CN212766713U - Collapsible many rotor unmanned aerial vehicle - Google Patents
Collapsible many rotor unmanned aerial vehicle Download PDFInfo
- Publication number
- CN212766713U CN212766713U CN202021137270.4U CN202021137270U CN212766713U CN 212766713 U CN212766713 U CN 212766713U CN 202021137270 U CN202021137270 U CN 202021137270U CN 212766713 U CN212766713 U CN 212766713U
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- Prior art keywords
- foot rest
- thick bamboo
- installation section
- mounting hole
- rotor
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- Expired - Fee Related
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- 238000009434 installation Methods 0.000 claims abstract description 35
- 235000017166 Bambusa arundinacea Nutrition 0.000 claims abstract description 34
- 235000017491 Bambusa tulda Nutrition 0.000 claims abstract description 34
- 241001330002 Bambuseae Species 0.000 claims abstract description 34
- 235000015334 Phyllostachys viridis Nutrition 0.000 claims abstract description 34
- 239000011425 bamboo Substances 0.000 claims abstract description 34
- 238000005553 drilling Methods 0.000 abstract 1
- 238000000034 method Methods 0.000 description 2
- 241000425571 Trepanes Species 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
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Abstract
The utility model provides a collapsible many rotor unmanned aerial vehicle, the reciprocating impact tunnel drilling machine comprises a machine body, the top of fuselage is equipped with the connecting plate, be equipped with the first mounting hole of a plurality of and second mounting hole on the connecting plate, be equipped with a foot rest installation section of thick bamboo on the first mounting hole, the other end of foot rest installation section of thick bamboo is equipped with the foot rest pole, the bottom of foot rest pole is equipped with the support foot rest, be equipped with an arm installation section of thick bamboo on the second mounting hole, the other end of an arm installation section of thick bamboo is equipped with the rotor arm. Compared with the prior art: the connecting plate is designed above the machine body, the foot stand mounting cylinder and the machine arm mounting cylinder are connected with the connecting plate through the hinge, so that the foot stand rods and the rotor arms can be rotated and folded, the foot stand rods and the rotor arms do not need to be disassembled during storage, and the foot stand rods and the rotor arms are uniformly folded upwards, so that the space occupation is reduced; the design of connecting sleeve and adapter sleeve, the leg of a foot rest of being convenient for and support leg frame between be connected and rotate, have guaranteed to connect and have made things convenient for when firm and accomodate.
Description
[ technical field ] A method for producing a semiconductor device
The utility model relates to an unmanned aerial vehicle designs technical field, in particular to collapsible many rotor unmanned aerial vehicle.
[ background of the invention ]
The unmanned aerial vehicle is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, has wide application, and is applied to the industries of police, city management, agriculture, geology, meteorology, electric power, emergency rescue and relief, video shooting and the like.
Among the prior art, unmanned aerial vehicle's structure is fixed mostly, because the unable regulation of angle and occupation space of horn and foot rest are great, can't carry out reasonable accomodating, and current unmanned aerial vehicle need be dismantled horn and foot rest when accomodating, during the use, need reassemble again, does so and wastes time and energy.
[ Utility model ] content
An object of the utility model is to provide a collapsible many rotor unmanned aerial vehicle to overcome among the prior art the most fixed not enough of unmanned aerial vehicle structure.
In order to achieve the above object, the utility model provides a following technical scheme:
the application discloses collapsible many rotor unmanned aerial vehicle, including fuselage, connecting plate, a foot rest installation section of thick bamboo, horn installation section of thick bamboo, support foot rest and rotor head, the top of fuselage is equipped with the connecting plate, be equipped with the first mounting hole of a plurality of and second mounting hole on the connecting plate, be equipped with a foot rest installation section of thick bamboo on the first mounting hole, the other end of a foot rest installation section of thick bamboo is equipped with the foot rest pole, the bottom of foot rest pole is equipped with the support foot rest, be equipped with a horn installation section of thick bamboo on the second mounting hole, the other end of a horn installation section of thick bamboo is equipped with the rotor arm, the other end of rotor arm is equipped with the rotor head.
