CN212580135U - Aircraft with foldable and deformable frame - Google Patents
Aircraft with foldable and deformable frame Download PDFInfo
- Publication number
- CN212580135U CN212580135U CN202021138898.6U CN202021138898U CN212580135U CN 212580135 U CN212580135 U CN 212580135U CN 202021138898 U CN202021138898 U CN 202021138898U CN 212580135 U CN212580135 U CN 212580135U
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- Prior art keywords
- folding
- worm
- machine arm
- horn
- fuselage
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- Expired - Fee Related
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- 238000009434 installation Methods 0.000 claims abstract description 10
- 238000005553 drilling Methods 0.000 abstract 1
- 238000000034 method Methods 0.000 description 4
- 238000010276 construction Methods 0.000 description 2
- 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 an aircraft of collapsible deformation frame, the reciprocating impact tunnel drilling machine comprises a machine body, the fuselage includes front and back baffle, roof and side shield, be equipped with the work worm between the side shield, be equipped with folding horn around between the baffle, the upper end of folding horn is equipped with the worm wheel sleeve, the telescopic front side of worm wheel is equipped with the work worm wheel, work worm wheel and work worm intermeshing, the one end that the fuselage was kept away from to folding horn is equipped with the function horn, the below at both ends is equipped with folding foot rest around the function horn, the top of fuselage is equipped with the cloud platform. Compared with the prior art, the folding machine arm has the advantages that the working worm is designed inside the machine body, and the working worm wheel is designed above the folding machine arm, so that the folding machine arm can be adjusted and rotated through the worm and the worm wheel as required, and the folding machine arm is convenient to store and use; the horn carries out the folding design downwards, does not influence the installation of fuselage top cloud platform for the cloud platform need not to dismantle when accomodating, and is convenient and fast more during the use.
Description
[ technical field ] A method for producing a semiconductor device
The utility model relates to an unmanned vehicles designs technical field, in particular to aircraft of collapsible deformation frame.
[ 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 vehicles's rack construction is fixed mostly, because the angle of horn can't be adjusted, when accomodating, need dismantle the horn, during the use, need reassemble again, and the cloud platform that is used for installing camera equipment above the aircraft also can dismantle when accomodating, reassembles during the use, and the process is very loaded down with trivial details.
[ Utility model ] content
An object of the utility model is to provide an aircraft of collapsible deformation frame to overcome among the prior art not enough that unmanned vehicles's rack construction is most fixed.
In order to achieve the above object, the utility model provides a following technical scheme:
the application discloses aircraft of collapsible deformation frame, including fuselage, folding horn and work worm, baffle, roof and side shield around the fuselage includes, be equipped with the work worm between the side shield, be equipped with the folding horn between the baffle around, the upper end of folding horn is equipped with the worm wheel sleeve, the telescopic front side of worm wheel is equipped with the work worm wheel, work worm wheel and work worm intermeshing, the one end that the fuselage was kept away from to the folding horn is equipped with the function horn, the below at both ends is equipped with folding foot rest around the function horn, the top of folding foot rest is equipped with screw installation axle, the top of fuselage is equipped with the cloud platform.
Preferably, the front end and the rear end of the worm gear sleeve are provided with mounting shafts, mounting holes corresponding to the mounting shafts are formed in front and rear baffles of the machine body, the folding machine arm is connected with the machine body through the mounting shafts and the mounting holes, side holes used for mounting a working worm are formed in the side baffles, and two ends of the working worm are connected with the side holes.
Preferably, the folding machine arm is provided with a shoulder plate, the bottom of the shoulder plate is connected with the folding machine arm through a hinge, and the upper end of the shoulder plate is connected with the side baffle of the machine body through a hinge.
Preferably, the folding machine arm is connected with the functional machine arm through a three-way sleeve.
Preferably, the upper end of the folding foot rest is connected with the functional machine arm through a hinge, a foot rest fixing rod is arranged on the inner side of the lower end of the folding foot rest, and the upper end of the foot rest fixing rod is connected with the functional machine arm.
The utility model has the advantages that: compared with the prior art, the utility model provides a pair of aircraft of collapsible deformation frame, it is rational in infrastructure:
(1) a working worm is designed in the machine body, and a working worm wheel is designed above the folding machine arm, so that the folding machine arm can be adjusted and rotated through the worm and the worm wheel as required, and the folding machine arm is convenient to store and use;
(2) the design that the machine arm is folded downwards does not affect the installation of the cradle head above the machine body, so that the cradle head does not need to be disassembled when being stored, and the use is more convenient and quicker;
(3) folding foot rest and foot rest dead lever's design had both guaranteed that the aircraft can be steady when using to stand, has also made things convenient for accomodating of aircraft simultaneously.
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 an aircraft arm of a foldable and transformable frame of the present invention when unfolded;
fig. 2 is a schematic structural diagram of the folding deformable frame of the aircraft arm of the invention when folded;
fig. 3 is a schematic structural view of the fuselage of the present invention;
fig. 4 is a schematic structural view of the joint between the folding arm and the working worm according to the present invention.
In the figure: 1-machine body, 11-front and rear baffles, 12-top plate, 13-side baffle, 15-mounting hole, 16-side hole, 2-folding machine arm, 21-worm wheel sleeve, 22-working worm wheel, 23-mounting shaft, 3-functional machine arm, 31-three-way sleeve, 4-folding foot rest, 41-foot rest fixing rod, 42-propeller mounting shaft, 5-tripod head, 6-shoulder plate and 7-working worm.
[ 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 an aircraft of collapsible deformation frame, including fuselage 1, folding horn 2 and work worm 7, fuselage 1 includes front and back baffle 11, roof 12 and side shield 13, be equipped with work worm 7 between the side shield 13, be equipped with folding horn 2 around between the baffle 11, the upper end of folding horn 2 is equipped with worm wheel sleeve 21, the front side of worm wheel sleeve 21 is equipped with work worm wheel 22, work worm wheel 22 and work worm 7 intermeshing, the one end that fuselage 1 was kept away from to folding horn 2 is equipped with function horn 3, the below at both ends is equipped with folding foot rest 4 around function horn 3, the top of folding foot rest 4 is equipped with screw 42, the top of fuselage 1 is equipped with mounting shaft 5.
Both ends are equipped with installation axle 23 around worm wheel sleeve 21, be equipped with on the baffle 11 around fuselage 1 with the corresponding mounting hole 15 of installation axle 23, folder arm 2 through installation axle 23, mounting hole 15 with fuselage 1 is connected, be equipped with the side opening 16 that is used for installing work worm 7 on the side shield 13, the both ends of work worm 7 with side opening 16 is connected.
The folding machine arm 2 is provided with a shoulder plate 6, the bottom of the shoulder plate 6 is connected with the folding machine arm 2 through a hinge, and the upper end of the shoulder plate 6 is connected with a side baffle 13 of the machine body 1 through a hinge. The folding machine arm 2 is connected with the functional machine arm 3 through a three-way sleeve 31. The upper end of the folding foot stand 4 is connected with the functional horn 3 through a hinge, a foot stand fixing rod 41 is arranged on the inner side of the lower end of the folding foot stand 4, and the upper end of the foot stand fixing rod 41 is connected with the functional horn 3.
The utility model discloses the working process:
in the working process of the aircraft with the foldable and deformable frame, the working worm 7 rotates to drive the working worm wheel 22 to rotate, and the working worm wheel 22 drives the worm wheel sleeve 21 and the folding arm 2 on the worm wheel sleeve 21 to rotate, so that the folding arm 2 is folded and unfolded; when the foldable foot rest 4 is used, the foot rest fixing rod 41 is elongated and adjusted to be vertical, and when the foldable foot rest 4 is stored, the length of the foot rest fixing rod 41 is adjusted, so that the foldable foot rest 4 and the foldable foot rest are folded together.
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. An aircraft with a collapsible airframe, comprising: comprises a machine body (1), a folding machine arm (2) and a working worm (7), wherein the machine body (1) comprises a front baffle plate, a rear baffle plate (11), a top plate (12) and a side baffle plate (13), a working worm (7) is arranged between the side baffles (13), a folding machine arm (2) is arranged between the front baffle and the rear baffle (11), a worm gear sleeve (21) is arranged at the upper end of the folding machine arm (2), a working worm gear (22) is arranged at the front side of the worm gear sleeve (21), the working worm wheel (22) is meshed with the working worm (7), one end of the folding machine arm (2) far away from the machine body (1) is provided with a functional machine arm (3), folding foot stands (4) are arranged below the front end and the rear end of the functional machine arm (3), the top of folding foot rest (4) is equipped with screw installation axle (42), the top of fuselage (1) is equipped with cloud platform (5).
2. An aircraft with a collapsible, transformable frame, as claimed in claim 1, wherein: both ends are equipped with installation axle (23) around worm wheel sleeve (21), be equipped with on baffle (11) around fuselage (1) with installation axle (23) corresponding mounting hole (15), folding horn (2) through installation axle (23), mounting hole (15) with fuselage (1) is connected, be equipped with side opening (16) that are used for installing work worm (7) on side shield (13), the both ends of work worm (7) with side opening (16) are connected.
3. An aircraft with a collapsible, transformable frame, as claimed in claim 1, wherein: be equipped with shoulder board (6) on folding horn (2), the bottom of shoulder board (6) with folding horn (2) pass through hinged joint, the upper end of shoulder board (6) with pass through hinged joint between side shield (13) of fuselage (1).
4. An aircraft with a collapsible, transformable frame, as claimed in claim 1, wherein: the folding machine arm (2) is connected with the functional machine arm (3) through a three-way sleeve (31).
5. An aircraft with a collapsible, transformable frame, as claimed in claim 1, wherein: the upper end of the folding foot stand (4) is connected with the functional machine arm (3) through a hinge, a foot stand fixing rod (41) is arranged on the inner side of the lower end of the folding foot stand (4), and the upper end of the foot stand fixing rod (41) is connected with the functional machine arm (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021138898.6U CN212580135U (en) | 2020-06-18 | 2020-06-18 | Aircraft with foldable and deformable frame |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021138898.6U CN212580135U (en) | 2020-06-18 | 2020-06-18 | Aircraft with foldable and deformable frame |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212580135U true CN212580135U (en) | 2021-02-23 |
Family
ID=74651138
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021138898.6U Expired - Fee Related CN212580135U (en) | 2020-06-18 | 2020-06-18 | Aircraft with foldable and deformable frame |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212580135U (en) |
-
2020
- 2020-06-18 CN CN202021138898.6U patent/CN212580135U/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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210223 |