CN218400986U - Small wind resistance airborne hanging cabin for helicopter - Google Patents
Small wind resistance airborne hanging cabin for helicopter Download PDFInfo
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- CN218400986U CN218400986U CN202222449383.3U CN202222449383U CN218400986U CN 218400986 U CN218400986 U CN 218400986U CN 202222449383 U CN202222449383 U CN 202222449383U CN 218400986 U CN218400986 U CN 218400986U
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Abstract
The utility model discloses a helicopter carries hanging storehouse with little windage resistance machine, including helicopter hanging storehouse subassembly for connect the helicopter, hoist and mount goods, helicopter hanging storehouse subassembly is in with the setting including the airborne hanging storehouse frame that sets up the mounting disc of airborne hanging storehouse frame intermediate position, direction subassembly are including fixing the first installation flat board of airborne hanging storehouse frame lateral wall, setting are in the second installation flat board of first installation flat board below, install driving motor, the connection on first installation flat board surface are in the pivot and the connection of driving motor output are in the deflector on pivot surface looks over the subassembly. The utility model discloses a helicopter hanging storehouse structure, the guide structure that set up and looking over mutually supporting of structure reach and utilize wind-force to carry out supplementary direction when carrying out the hanging storehouse and adjust, reduce the load of motor to the motor distributes the direction alone, improves the flexibility of adjustment, and the wind-force in the make full use of helicopter flight avoids the energy extravagant.
Description
Technical Field
The utility model relates to a helicopter machine carries hanging storehouse technical field specifically is a helicopter is with little windage resistance machine carries hanging storehouse.
Background
According to the small wind resistance airborne hangar for the unmanned aerial vehicle disclosed in the publication No. CN 208559779U, in the recorded technical scheme, the streamlined shell of the shuttle structure is arranged outside the hangar, the wind resistance is reduced compared with a disordered direct hanging and loading structure, so that the energy consumption is reduced, and the function of changing along with the wind direction like a sail is realized by arranging the steering device, the possibility that the wind resistance is larger due to windward side surfaces is avoided.
SUMMERY OF THE UTILITY MODEL
Therefore, the utility model aims at providing a helicopter is with little wind resistance machine carries hanging storehouse, through helicopter hanging storehouse structure, guide structure who sets up and looking over mutually supporting of structure, reaches to utilize wind-force to assist the direction when carrying out the hanging storehouse regulation, reduces the load of motor to the motor distributes the direction alone, improves the flexibility of adjustment, and the wind-force in the make full use of helicopter flight avoids the energy extravagant.
In order to solve the technical problem, according to the utility model discloses an aspect, the utility model provides a following technical scheme:
a small wind resistance airborne hangar for a helicopter, comprising:
the helicopter hanging cabin assembly is used for connecting a helicopter and hanging cargos, and comprises an airborne hanging cabin frame and a mounting plate arranged in the middle of the airborne hanging cabin frame;
the guide assembly comprises a first mounting flat plate fixed on the side wall of the airborne hanging cabin frame, a second mounting flat plate arranged below the first mounting flat plate, a driving motor arranged on the surface of the first mounting flat plate, a rotating shaft connected to the output end of the driving motor and a guide plate connected to the surface of the rotating shaft;
and the viewing assembly is used for remotely monitoring and viewing the orientation of the airborne pod frame.
As a helicopter is with a preferred scheme of little wind resistance machine-carried hanging cabin, wherein, helicopter hanging cabin subassembly is still including setting up the arc port at machine-carried hanging cabin frame both ends and the connection machine-carried hanging cabin frame with support frame between the mounting disc.
As a helicopter is with preferred scheme of little windage resistance machine carries hanging cabin, wherein, look over the subassembly including fixing the installation pole of mounting disc top surface, connect and be in the connecting rod of installation pole top surface, connect and be in the surveillance camera head of connecting rod bottom surface, setting are in the controller and the signal transmission ware on surveillance camera head surface.
As a helicopter is with preferred scheme of little wind resistance machine-carried hanging cabin, wherein, still include direction adjustment subassembly, direction adjustment subassembly is including setting up arc deflector, the fixing of machine-carried hanging cabin frame one side arc deflector inboard swash plate, fixing of arc deflector the gag lever post of swash plate bottom surface, fix the thread head of gag lever post bottom surface with set up the round hole on first installation flat surface.
As a helicopter carry preferred scheme of hanging storehouse with little windage resistance machine, wherein, the gag lever post with the round hole registrates each other to the thread end is connected with a thread section of thick bamboo.
As a helicopter carries an optimal scheme of hanging oneself from a storehouse with little windage resistance machine, wherein, direction adjustment subassembly is provided with two, and two direction adjustment subassemblies in the central line position symmetry setting of machine year hanging oneself from a storehouse frame.
Compared with the prior art, the utility model discloses the beneficial effect who has is: through the helicopter hanging cabin structure that sets up, the mutual cooperation of guide structure and viewing structure, reach and utilize wind-force to carry out supplementary direction when carrying out the hanging cabin regulation, reduce the load of motor, and the direction is distributed alone to the motor, improve the flexibility of adjustment, make full use of helicopter is wind-force in the flight, avoid the energy waste, when specifically using, machine carries the hanging cabin frame at the in-process that helicopter hoist and mount aversion, streamlined arc port leads, reduce the windage, when the side of machine carries the hanging cabin frame leads, the user drives the pivot through driving motor this moment and rotates, the pivot drives deflector adjustment angle, the deflector carries out wind-force direction, wind directly blows the deflector, thereby promote whole machine carries the hanging cabin frame and changes the position, until arc port is the same with the direction of motion, carry out wind-force direction, reduce the resistance, the operator passes through the picture that the surveillance camera was shot, and through the cooperation of signal transmission ware and controller, can real time monitoring adjustment machine carries the orientation of hanging cabin frame like this.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the present invention will be described in detail with reference to the accompanying drawings and detailed embodiments, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without inventive labor. Wherein:
FIG. 1 is a block diagram of the present invention;
FIG. 2 is a block diagram of the viewing assembly of the present invention;
fig. 3 is a structural diagram of the guiding adjustment assembly of the present invention.
In the figure: 100. a helicopter pod assembly; 110. an airborne hangar frame; 120. an arcuate port; 130. a support frame; 140. mounting a disc; 200. a guide assembly; 210. a first mounting plate; 220. a second mounting plate; 230. a drive motor; 240. a rotating shaft; 250. a guide plate; 300. a view component; 310. mounting a rod; 320. a connecting rod; 330. a surveillance camera; 340. a controller; 350. a signal transmitter; 400. a guide adjustment assembly; 410. an arc-shaped guide plate; 420. a sloping plate; 430. a limiting rod; 440. a screw head; 450. a circular hole.
Detailed Description
In order to make the above objects, features and advantages of the present invention more comprehensible, embodiments of the present invention are described in detail below with reference to the accompanying drawings.
In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention, but the present invention may be implemented in other ways than those specifically described herein, and one skilled in the art may similarly generalize the present invention without departing from the spirit of the present invention, and therefore the present invention is not limited to the specific embodiments disclosed below.
Next, the present invention will be described in detail with reference to the drawings, and in order to describe the embodiments of the present invention in detail, the sectional view showing the device structure will not be enlarged partially according to the general scale for convenience of description, and the drawings are only examples, which should not limit the scope of the present invention. In addition, the three-dimensional dimensions of length, width and depth should be included in the actual fabrication.
To make the objects, technical solutions and advantages of the present invention more apparent, embodiments of the present invention will be described in detail with reference to the accompanying drawings.
The utility model provides a helicopter is with little windage resistance machine carries hanging storehouse, mutually supports through helicopter hanging storehouse structure, the guide structure who sets up and look over the structure, reaches and utilizes wind-force to carry out supplementary direction when carrying out the hanging storehouse regulation, reduces the load of motor to the motor distributes the direction alone, improves the flexibility of adjustment, and the energy waste is avoided to the wind-force in the make full use of helicopter flight.
Fig. 1 to 3 are schematic diagrams showing an overall structure of an embodiment of a small wind resistance airborne pod for a helicopter of the present invention, and referring to fig. 1 to 3, a main body of the small wind resistance airborne pod for a helicopter of the present embodiment includes a helicopter pod assembly 100, a guide assembly 200, and a viewing assembly 300.
Helicopter hanging cabin subassembly 100 is used for connecting the helicopter, hoist and mount goods, and is specific, helicopter hanging cabin subassembly 100 is including the airborne hanging cabin frame 110 that sets up and the mounting disc 140 of setting at airborne hanging cabin frame 110 intermediate position, helicopter hanging cabin subassembly 100 still includes the arc port 120 that sets up at airborne hanging cabin frame 110 both ends and connects the support frame 130 between airborne hanging cabin frame 110 and mounting disc 140, when specifically using, store goods in airborne hanging cabin frame 110, and airborne hanging cabin frame 110 passes through mounting disc 140 and is connected with the helicopter, and rotate through the axis of rotation between mounting disc 140 and the helicopter and be connected.
The guide assembly 200 is used for guiding and adjusting wind power, and in particular, the guide assembly 200 comprises a first installation flat plate 210 fixed on the side wall of the airborne pod frame 110, a second installation flat plate 220 arranged below the first installation flat plate 210, a driving motor 230 installed on the surface of the first installation flat plate 210, a rotating shaft 240 connected to the output end of the driving motor 230 and a guide plate 250 connected to the surface of the rotating shaft 240, when the guide assembly is used specifically, in the process of hoisting and shifting the airborne pod frame 110 in a helicopter, the streamlined arc-shaped port 120 guides to reduce wind resistance, when the lateral side of the airborne pod frame 110 guides, a user drives the rotating shaft 240 to rotate through the driving motor 230, the rotating shaft 240 drives the guide plate 250 to adjust the angle, the guide plate 250 guides the wind power, and the wind directly blows the guide plate 250, so that the whole airborne pod frame 110 is pushed to change the direction until the arc-shaped port 120 is the same as the moving direction, the wind power is guided, and the resistance is reduced.
The viewing assembly 300 is used for remotely monitoring and viewing the orientation of the airborne pod frame 110, specifically, the viewing assembly 300 comprises a mounting rod 310 fixed on the top surface of the mounting plate 140, a connecting rod 320 connected to the top surface of the mounting rod 310, a monitoring camera 330 connected to the bottom surface of the connecting rod 320, a controller 340 arranged on the surface of the monitoring camera 330 and a signal transmitter 350, when the remote monitoring and controlling device is used specifically, an operator can monitor and adjust the orientation of the airborne pod frame 110 in real time through pictures shot by the monitoring camera 330 and through the cooperation of the signal transmitter 350 and the controller 340.
With reference to fig. 1 to 3, in a specific use of the small wind resistance airborne pod for a helicopter of the present embodiment, during a process of hoisting and displacing the airborne pod frame 110 of the helicopter, the streamlined arc-shaped port 120 guides to reduce wind resistance, when the side surface of the airborne pod frame 110 guides, a user drives the rotating shaft 240 to rotate through the driving motor 230, the rotating shaft 240 drives the guiding plate 250 to adjust an angle, the guiding plate 250 guides wind, and the wind directly blows the guiding plate 250, so as to push the entire airborne pod frame 110 to change the direction until the arc-shaped port 120 is the same as the moving direction, so as to guide wind and reduce resistance, and an operator can monitor and adjust the orientation of the airborne pod frame 110 in real time through a picture taken by the monitoring camera 330 and through the cooperation of the signal transmitter 350 and the controller 340.
Further, through the direction adjustment subassembly 400 that sets up, the erection joint of wind-force direction can be carried out, can adjust the adjustment direction of hanging storehouse like this, the high practicality, it is concrete, still include direction adjustment subassembly 400, direction adjustment subassembly 400 is including setting up the arc deflector 410 in airborne hanging storehouse frame 110 one side, fix the swash plate 420 at arc deflector 410 inboard, fix the gag lever post 430 in swash plate 420 bottom surface, fix the thread head 440 in gag lever post 430 bottom surface and set up the round hole 450 on first installation flat plate 210 surface, when specifically using, gag lever post 430 and round hole 450 overlap each other, and thread head 440 and thread cylinder are connected, can install arc deflector 410 like this, whole arc deflector 410 shelters from arc port 120 completely this moment, arc deflector 410 leads, can wholly change the spigot surface like this, conveniently be applicable to hanging storehouse transportation under the different environment and use.
While the invention has been described above with reference to an embodiment, various modifications may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In particular, as long as there is no structural conflict, the various features of the disclosed embodiments of the present invention can be used in any combination with each other, and the description of these combinations not exhaustive in this specification is merely for the sake of brevity and resource conservation. Therefore, it is intended that the invention not be limited to the particular embodiments disclosed, but that the invention will include all embodiments falling within the scope of the appended claims.
Claims (6)
1. The utility model provides a helicopter is with little wind resistance machine-mounted hanging cabin which characterized in that includes:
the helicopter hanging cabin assembly (100) is used for connecting a helicopter and hanging cargos, and the helicopter hanging cabin assembly (100) comprises an airborne hanging cabin frame (110) and a mounting plate (140) arranged in the middle of the airborne hanging cabin frame (110);
the guide assembly (200) comprises a first mounting flat plate (210) fixed on the side wall of the airborne pod frame (110), a second mounting flat plate (220) arranged below the first mounting flat plate (210), a driving motor (230) mounted on the surface of the first mounting flat plate (210), a rotating shaft (240) connected to the output end of the driving motor (230) and a guide plate (250) connected to the surface of the rotating shaft (240);
a viewing assembly (300) for remotely monitoring the orientation of viewing the airborne pod frame (110).
2. The helicopter pod assembly (100) of claim 1 further comprising an arcuate port (120) disposed at each end of the pod frame (110) and a support bracket (130) connected between the pod frame (110) and the mounting plate (140).
3. The small wind resistance airborne pod for helicopter of claim 2, wherein said viewing assembly (300) comprises a mounting rod (310) fixed on the top surface of said mounting plate (140), a connecting rod (320) connected on the top surface of said mounting rod (310), a monitoring camera (330) connected on the bottom surface of said connecting rod (320), a controller (340) and a signal transmitter (350) arranged on the surface of said monitoring camera (330).
4. The small wind resistance airborne pod for helicopter of claim 3, further comprising a guiding adjustment assembly (400), wherein said guiding adjustment assembly (400) comprises an arc-shaped guide plate (410) disposed on one side of said airborne pod frame (110), a sloping plate (420) fixed on the inner side of said arc-shaped guide plate (410), a limiting rod (430) fixed on the bottom surface of said sloping plate (420), a screw head (440) fixed on the bottom surface of said limiting rod (430) and a circular hole (450) disposed on the surface of said first mounting plate (210).
5. The small wind resistance airborne pod for helicopters according to claim 4, characterized in that said stop rod (430) and said circular hole (450) are mutually nested and the screw head (440) is connected with the screw barrel.
6. The helicopter with low wind resistance airborne pod of claim 5, characterized in that there are two guiding adjustment assemblies (400), and two guiding adjustment assemblies (400) are symmetrically disposed at the centerline position of the airborne pod frame (110).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222449383.3U CN218400986U (en) | 2022-09-15 | 2022-09-15 | Small wind resistance airborne hanging cabin for helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222449383.3U CN218400986U (en) | 2022-09-15 | 2022-09-15 | Small wind resistance airborne hanging cabin for helicopter |
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| Publication Number | Publication Date |
|---|---|
| CN218400986U true CN218400986U (en) | 2023-01-31 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202222449383.3U Active CN218400986U (en) | 2022-09-15 | 2022-09-15 | Small wind resistance airborne hanging cabin for helicopter |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116513451A (en) * | 2023-04-10 | 2023-08-01 | 烟台南山学院 | Folding unmanned aerial vehicle undercarriage |
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2022
- 2022-09-15 CN CN202222449383.3U patent/CN218400986U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116513451A (en) * | 2023-04-10 | 2023-08-01 | 烟台南山学院 | Folding unmanned aerial vehicle undercarriage |
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