CN209112422U - A kind of combined type vertical take-off and landing drone easy to disassemble with vanning - Google Patents
A kind of combined type vertical take-off and landing drone easy to disassemble with vanning Download PDFInfo
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- CN209112422U CN209112422U CN201821742821.2U CN201821742821U CN209112422U CN 209112422 U CN209112422 U CN 209112422U CN 201821742821 U CN201821742821 U CN 201821742821U CN 209112422 U CN209112422 U CN 209112422U
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- fuselage
- shoe
- airfoil
- intermediate airfoil
- wing
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Abstract
The utility model discloses a kind of combined type vertical take-off and landing drone easy to disassemble with vanning, it include: fuselage, it is connect below the fuselage with undercarriage, the fuselage rear is equipped with engine, a blade is connected on the engine, the top of the fuselage is connected with intermediate airfoil, the intermediate airfoil is spliced with left winger, outside right forward, the rear end part of the left winger is port aileron, left horn and left shoe are installed on the left of the intermediate airfoil, right side structure is identical as left side, and left shoe is connect with empennage jointly with right shoe.The utility model realizes the fast quick-detach between each component of unmanned plane, the storage volume for substantially reducing unmanned plane saves transportation cost, while the unmanned plane can carry out segmentation manufacture with all parts, the manufacture processing cost of unmanned plane production is reduced, mass production is convenient for.
Description
Technical field
The utility model relates to unmanned plane manufacturing field, specially a kind of combined type VTOL easy to disassemble with vanning
Unmanned plane.
Background technique
Vertical take-off and landing drone has both the advantages of gyroplane and fixed-wing unmanned plane, both can as gyroplane VTOL,
Hovering, and have the characteristics that fixed-wing unmanned plane speed is fast, voyage is remote, there is preferable development prospect.By to all types of
The analysis of vertical take-off and landing drone, discovery combined type VTOL fixed-wing unmanned plane compared to other vertical take-off and landing drone,
Have many advantages, such as that technology realizability is strong, high stability, cost is relatively low.But the wing developed dimension of fixed-wing unmanned plane compared with
Greatly, occupied space is more, brings difficulty to manufacture, transport, preservation etc., is unfavorable for producing in batches and storing and carry.
Utility model content
The purpose of this utility model is to provide a kind of combined type vertical take-off and landing drone easy to disassemble with vanning, with solution
Certainly problems set forth above.
To achieve the above object, the utility model provides the following technical solutions: a kind of combined type easy to disassemble with vanning
Vertical take-off and landing drone, including unmanned aerial vehicle body accessory, wing accessory, connection buckle and Joining clasp, the unmanned aerial vehicle body
Accessory includes fuselage, undercarriage, engine and fuselage upper cover, and the wing accessory includes outside right forward, starboard aileron, right arm, the right side
Shoe, intermediate airfoil, left horn, left shoe, left winger, port aileron and empennage, the fuselage lower section is connect with undercarriage, described
The top of fuselage is connected with intermediate airfoil, and the intermediate airfoil is spliced with left winger, outside right forward, the rear end of the left winger
Part is port aileron, is equipped with left horn and left shoe on the left of the intermediate airfoil, right side structure is identical as left side, the left side
Shoe is connect with empennage jointly with right shoe；
The fuselage is equipped with connecting hole, fuselage upper cover and engine, and the junction of the fuselage and intermediate airfoil is equipped with
Connecting hole, the engine are mounted on the rear of fuselage, are fuselage upper cover above the first half of the fuselage；
The fixation device of the intermediate airfoil is made of fixation hole, the first dowel hole and first end of thread, and described first
The junction of intermediate airfoil and horn is arranged in dowel hole, and the connection of intermediate airfoil and shoe is arranged in first end of thread
The stitching portion of intermediate airfoil and fuselage is arranged in place, the fixation hole；
The fixed device of the side wing is made of the first electric connector, supporting square tube and connector, the supporting square tube setting
In the junction of Bian Yiyu intermediate airfoil, the left side of the supporting square tube is equipped with the first electric connector, the right side of the supporting square tube
Side is equipped with a connector；
The fixed device of the shoe is made of connector nut, the second electric connector, the second dowel hole, the connector
Nut is arranged in the junction of shoe and intermediate airfoil, is equipped with the second electric connector inside the connector nut, and described second
The side of electric connector is equipped with the second dowel hole；
The empennage is made of vertical fin, horizontal tail and second end of thread, and empennage and shoe is arranged in second end of thread
Junction.
Preferably, the quick-disassembly structure part between the unmanned aerial vehicle body accessory and wing accessory is that aluminium is added by CNC
Integral structure part made of work technique.
Preferably, the junction of the left winger and intermediate airfoil is equipped with a connection buckle, the connection buckle and company
Snap ring is connect to be fixed.
Preferably, the connecting hole with intermediate airfoil assembling, the company of the intermediate airfoil and fuselage are provided on the fuselage
It meets place and is equipped with fixation hole.
Preferably, it is mounted on a rotor motor on the left horn, left shoe, engine, right arm and right shoe,
And it is connected separately with a blade.
Preferably, the unmanned aerial vehicle body accessory and wing accessory can be dismantled and be cased respectively to fuselage packing case and machine
In wing components packing box, the unmanned aerial vehicle body accessory is placed on fuselage packaging material, and tool box is placed on the fuselage packaging material, is flown
Row battery charger, fixed-wing mode battery, rotor mode battery, engine primer battery and engine primer, it is described
Remote controler is placed on airfoil member packing case, the wing accessory layering is assemblied in the upper half storey of airfoil member packing case.
Preferably, the undercarriage is fixed by goat's horn nut with fuselage.
The technical effect and advantage of the utility model: compared with prior art, between the utility model UAV Components
Fast quick-detach substantially reduces the storage volume of VTOL fixed-wing unmanned plane, convenient for storage and carries, saves at nobody
Cost during machine packed and transported；Protection unmanned plane propeller and unmanned plane body are had also achieved simultaneously, are prevented in transit
The purpose collided with and damaged；The unmanned plane complete machine device for quickly disassembling can make fixed-wing unmanned plane all parts carry out segmentation system simultaneously
It makes, reduces the manufacture processing cost of unmanned plane production, produced convenient for unmanned plane rapid batch metaplasia.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the top view of the utility model；
Fig. 3 is the main view of the utility model；
Fig. 4 is the side view of the utility model；
Fig. 5 is the structure disassembly diagram of the utility model；
Fig. 6 is the airframe structure schematic diagram of the utility model；
Fig. 7 is the accessory figure of the intermediate airfoil of the utility model；
Fig. 8 is the side wing assembling fittings figure of the utility model；
Fig. 9 is the shoe structural schematic diagram of the utility model；
Figure 10 is the empennage block diagram of the utility model；
Figure 11 is the Bian Yiyu intermediate airfoil connection buckle structural schematic diagram of the utility model；
Figure 12 is the vanning laying method schematic diagram of the utility model.
Description of symbols: 1 outside right forward, 2 starboard ailerons, 3 right arms, 4 right shoes, 5 intermediate airfoils, 6 fuselages, 7 are risen and fallen
Frame, 8 left horns, 9 left shoes, 10 left wingers, 11 port ailerons, 12 empennages, 13 engines, 14 fuselage upper covers, 15 connecting holes, 16 feet
Frame goat's horn nut, 17 first dowel holes, 18 fixation holes, 19 first ends of thread, 20 first electric connectors, 21 supporting square tubes, 22
Connector, 23 blades, 24 rotor motors, 25 connector nuts, 26 second appliance plugs, 27 second dowel holes, 28 vertical fins,
29 second ends of thread, 30 horizontal tails, 31 connection buckles, 32 Joining clasps, 33 fuselage packing cases, 34 fuselage packaging materials, 35 tool boxes,
36 flight battery chargers, 37 fixed-wing mode batteries, 38 rotor mode batteries, 39 engine primer batteries, 40 engines
Starter, 41 airfoil member packing cases, 42 wing packaging materials, 43 remote controlers.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
It is easy to disassemble vertical take-off and landing unmanned with the combined type of vanning that the utility model provides one kind as shown in figs. 1-12
Machine, including outside right forward 1, starboard aileron 2, right arm 3, right shoe 4, intermediate airfoil 5, fuselage 6, undercarriage 7, left horn 8, left shoe
9, left winger 10, port aileron 11, empennage 12, engine 13, fuselage upper cover 14, connecting hole 15, foot prop goat's horn nut 16, first are fixed
Position pin hole 17, fixation hole 18, first end of thread 19, the first electric connector 20, supporting square tube 21, connector 22, blade 23, rotor
Motor 24, connector nut 25, the second appliance plug 26, the second dowel hole 27, vertical fin 28, second end of thread 29, horizontal tail
30, connection buckle 31, Joining clasp 32, fuselage packing case 33, fuselage packaging material 34, tool box 35, flight battery charger 36, solid
Determine wing mode battery 37, rotor mode battery 38, engine primer battery 39, engine primer 40, airfoil member packaging
Case 41, wing packaging material 42 and remote controler 43,6 lower section of fuselage are connect with undercarriage 7, the top of the fuselage 6 and intermediate machine
The wing 5 is connected, and the intermediate airfoil 5 is spliced with left winger 10, outside right forward 1, and the rear end part of the left winger 10 is left secondary
The wing 11, the left side of the intermediate airfoil 5 are equipped with left horn 8 and left shoe 9, and right side structure is identical as left side, the left shoe 9
It is connect jointly with empennage 12 with right shoe 4；
The fuselage 6 is equipped with connecting hole 15, fuselage upper cover 14 and engine 13, the company of the fuselage 6 and intermediate airfoil 5
It meets place and is equipped with connecting hole 15, it is on fuselage above the first half of the fuselage 6 that the engine 13, which is mounted on the rear of fuselage 6,
Lid 14；
The fixation device of the intermediate airfoil 5 is made of fixation hole 18, the first dowel hole 17 and first end of thread 19,
The junction of intermediate airfoil 5 Yu horn is arranged in first dowel hole 17, and first end of thread 19 is arranged in intermediate machine
The stitching portion of intermediate airfoil 5 Yu fuselage 6 is arranged in the junction of the wing 5 and shoe, the fixation hole 18；
The fixed device of the side wing is made of the first electric connector 20, supporting square tube 21 and connector 22, the support side
The junction of Bian Yiyu intermediate airfoil 5 is arranged in pipe 21, and the left side of the supporting square tube 21 is equipped with the first electric connector 20, described
The right side of supporting square tube 21 is equipped with a connector；
The fixed device of the shoe is made of connector nut 25, the second electric connector 26, the second dowel hole 27, institute
The junction that shoe Yu intermediate airfoil 5 is arranged in connector nut 25 is stated, it is electrical to be equipped with second inside the connector nut 25
The side of plug 26, second electric connector 26 is equipped with the second dowel hole 27；
The empennage 12 is made of vertical fin 28, horizontal tail 30 and second end of thread 29, and second end of thread 29 is arranged in tail
The junction of the wing 12 and shoe.
Specifically, the quick-disassembly structure part between the unmanned plane either component is aluminium production, matter if CNC workpiece
Amount is ensured.
Specifically, the junction of the left winger 10 and intermediate airfoil 5 is equipped with a connection buckle 31, the connection buckle
31 fix with Joining clasp 32, snap connection mode more light and flexible, effectively increase disassembly packaging efficiency.
Specifically, being provided with the connecting hole 15 assembled with intermediate airfoil 5, the intermediate airfoil 5 and fuselage on the fuselage 6
6 junction is equipped with fixation hole 18, convenient for being fixedly connected.
Specifically, being mounted on a rotation on the left horn 8, left shoe 9, engine 13, right arm 3 and right shoe 4
Stability when wing motor 24, and be connected separately with a blade 23, multiple blades 23 can guarantee unmanned plane operation and controllable
Property, keep its more flexible.
Specifically, the unmanned plane is detachably cased to fuselage packing case 33 and airfoil member packing case 41, it is described nobody
Machine fuselage accessory is placed on fuselage packaging material 34, and tool box 35 is placed on the fuselage packaging material 34, flight battery charger 36, is consolidated
Determine wing mode battery 37, rotor mode battery 38, engine primer battery 39 and engine primer 40, the wing portion
It is placed with remote controler 43 on part packing case 41, the wing accessory layering is assemblied in the upper half storey of airfoil member packing case 41, can be with
The effective transportation problem for guaranteeing unmanned plane.
Specifically, the undercarriage 7 is fixed by foot prop goat's horn nut 16 and fuselage 6, it is easy-to-dismount to combine surely
It is qualitative.
The application method of the utility model: unmanned plane undercarriage 7 is carried out using foot prop goat's horn nut 16 and fuselage 6 to connecting
Lock is completed to fix；The fixation of fuselage 6 and intermediate airfoil 5 needs four fixation holes with screw by 5 rear and front end of intermediate airfoil
18 are torqued-up in the connecting hole 15 of fuselage 6, and specifically available four pieces of M5 screws are fixed；The connection of intermediate airfoil 5 and the side wing need by
Supporting square tube 21 is inserted into the supporting sleeve of intermediate airfoil 5, then the side wing is inserted into along supporting square tube 21, and the two is made mutually to fit, this
When press connection buckle 31 again, lock connection buckle 31 and Joining clasp 32；The connection of horn shoe and intermediate airfoil 5
It is to be realized by the end of thread on horn and shoe, so that the first dowel hole 17 is directed at the insertion of the second dowel hole 27, allow
It is very close to each other between screwing mechanism, the connector thread cap 25 on horn and shoe is tightened along clockwise direction, nobody
The connection type of the tail wing 12 is also such.
Unmanned plane is detachably cased to fuselage packing case 33 and airfoil member packing case 41, and the unmanned aerial vehicle body accessory is put
It sets on fuselage packaging material 34, tool box 35, flight battery charger 36, fixed-wing mode battery is placed on the fuselage packaging material 34
37, rotor mode battery 38, engine primer battery 39 and engine primer 40 are put on the airfoil member packing case 41
There is remote controler 43, the wing accessory layering is assemblied in the upper half storey of airfoil member packing case 41.
Finally, it should be noted that the above descriptions are merely preferred embodiments of the present invention, it is not limited to this
Utility model, although the utility model is described in detail with reference to the foregoing embodiments, for those skilled in the art
For, it is still possible to modify the technical solutions described in the foregoing embodiments, or to part of technical characteristic
It is equivalently replaced, within the spirit and principle of the utility model, any modification, equivalent replacement, improvement and so on,
It should be included within the scope of protection of this utility model.
Claims (7)
1. a kind of combined type vertical take-off and landing drone easy to disassemble with vanning, including unmanned aerial vehicle body accessory, wing accessory, company
Connect buckle (31) and Joining clasp (32), the unmanned aerial vehicle body accessory include fuselage (6), undercarriage (7), engine (13) and
Fuselage upper cover (14), the wing accessory include outside right forward (1), starboard aileron (2), right arm (3), right shoe (4), intermediate airfoil
(5), left horn (8), left shoe (9), left winger (10), port aileron (11) and empennage (12), it is characterised in that: the fuselage
(6) lower section connect with undercarriage (7), the top of the fuselage (6) is connected with intermediate airfoil (5), the intermediate airfoil (5) and
Left winger (10), outside right forward (1) are spliced, and the rear end part of the left winger (10) is port aileron (11), the intermediate airfoil
(5) left horn (8) and left shoe (9) are installed, right side structure is identical as left side, the left shoe (9) and right shoe on the left of
(4) it is connect jointly with empennage (12)；
The fuselage (6) is equipped with connecting hole (15), fuselage upper cover (14) and engine (13), the fuselage (6) and intermediate machine
The junction of the wing (5) is equipped with connecting hole (15), and the engine (13) is mounted on the rear of fuselage (6), before the fuselage (6)
It is above half portion fuselage upper cover (14)；
The fixation device of the intermediate airfoil (5) is by fixation hole (18), the first dowel hole (17) and first end of thread (19) group
At the first dowel hole (17) setting is in the junction of intermediate airfoil (5) and horn, first end of thread (19) setting
In the junction of intermediate airfoil (5) and shoe, stitching portion of fixation hole (18) setting in intermediate airfoil (5) and fuselage (6)；
The fixed device of the side wing is made of the first electric connector (20), supporting square tube (21) and connector (22), the support
In the junction of Bian Yiyu intermediate airfoil (5), it is electrical slotting that the left side of the supporting square tube (21) is equipped with first for square tube (21) setting
The right side of head (20), the supporting square tube (21) is equipped with a connector；
The fixed device of the shoe is made of connector nut (25), the second electric connector (26), the second dowel hole (27), institute
Connector nut (25) setting is stated in the junction of shoe and intermediate airfoil (5), the connector nut (25) is internal equipped with the
The side of two electric connectors (26), second electric connector (26) is equipped with the second dowel hole (27)；
The empennage (12) is made of vertical fin (28), horizontal tail (30) and second end of thread (29), and second end of thread (29) sets
Set the junction in empennage (12) and shoe.
2. one kind according to claim 1 combined type vertical take-off and landing drone easy to disassemble with vanning, it is characterised in that:
Quick-disassembly structure part between the unmanned aerial vehicle body accessory and wing accessory is aluminium one made of CNC processing technology
Change structural member.
3. one kind according to claim 1 combined type vertical take-off and landing drone easy to disassemble with vanning, it is characterised in that:
The junction of the left winger (10) and intermediate airfoil (5) is equipped with a connection buckle (31), the connection buckle (31) and company
Snap ring (32) is connect to fix.
4. one kind according to claim 1 combined type vertical take-off and landing drone easy to disassemble with vanning, it is characterised in that:
The connecting hole (15) with intermediate airfoil (5) assembling, the company of the intermediate airfoil (5) and fuselage (6) are provided on the fuselage (6)
It meets place and is equipped with fixation hole (18).
5. one kind according to claim 1 combined type vertical take-off and landing drone easy to disassemble with vanning, it is characterised in that:
A rotor motor is mounted on the left horn (8), left shoe (9), engine (13), right arm (3) and right shoe (4)
(24), and it is connected separately with a blade (23).
6. one kind according to claim 1 combined type vertical take-off and landing drone easy to disassemble with vanning, it is characterised in that:
The unmanned aerial vehicle body accessory and wing accessory can be dismantled and be cased respectively to fuselage packing case (33) and airfoil member and be packed
In case (41), the unmanned aerial vehicle body accessory is placed on fuselage packaging material (34), is placed with tool box on the fuselage packaging material (34)
(35), flight battery charger (36), fixed-wing mode battery (37), rotor mode battery (38), engine primer battery
(39) and engine primer (40) it, is placed with remote controler (43) on the airfoil member packing case (41), the wing accessory point
Layer is assemblied in the upper half storey of airfoil member packing case (41).
7. one kind according to claim 1 combined type vertical take-off and landing drone easy to disassemble with vanning, it is characterised in that:
The undercarriage (7) is fixed by foot prop goat's horn nut (16) and fuselage (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821742821.2U CN209112422U (en) | 2018-10-26 | 2018-10-26 | A kind of combined type vertical take-off and landing drone easy to disassemble with vanning |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821742821.2U CN209112422U (en) | 2018-10-26 | 2018-10-26 | A kind of combined type vertical take-off and landing drone easy to disassemble with vanning |
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| Publication Number | Publication Date |
|---|---|
| CN209112422U true CN209112422U (en) | 2019-07-16 |
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ID=67202272
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821742821.2U Active CN209112422U (en) | 2018-10-26 | 2018-10-26 | A kind of combined type vertical take-off and landing drone easy to disassemble with vanning |
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| CN (1) | CN209112422U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109720537A (en) * | 2018-10-26 | 2019-05-07 | 深圳市科卫泰实业发展有限公司 | A kind of combined type vertical take-off and landing drone easy to disassemble with vanning |
-
2018
- 2018-10-26 CN CN201821742821.2U patent/CN209112422U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109720537A (en) * | 2018-10-26 | 2019-05-07 | 深圳市科卫泰实业发展有限公司 | A kind of combined type vertical take-off and landing drone easy to disassemble with vanning |
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