CN211107123U - Unmanned aerial vehicle wing transport vechicle - Google Patents
Unmanned aerial vehicle wing transport vechicle Download PDFInfo
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- CN211107123U CN211107123U CN201922191289.0U CN201922191289U CN211107123U CN 211107123 U CN211107123 U CN 211107123U CN 201922191289 U CN201922191289 U CN 201922191289U CN 211107123 U CN211107123 U CN 211107123U
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- unmanned aerial
- aerial vehicle
- vehicle wing
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- wing
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Abstract
The utility model discloses an unmanned aerial vehicle wing transport vechicle, include: the lower part of the bottom frame is provided with at least two pairs of wheels; the upper supports are arranged along the length direction of the bottom frame, the lower parts of the upper supports are hinged with the fence, and the upper parts of each pair of upper supports are connected in an openable manner; the upper surface of the first shock absorption filling piece is provided with a groove matched with the wing structure of the unmanned aerial vehicle; the lower part of the second shock absorption filling part is provided with a groove matched with the wing structure of the unmanned aerial vehicle; through set up first shock attenuation filler in the rail of bottom frame, the unmanned aerial vehicle wing can be put into rather than the recess that the structure matches, set up second shock attenuation filler in a plurality of upper portion supports, thereby guarantee that the unmanned aerial vehicle wing between second shock attenuation filler and the first shock attenuation filler is laminated and fixed, reduce the vibration to the unmanned aerial vehicle wing in the transportation, improve the stability and the efficiency of unmanned aerial vehicle wing transportation, guarantee the transportation safety of unmanned aerial vehicle wing, reduce the human cost.
Description
Technical Field
The utility model belongs to unmanned aerial vehicle haulage equipment field, more specifically relates to an unmanned aerial vehicle wing transport vechicle.
Background
Due to the special shape of the wings of the unmanned aerial vehicle, the conventional transportation mode is difficult to meet the transportation requirements of the wings of the unmanned aerial vehicle. If no suitable wing transport vehicle exists, great trouble is caused to the wing transport of the unmanned aerial vehicle, the manpower transport cost is increased, a large amount of time and financial resources are wasted, and the transport efficiency is low, so that the wing transport of the unmanned aerial vehicle is a problem to be solved in the field of aerospace.
Therefore, a device suitable for wing transportation of the unmanned aerial vehicle is to be provided, and reliable and stable guarantee is provided for the transportation of the wings of the unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing an unmanned aerial vehicle wing transport vechicle improves wing conveying efficiency, guarantees the reliability of unmanned aerial vehicle wing transportation.
In order to achieve the above object, the utility model provides an unmanned aerial vehicle wing transport vechicle, include:
the device comprises a bottom frame, a driving device and a driving device, wherein a fence is enclosed at the upper edge of the bottom frame, and at least two pairs of wheels are arranged at the lower part of the bottom frame;
a plurality of pairs of upper brackets, the upper brackets being arranged along the length direction of the bottom frame, the lower portions of the upper brackets being hinged to the rail, and the upper portions of each pair of upper brackets being openably and closably connected;
the first shock absorption filling piece is arranged in the fence, and a groove matched with the wing structure of the unmanned aerial vehicle is formed in the upper surface of the first shock absorption filling piece;
a plurality of second shock attenuation infill, the lower part of second shock attenuation infill be equipped with unmanned aerial vehicle wing structure assorted recess, the second shock attenuation infill set up in a pair in the upper portion support.
Preferably, the upper support includes a vertical portion and a horizontal portion connected to one end of the vertical portion, the other end of the vertical portion is hinged to the rail, and the horizontal portions of each pair of the upper supports are openably and closably connected.
Preferably, the horizontal portions of each pair of the upper brackets are connected by a snap lock.
Preferably, the bottom frame comprises an upper frame and a lower frame which are arranged in parallel, and a plurality of shock absorbers are arranged between the upper frame and the lower frame.
Preferably, the heights of the pairs of upper brackets are sequentially increased along the length direction of the bottom frame.
Preferably, the heights of the second shock-absorbing fillers are sequentially increased in matching with the height of the upper bracket.
Preferably, the first shock absorption filling member is a plurality of sections, and each section of the first shock absorption filling member is sequentially arranged in the fence along the length direction of the bottom frame.
Preferably, the first and/or second shock-absorbing filling members are made of pearl wool foam.
Preferably, both ends of the bottom frame are respectively provided with a traction fixing piece.
Preferably, the bottom frame is formed by welding steel square pipes.