Preferably, the number of first mounting hole is two, first mounting hole with adopt hinged joint between the foot rest installation section of thick bamboo, the number of second mounting hole is four, the second mounting hole with adopt hinged joint between the horn installation section of thick bamboo, the bottom of second mounting hole is equipped with the limiting plate that is used for restricting horn installation section of thick bamboo turned angle.
Preferably, a fixing piece is arranged above the connecting plate, a limiting rod is arranged on the horn installation cylinder, and the other end of the limiting rod is hinged with the fixing piece.
Preferably, the limiting rod is provided with a locking device for controlling the movement of the limiting rod.
Preferably, the bottom of the foot rest rod is provided with a connecting sleeve, the connecting sleeve is provided with a trepanning, the middle of the supporting foot rest is provided with a connecting piece, the connecting piece is provided with a connecting sleeve, and the connecting sleeve is connected with the connecting sleeve.
The utility model has the advantages that:
(1) the connecting plate is designed above the machine body, the foot stand mounting cylinder and the machine arm mounting cylinder are connected with the connecting plate through the hinge, so that the foot stand rods and the rotor arms can be rotated and folded, the foot stand rods and the rotor arms do not need to be disassembled during storage, and the foot stand rods and the rotor arms are uniformly folded upwards, so that the space occupation is reduced;
(2) due to the design of the limiting plate, the limiting rod and the fixing piece, the rotation angle of the rotor arm can be limited, and the influence on the flight performance of the unmanned aerial vehicle caused by overlarge rotation angle of the rotor arm is avoided;
(3) the design of connecting sleeve and adapter sleeve, the leg of a foot rest of being convenient for and support leg frame between be connected and rotate, have guaranteed to connect and have made things convenient for when firm and accomodate.
The features and advantages of the present invention will be described in detail by embodiments with reference to the accompanying drawings.
[ description of the drawings ]
Fig. 1 is a schematic structural view of the foldable multi-rotor unmanned aerial vehicle when unfolded;
FIG. 2 is a schematic view of a connection structure of components at a connection plate according to the present invention;
FIG. 3 is a schematic view of the connection structure of the support leg and the leg rod of the present invention;
fig. 4 is the utility model relates to a structure schematic diagram when collapsible many rotor unmanned aerial vehicle is folding.
In the figure: the aircraft comprises an aircraft body 1, a connecting plate 2, a first mounting hole 21, a second mounting hole 22, a limiting plate 23, a fixing piece 24, a foot rest mounting barrel 3, a foot rest mounting barrel 31, a foot rest rod 32, a connecting sleeve 33, a trepanning hole 4, an aircraft arm mounting barrel 41, a rotor arm 42, a limiting rod 43, a locking device 43, a supporting foot rest 5, a connecting piece 51, a connecting sleeve 52 and a rotor head 6.
[ detailed description ] embodiments
In order to make the objects, technical solutions and advantages of the present invention more clear, the present invention is further described in detail through the accompanying drawings and embodiments. It should be understood, however, that the description herein of specific embodiments is only intended to illustrate the invention and not to limit the scope of the invention. Moreover, in the following description, descriptions of well-known structures and techniques are omitted so as to not unnecessarily obscure the concepts of the present invention.
Referring to fig. 1 to 4, the embodiment of the utility model provides a collapsible many rotor unmanned aerial vehicle, including fuselage 1, connecting plate 2, foot rest installation section of thick bamboo 3, horn installation section of thick bamboo 4, support foot rest 5 and rotor head 6, the top of fuselage 1 is equipped with connecting plate 2, be equipped with the first mounting hole 21 of a plurality of and second mounting hole 22 on the connecting plate 2, be equipped with foot rest installation section of thick bamboo 3 on the first mounting hole 21, the other end of foot rest installation section of thick bamboo 3 is equipped with foot rest pole 31, the bottom of foot rest pole 31 is equipped with support foot rest 5, be equipped with horn installation section of thick bamboo 4 on the second mounting hole 22, the other end of horn installation section of thick bamboo 4 is equipped with rotor arm 41, the other end of rotor arm 41 is equipped with rotor head 6.
