small abrasion to unmanned plane, by be arranged radiator fan, help unmanned plane heat dissipation, extend the service life of unmanned plane, by
It is evenly provided with spring between cross bar and bottom plate, there is good damping effect, the bottom of bottom plate is fixed viscous by adhesive glue
It is connected with cushion, has the function that level 2 buffering, the impact force generated when effectively reducing UAV Landing protects unmanned plane
Shield is airbag structure by setting bottom plate, and the side of bottom plate is fixedly installed valve cock, is connected to, keeps away in valve cock and bottom plate
Unmanned plane is exempted to sink in rivers and lakes when breaking down, by the way that telescopic rod is arranged, telescoping switch has been set on telescopic rod, is stretched
PLC controller is set on switch, and PLC controller is connect with unmanned aerial vehicle (UAV) control end, convenient for the support frame receipts in unmanned plane during flying
Contracting reduces unmanned plane during flying resistance so that unmanned plane during flying is more steady, avoid support frame in flight resistance compared with havoc without
The problem of man-machine flight balance, and it is convenient for the unmanned plane in flight that can normally pass through narrow space, avoid support
Frame, which expands unmanned plane volume, makes it can not be the problem of narrow space carries out normal flight, by the way that steel wire, steel wire is arranged
Other component can be placed on the net, be convenient for loading, which designs reasonable and practical, and it is easy to operate, it is suitble to
It promotes the use of.
Detailed description of the invention
Attached drawing is used to provide further understanding of the present invention, and constitutes part of specification, with reality of the invention
It applies example to be used to explain the present invention together, not be construed as limiting the invention.In the accompanying drawings:
Fig. 1 is the structural diagram of the present invention；
Fig. 2 is the overlooking structure diagram of cross bar and connecting rod of the invention.
Attached drawing mark explanation:
1, cross bar, 2, connecting rod, 3, support frame, 4, radiator fan, 5, spring, 6, bottom plate, 7, valve cock, 8, cushion,
9, telescopic rod, 10, telescoping switch, 11, groove, 12, buffer layer, 13, buffer spring, 14, opening, 15, fan swicth, 16, storage
Battery, 17, steel wire.
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.
Please refer to a kind of Fig. 1-Collapsible support for unmanned plane shown in Fig. 2, including cross bar 1, connecting rod 2, branch
Support 3 and radiator fan 4, the cross bar 1 are equipped with two side by side, are welded with two connecting rods in parallel between two cross bars 1
2, steel wire 17 is fixed between the cross bar 1 and connecting rod 2, the bottom of the cross bar 1 is connected with bottom plate 6, institute by spring 5
Stating bottom plate 6 is airbag structure, and the side of bottom plate 6 is fixedly installed valve cock 7, is connected in the valve cock 7 and bottom plate 6, institute
The bottom for stating bottom plate 6 is additionally provided with cushion 8, is set on the cross bar 1 there are four telescopic rod 9, the top of the telescopic rod 9 is fixed on
On support frame 3, the telescopic rod 9 is equipped with telescoping switch 10, and the top of support frame as described above 3 opens up fluted 11, the groove
11 bottom is equipped with buffer layer 12, is fixed with several buffer springs 13, support frame as described above 3 and buffer layer 12 in the buffer layer 12
On offer opening 14, the bottom of support frame as described above 3 is equipped with radiator fan 4, and the side of support frame as described above 3 is opened equipped with fan
15 are closed, is additionally provided with cell jar in support frame as described above 3, the cell jar is embedded with battery 16,10 He of telescoping switch
Battery 16 is electrically connected, and PLC controller is provided on telescoping switch 10, the PLC controller with unmanned aerial vehicle (UAV) control end
Connection.
In order to further increase a kind of use function of Collapsible support for unmanned plane, gone back in the buffer layer 12
It is uniformly provided with foam.
In order to further increase a kind of use function of Collapsible support for unmanned plane, the telescopic rod 9 includes
Casing and support column, offer screw hole on casing, with being arranged with holding screw in screw hole.
In order to further increase a kind of use function of Collapsible support for unmanned plane, 4 He of radiator fan
Fan swicth 15 is electrically connected, and the fan swicth 15 and battery 16 are electrically connected.
In order to further increase a kind of use function of Collapsible support for unmanned plane, the spring 5 is at least set
Four groups are set, the spring 5 is fixedly connected on cross bar 1 and bottom plate 6 by welding.
In order to further increase a kind of use function of Collapsible support for unmanned plane, the cushion 12 is thickness
Degree is not less than the rubber pad of 5mm, and the cushion 12 is adhered to bottom plate 6 by adhesive glue fixation.
The working principle of the invention and beneficial effect achieved are: when using the unmanned plane support frame, unmanned plane being put
It sets in groove 11, the stabilizer blade of unmanned plane is put down out of groove 11, according to the model of unmanned plane, adjust the length of telescopic rod 9,
If unmanned plane just used, body is hot, openable fan swicth 15, is radiated using radiator fan 4 to unmanned plane, by setting
Set groove 11, it is more stable that unmanned plane is placed on the inside, will not slide, by the way that buffer layer 12 is arranged, unmanned plane is placed on easily
When in groove 11, vibration can be reduced, reduce the abrasion to unmanned plane, by the way that radiator fan 4 is arranged, unmanned plane heat dissipation is helped, prolong
The service life of long unmanned plane has good damping effect by being evenly provided with spring 5 between cross bar 1 and bottom plate 6
There is cushion 8 in fruit, the bottom of bottom plate 6 by the fixed adhesion of adhesive glue, has the function that level 2 buffering, effectively reduces unmanned plane
The impact force generated when land, protects unmanned plane, is airbag structure by setting bottom plate 6, and the side fixation of bottom plate 6 is set
It is equipped with valve cock 7, is connected in valve cock 7 and bottom plate 6, unmanned plane is avoided and is sunk in rivers and lakes when breaking down, passed through
Telescopic rod 9 is set, telescoping switch 10 is set on telescopic rod 9, PLC controller is set on telescoping switch 10, PLC controller with nothing
The connection of Human-machine Control end reduces unmanned plane during flying resistance, so that unmanned plane during flying convenient for the support frame contraction in unmanned plane during flying
It is more steady, avoid the problem that support frame resistance in flight is balanced compared with havoc unmanned plane during flying, and convenient in flight
Unmanned plane can normally pass through narrow space, and avoiding support frame and expanding unmanned plane volume makes it can not be in narrow sky
Between the problem of carrying out normal flight, other component can be placed by the way that steel wire 17 is arranged, on steel wire 17, be convenient for loading, should
Unmanned plane support frame designs reasonable and practical, easy to operate, is suitble to promote the use of.
In the description of the present invention, it is to be understood that, term " coaxial ", " bottom ", " one end ", " top ", " middle part ",
The orientation or positional relationship of the instructions such as " other end ", "upper", " side ", " top ", "inner", " front ", " center ", " both ends " is
It is based on the orientation or positional relationship shown in the drawings, is merely for convenience of description of the present invention and simplification of the description, rather than instruction or dark
Show that signified device or element must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as pair
Limitation of the invention.
In addition, term " first ", " second ", " third ", " the 4th " are used for description purposes only, and should not be understood as instruction or
It implies relative importance or implicitly indicates the quantity of indicated technical characteristic, define " first ", " second ", " the as a result,
Three ", the feature of " the 4th " can explicitly or implicitly include at least one of the features.
In the present invention unless specifically defined or limited otherwise, term " installation ", " setting ", " connection ", " fixation ",
Terms such as " being screwed on " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or integral；It can be with
It is mechanical connection, is also possible to be electrically connected；It can be directly connected, two can also be can be indirectly connected through an intermediary
The interaction relationship of connection or two elements inside a element, unless otherwise restricted clearly, for the common of this field
For technical staff, the specific meanings of the above terms in the present invention can be understood according to specific conditions.
Finally, it should be noted that the foregoing is only a preferred embodiment of the present invention, it is not intended to restrict the invention,
Although the present invention is described in detail referring to the foregoing embodiments, for those skilled in the art, still may be used
To modify the technical solutions described in the foregoing embodiments or equivalent replacement of some of the technical features.
All within the spirits and principles of the present invention, any modification, equivalent replacement, improvement and so on should be included in of the invention
Within protection scope.
Claims (6)
1. a kind of Collapsible support for unmanned plane, it is characterised in that: including cross bar, connecting rod, support frame and radiation air
Fan, the cross bar are equipped with two side by side, are welded with two connecting rods, the cross bar and connecting rod between two cross bars in parallel
Between be fixed with steel wire, the bottom of the cross bar is connected with bottom plate by spring, the bottom plate is airbag structure, and bottom plate
Side is fixedly installed valve cock, is connected in the valve cock and bottom plate, the bottom of the bottom plate is additionally provided with cushion, the cross
It is set on bar there are four telescopic rod, the top of the telescopic rod is fixed on the support frame, and the telescopic rod is equipped with telescoping switch, institute
It states and opens up fluted above support frame, the bottom of the groove is equipped with buffer layer, is fixed with several bufferings in the buffer layer
Opening is offered on spring, support frame as described above and buffer layer, the bottom of support frame as described above is equipped with radiator fan, the support
The side of frame is equipped with fan swicth, is additionally provided with cell jar in support frame as described above, the cell jar is embedded with battery, described
Telescoping switch and battery are electrically connected, and PLC controller is provided on telescoping switch, the PLC controller and and unmanned plane
Control terminal connection.
2. a kind of Collapsible support for unmanned plane according to claim 1, it is characterised in that: in the buffer layer
Also it is uniformly provided with foam.
3. a kind of Collapsible support for unmanned plane according to claim 1, it is characterised in that: the telescopic rod packet
Casing and support column are included, screw hole is offered on casing, matches in screw hole and is arranged with holding screw.
4. a kind of Collapsible support for unmanned plane according to claim 1, it is characterised in that: the radiator fan
It is electrically connected with fan swicth, the fan swicth and battery are electrically connected.
5. a kind of Collapsible support for unmanned plane according to claim 1, it is characterised in that: the spring is at least
It is arranged four groups, the spring is fixedly connected on cross bar and bottom plate by welding.
6. a kind of Collapsible support for unmanned plane according to claim 1, it is characterised in that: the cushion is
Thickness is not less than the rubber pad of 5mm, and the cushion is adhered to bottom plate by adhesive glue fixation.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910709195.XA CN110341945A (en) | 2019-08-01 | 2019-08-01 | A kind of Collapsible support for unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910709195.XA CN110341945A (en) | 2019-08-01 | 2019-08-01 | A kind of Collapsible support for unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110341945A true CN110341945A (en) | 2019-10-18 |
Family
ID=68183709
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910709195.XA Pending CN110341945A (en) | 2019-08-01 | 2019-08-01 | A kind of Collapsible support for unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110341945A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114620653A (en) * | 2022-04-06 | 2022-06-14 | 山西八建集团有限公司 | High-safety electric hanging basket control device and using method thereof |
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| CN109386568A (en) * | 2017-08-04 | 2019-02-26 | 郑州工业应用技术学院 | A kind of unmanned plane landing damping |
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2019
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|---|---|---|---|---|
| CN101234671A (en) * | 2007-11-09 | 2008-08-06 | 陈文杰 | Airplane with falling protecting device |
| CN101239656A (en) * | 2007-11-09 | 2008-08-13 | 陈文杰 | Airplane with falling protecting device airplane with falling protection device |
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20191018 |
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