The beneficial effects of the utility model reside in that: through set up first shock attenuation filler in the rail of bottom frame, the unmanned aerial vehicle wing can be put into rather than the recess that the structure matches, set up second shock attenuation filler in a plurality of upper portion supports, the lower part and the unmanned aerial vehicle wing shape of second shock attenuation filler match, the upper portion support is fixed with second shock attenuation filler, thereby guarantee second shock attenuation filler and first shock attenuation filler and unmanned aerial vehicle wing laminating and fixed, reduce the vibration to the unmanned aerial vehicle wing in the transportation, improve the stability and the efficiency of unmanned aerial vehicle wing transportation, the transportation safety of guarantee unmanned aerial vehicle wing, reduce the human cost.
Other features and advantages of the present invention will be described in detail in the detailed description which follows.
Drawings
The invention will be described in more detail below with reference to the accompanying drawings. While the preferred embodiments of the present invention have been illustrated in the accompanying drawings, it is to be understood that the invention may be embodied in various forms and should not be limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the invention to those skilled in the art.
Fig. 1 shows a front view of an unmanned aerial vehicle wing transport vehicle according to an embodiment of the present invention.
Fig. 2 shows a top view of an unmanned aerial vehicle wing transport vehicle according to an embodiment of the present invention.
Fig. 3 shows a left side view of an unmanned aerial vehicle wing transport vehicle according to an embodiment of the present invention.
Fig. 4 shows a schematic diagram of an installation step one of an unmanned aerial vehicle wing transport vehicle according to an embodiment of the present invention.
Fig. 5 shows a schematic diagram of an installation step two of the unmanned aerial vehicle wing transport vehicle according to an embodiment of the present invention.
Fig. 6 shows a schematic diagram of an installation step three of the unmanned aerial vehicle wing transport vehicle according to an embodiment of the present invention.
Fig. 7 shows a schematic diagram of a fourth installation step of the unmanned aerial vehicle wing transport vehicle according to an embodiment of the present invention.
Description of reference numerals:
1. a bottom frame; 2. a fence; 3. an upper bracket; 4. a first cushion filler; 5. a second cushion filler; 6. a wheel; 7. pulling the fixed part; 8. locking; 9. a shock absorber; 10. a horizontal portion; 11. a vertical portion.
Detailed Description
Preferred embodiments of the present invention will be described in more detail below. While the following describes preferred embodiments of the present invention, it should be understood that the present invention may be embodied in various forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the invention to those skilled in the art.
According to the utility model discloses unmanned aerial vehicle wing transport vechicle, include:
the device comprises a bottom frame, a rail, a driving device and a driving device, wherein the upper edge of the bottom frame is surrounded by the rail, and the lower part of the bottom frame is provided with at least two pairs of wheels; the upper supports are arranged along the length direction of the bottom frame, the lower parts of the upper supports are hinged with the fence, and the upper parts of each pair of upper supports are connected in an openable manner; the first shock absorption filling piece is arranged in the fence, and a groove matched with the wing structure of the unmanned aerial vehicle is formed in the upper surface of the first shock absorption filling piece; a plurality of second shock attenuation infill, the lower part of second shock attenuation infill be equipped with unmanned aerial vehicle wing structure assorted recess, second shock attenuation infill set up in a pair of upper portion support.
Arranging a first shock absorption filling part in a fence of a bottom frame, wherein the upper surface of the first shock absorption filling part is provided with a groove matched with the wing structure of the unmanned aerial vehicle, the wing of the unmanned aerial vehicle is inserted in the groove in the first shock absorption filling part along the length direction of the wing, grooves matched with the wing structure of the unmanned aerial vehicle are arranged at the lower parts of a plurality of second shock absorption filling parts, the second shock absorption filling parts are inserted on the wing of the unmanned aerial vehicle at the upper part of the first shock absorption filling part, the lower parts of each pair of upper supports are hinged with the fence, so that the upper supports are respectively overturned towards two sides of the bottom frame, the upper supports are put down before the wing is loaded, the second shock absorption filling parts are fixed after the wing is loaded, the wing unmanned aerial vehicle is attached and fixed with the first shock absorption filling part and the second shock absorption filling part, the vibration to the wing of the unmanned aerial vehicle in the transportation process is reduced, the transportation safety of unmanned aerial vehicle wing is ensured, and the human cost is reduced.
As one example, the vehicle employs universal wheels to facilitate steering of the transporter. A steel plate with the thickness of 10mm is welded on the lower portion of the bottom frame, and a mounting seat of the wheel is fixed with the steel plate to ensure that the wheel is firmly connected with the bottom frame.
Preferably, the upper support includes a vertical portion and a horizontal portion connected to one end of the vertical portion, the other end of the vertical portion is hinged to the fence, and the horizontal portions of each pair of upper supports are openably and closably connected.
Specifically, when a pair of upper portion support was buckled, can be fixed in the fixed space that vertical portion and horizontal part enclose with second shock attenuation filling member in, the upper portion and the both sides of second shock attenuation filling member are laminated in horizontal part and vertical portion respectively to make inorganic wing firmly fixed in second shock attenuation filling member and first shock attenuation filling member, reduce the vibration in the transportation, guarantee the reliability of unmanned aerial vehicle wing transportation.
Preferably, the horizontal portions of each pair of upper brackets are connected by a snap lock. The staff can manually buckle and open the lock catches of each pair of horizontal parts, thereby realizing the opening and closing of the upper support.
As preferred scheme, the bottom frame includes parallel arrangement's upper frame and lower floor's frame, is equipped with a plurality of bumper shock absorbers between upper frame and the lower floor's frame, can greatly reduce the influence of vibrations in the transportation to the unmanned aerial vehicle wing.
Preferably, the heights of the plurality of pairs of upper supports are sequentially increased along the length direction of the bottom frame.
Preferably, the heights of the second shock-absorbing filling members are sequentially increased in matching with the height of the upper bracket.
Specifically, for the curved structure of adaptation unmanned aerial vehicle wing, the height of upper portion support increases progressively in proper order to and the height of the second shock attenuation filler piece that matches with it increases progressively in proper order, make second shock attenuation filler piece firmly fix in upper portion support.
As an example, the vertical part of the upper bracket is made of a telescopic sleeve, and the sleeve is provided with a clamping hole which can enable the height of the sleeve to be fixed, so that the fixation of various wings is met.
As preferred scheme, first shock attenuation filler is the multistage, and every section of first shock attenuation filler sets gradually in the rail along bottom frame length direction, and the installation and the dismantlement of the first shock attenuation filler of being convenient for also make things convenient for the groove shape of the first shock attenuation filler rather than corresponding according to the local shape adjustment of different unmanned aerial vehicle wings.
Preferably, the first and/or second cushion filler members are made of pearl wool foam.
As an example, the first shock-absorbing filling member and/or the second shock-absorbing filling member is made of light and durable pearl cotton foam, and is grooved according to the shape of the wing of the unmanned aerial vehicle.
Preferably, the two ends of the bottom frame are respectively provided with a traction fixing piece.
As an example, the towing fixture is provided with a plurality of screw holes, and the unmanned aerial vehicle wing transport vehicle is fixed in the container through bolts.
Preferably, the bottom frame is formed by welding steel square pipes.
As an example, the bottom frame is welded with 50mmx30mm steel square tubes with a wall thickness of 4 mm.
Examples
Figure 1 shows a front view of an unmanned aerial vehicle wing transporter according to one embodiment of the present invention,
fig. 2 shows according to the utility model discloses an embodiment's top view of unmanned aerial vehicle wing transport vechicle, fig. 3 shows according to the utility model discloses an embodiment's left side view of unmanned aerial vehicle wing transport vechicle, fig. 4 shows according to the utility model discloses an embodiment's mounting step a's schematic diagram, fig. 5 shows according to the utility model discloses an embodiment's mounting step two's schematic diagram, fig. 6 shows according to the utility model discloses an embodiment's mounting step three's schematic diagram, fig. 7 shows according to the utility model discloses an embodiment's mounting step four's schematic diagram of unmanned aerial vehicle wing transport vechicle.
As shown in fig. 1-3, the unmanned aerial vehicle wing transport vehicle of this embodiment includes:
the device comprises a bottom frame 1, wherein a fence 2 is enclosed at the upper edge of the bottom frame 1, and at least two pairs of wheels 6 are arranged at the lower part of the bottom frame 1; a plurality of pairs of upper supports 3, the plurality of pairs of upper supports 3 are arranged along the length direction of the bottom frame 1, the lower parts of the upper supports 3 are hinged with the fence 2, and the upper parts of each pair of upper supports 3 are connected in an openable manner; the first shock absorption filling piece 4 is arranged in the fence 2, and a groove matched with the wing structure of the unmanned aerial vehicle is formed in the upper surface of the first shock absorption filling piece 4; a plurality of second shock attenuation infill 5, the lower part of second shock attenuation infill 5 be equipped with unmanned aerial vehicle wing structure assorted recess, second shock attenuation infill 5 sets up in a pair of upper portion support 3.
The upper frame 3 includes a vertical portion 11 and a horizontal portion 10 connected to one end of the vertical portion 11, the other end of the vertical portion 11 is hinged to the fence 2, and the horizontal portions 10 of each pair of upper frames 3 are openably and closably connected. Every horizontal part 10 to upper bracket 3 passes through hasp 8 to be connected, bottom frame 1 includes parallel arrangement's upper frame and lower floor's frame, be equipped with a plurality of bumper shock absorbers 9 between upper frame and the lower floor's frame, length direction along bottom frame 1, it increases progressively in proper order to many height to upper bracket 3, the height of second shock attenuation filler 5 and upper bracket 3 highly assorted increase progressively in proper order, first shock attenuation filler 4 is the multistage, every section first shock attenuation filler 4 sets gradually in rail 2 along 1 length direction of bottom frame, first shock attenuation filler 4 and/or second shock attenuation filler 5 are made by the cotton foam of pearl, the both ends of bottom frame 1 are equipped with respectively and pull mounting 7, bottom frame 1 is formed by the welding of steel side pipe.
As shown in fig. 4-7, transporting wings using the unmanned airplane wing transport vehicle includes the following steps:
the method comprises the following steps: moving the unmanned aerial vehicle wing transport vehicle to the side of the unmanned aerial vehicle wing to be transported;
step two: turning over an upper support 3 of the unmanned aerial vehicle wing transport vehicle to open towards two sides of a bottom frame 1;
step three: sequentially placing the first shock absorption filling parts 4 into the fence 2 of the bottom frame 1, and placing the second shock absorption filling parts 5 at one side of the bottom frame 1 for later use;
step four: firstly, mounting the tail wing at the middle position of the unmanned aerial vehicle, and then placing the tail wing of the unmanned aerial vehicle into the groove corresponding to the first shock absorption filling part 4; inserting the groove of the second shock-absorbing filling piece 5 into the wing of the unmanned aerial vehicle corresponding to the upper bracket 3;
step five: the upper bracket 3 is folded, the main wing is fixed, and the lock catch 8 is fastened.
If need put down unmanned aerial vehicle wing from the transport vechicle, only need according to above-mentioned flow opposite can, do not eat here again
The foregoing description of the embodiments of the invention has been presented for purposes of illustration and not limitation, and is not intended to be exhaustive or limited to the embodiments disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art without departing from the scope and spirit of the illustrated embodiments.
Claims (10)
1. An unmanned aerial vehicle wing transport vechicle, its characterized in that includes:
the device comprises a bottom frame (1), wherein a fence (2) is enclosed at the upper edge of the bottom frame (1), and at least two pairs of wheels (6) are arranged at the lower part of the bottom frame (1);
the upper supports (3) are arranged along the length direction of the bottom frame (1), the lower parts of the upper supports (3) are hinged with the fence (2), and the upper parts of the upper supports (3) are connected in an openable manner;
the first shock absorption filling piece (4) is arranged in the fence (2), and a groove matched with an unmanned aerial vehicle wing structure is formed in the upper surface of the first shock absorption filling piece (4);
a plurality of second shock attenuation infill (5), the lower part of second shock attenuation infill (5) be equipped with unmanned aerial vehicle wing structure assorted recess, second shock attenuation infill (5) set up in a pair of in upper portion support (3).
2. The unmanned aerial vehicle wing transporter according to claim 1, wherein the upper bracket (3) comprises a vertical portion (11) and a horizontal portion (10) connected to one end of the vertical portion (11), the other end of the vertical portion (11) being hinged to the fence (2), the horizontal portion (10) of each pair of upper brackets (3) being openably and closably connected.
3. The unmanned aerial vehicle wing transporter according to claim 2, wherein the horizontal portions (10) of each pair of the upper brackets (3) are connected by a latch (8).
4. The unmanned aerial vehicle wing transporter of claim 1, wherein the bottom frame (1) comprises an upper frame and a lower frame arranged in parallel, and a plurality of shock absorbers (9) are arranged between the upper frame and the lower frame.
5. The unmanned aerial vehicle wing transporter of claim 1, wherein the height of the pairs of upper brackets (3) increases sequentially along the length of the bottom frame (1).
6. Unmanned aerial vehicle wing transporter according to claim 5, characterized in that the height of the second shock-absorbing filling (5) is successively increasing in matching relation to the height of the upper support (3).
7. The unmanned aerial vehicle wing transporter of claim 1, wherein the first shock absorbing filler (4) is a plurality of segments, and each segment of the first shock absorbing filler (4) is sequentially arranged in the fence (2) along the length direction of the bottom frame (1).
8. Unmanned aerial vehicle wing transporter according to claim 1, wherein the first and/or second shock-absorbing filler (4, 5) is made of pearl wool foam.
9. Unmanned aerial vehicle wing transporter according to claim 1, characterized in that both ends of the bottom frame (1) are provided with traction fixtures (7), respectively.
10. The unmanned aerial vehicle wing transporter according to claim 1, wherein the bottom frame (1) is welded from steel square tubes.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922191289.0U CN211107123U (en) | 2019-12-06 | 2019-12-06 | Unmanned aerial vehicle wing transport vechicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922191289.0U CN211107123U (en) | 2019-12-06 | 2019-12-06 | Unmanned aerial vehicle wing transport vechicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211107123U true CN211107123U (en) | 2020-07-28 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922191289.0U Active CN211107123U (en) | 2019-12-06 | 2019-12-06 | Unmanned aerial vehicle wing transport vechicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211107123U (en) |
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2019
- 2019-12-06 CN CN201922191289.0U patent/CN211107123U/en active Active
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