The quantity of first mounting hole 21 is two, first mounting hole 21 with adopt hinged joint between the foot rest installation section of thick bamboo 3, the quantity of second mounting hole 22 is four, second mounting hole 22 with adopt hinged joint between the horn installation section of thick bamboo 4, the bottom of second mounting hole 22 is equipped with limiting plate 23 that is used for restricting 4 turned angles of horn installation section of thick bamboo. The upper portion of connecting plate 2 is equipped with mounting 24, be equipped with gag lever post 42 on the horn installation section of thick bamboo 4, the other end of gag lever post 42 with mounting 24 hinged joint. The limiting rod 42 is provided with a locking device 43 for controlling the movement of the limiting rod 42.
The bottom of the foot rest rod 31 is provided with a connecting sleeve 32, the connecting sleeve 32 is provided with a trepan boring 33, the middle part of the supporting foot rest 5 is provided with a connecting piece 51, the connecting piece 51 is provided with a connecting sleeve 52, and the connecting sleeve 52 is connected with the connecting sleeve 32.
The utility model discloses the working process:
the utility model relates to a collapsible many rotor unmanned aerial vehicle is in the course of the work, when accomodating, press locking device 43 and remove the locking to gag lever post 42, upwards rotate the rotor arm 41 folding, until the rotor arm 41 is vertical, rotate supporting leg frame 5, make it parallel with foot rest pole 31, rotate foot rest installation section of thick bamboo 3 again for foot rest pole 31 upwards folds, until foot rest pole 31 is vertical, the completion is folding, thereby has reduced unmanned aerial vehicle's space and has taken, convenient storage.
The above description is only exemplary of the present invention and should not be taken as limiting the scope of the present invention, as any modification, equivalent replacement or improvement made within the spirit and principle of the present invention should be included in the present invention.
Claims (5)
1. The utility model provides a collapsible many rotor unmanned aerial vehicle which characterized in that: including fuselage (1), connecting plate (2), foot rest installation section of thick bamboo (3), an arm installation section of thick bamboo (4), support foot rest (5) and rotor head (6), the top of fuselage (1) is equipped with connecting plate (2), be equipped with the first mounting hole of a plurality of (21) and second mounting hole (22) on connecting plate (2), be equipped with foot rest installation section of thick bamboo (3) on first mounting hole (21), the other end of a foot rest installation section of thick bamboo (3) is equipped with foot rest pole (31), the bottom of foot rest pole (31) is equipped with support foot rest (5), be equipped with an arm installation section of thick bamboo (4) on second mounting hole (22), the other end of an arm installation section of thick bamboo (4) is equipped with rotor arm (41), the other end of rotor arm (41) is equipped with rotor head (6).
2. A foldable multi-rotor drone according to claim 1, characterized in that: the quantity of first mounting hole (21) is two, first mounting hole (21) with adopt hinged joint between the foot rest installation section of thick bamboo (3), the quantity of second mounting hole (22) is four, second mounting hole (22) with adopt hinged joint between the horn installation section of thick bamboo (4), the bottom of second mounting hole (22) is equipped with limiting plate (23) that are used for restricting horn installation section of thick bamboo (4) turned angle.
3. A foldable multi-rotor drone according to claim 1, characterized in that: the upper portion of connecting plate (2) is equipped with mounting (24), be equipped with gag lever post (42) on horn installation section of thick bamboo (4), the other end of gag lever post (42) with mounting (24) hinged joint.
4. A foldable multi-rotor drone according to claim 3, characterized in that: and a locking device (43) for controlling the movement of the limiting rod (42) is arranged on the limiting rod (42).
5. A foldable multi-rotor drone according to claim 1, characterized in that: the bottom of the foot rest rod (31) is provided with a connecting sleeve (32), the connecting sleeve (32) is provided with a trepanning (33), the middle of the support foot rest (5) is provided with a connecting piece (51), the connecting piece (51) is provided with a connecting sleeve (52), and the connecting sleeve (52) is connected with the connecting sleeve (32).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021137270.4U CN212766713U (en) | 2020-06-18 | 2020-06-18 | Collapsible many rotor unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021137270.4U CN212766713U (en) | 2020-06-18 | 2020-06-18 | Collapsible many rotor unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212766713U true CN212766713U (en) | 2021-03-23 |
Family
ID=75073752
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021137270.4U Expired - Fee Related CN212766713U (en) | 2020-06-18 | 2020-06-18 | Collapsible many rotor unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212766713U (en) |
-
2020
- 2020-06-18 CN CN202021137270.4U patent/CN212766713U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210323 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |