CN216734786U - Unmanned aerial vehicle engine stores pylon - Google Patents
Unmanned aerial vehicle engine stores pylon Download PDFInfo
- Publication number
- CN216734786U CN216734786U CN202220046240.5U CN202220046240U CN216734786U CN 216734786 U CN216734786 U CN 216734786U CN 202220046240 U CN202220046240 U CN 202220046240U CN 216734786 U CN216734786 U CN 216734786U
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- rack
- aerial vehicle
- unmanned aerial
- connecting frame
- bolster
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Abstract
The utility model discloses an engine hanging rack of an unmanned aerial vehicle, which is used for fixedly installing an engine on a rack of the unmanned aerial vehicle and comprises an installation plate; a connecting frame; the mounting plate is connected to the lower end of the connecting frame, and the upper end of the connecting frame is fixedly connected with the rack; the link is provided with a plurality ofly, the link with frame fixed connection's one end is provided with the installation department, the orientation of installation department the frame place side is opened and is equipped with the draw-in groove, the frame part accept in the draw-in groove, a plurality of bolts pass behind the frame screw in on the installation department. A buffer member; the bolster be located the link with the link of mounting panel, to the mounting panel cushions.
Description
Technical Field
The utility model belongs to the technical field, and particularly relates to an unmanned aerial vehicle engine hanger.
Background
For an unmanned aerial vehicle, a motor and an engine are often adopted as power parts of the unmanned aerial vehicle, and for the motor, the unmanned aerial vehicle runs stably, has small vibration and has small starting and stopping impact; however, in the case of the engine, during the operation process, since the crankshaft, the piston and other components often have large vibration, and the impact of starting and stopping the engine is large, the vibration will have an adverse effect on the operation of the unmanned aerial vehicle; and because the engine has great dead weight, the support that still needs the installation engine has sufficient intensity then, satisfies actual engine installation user demand.
Disclosure of Invention
The utility model aims to provide an engine pylon of an unmanned aerial vehicle, which aims to solve the technical problem in the background technology.
In order to solve the technical problem, the utility model aims to realize that:
an engine hanging rack of an unmanned aerial vehicle is used for fixedly installing an engine on a frame of the unmanned aerial vehicle and comprises an installation plate;
a connecting frame; the mounting plate is connected to the lower end of the connecting frame, and the upper end of the connecting frame is fixedly connected with the rack; the link is provided with a plurality ofly, the link with frame fixed connection's one end is provided with the installation department, the orientation of installation department the frame place side is opened and is equipped with the draw-in groove, the frame part accept in the draw-in groove, a plurality of bolts pass behind the frame screw in on the installation department.
A buffer member; the bolster be located the link with the link of mounting panel, to the mounting panel cushions.
On the basis of the above scheme and as a preferable scheme of the scheme: the bolster includes first bolster and second bolster, first bolster is located the lower extreme of link with between the upper end of mounting panel, the second bolster is located the lower extreme of mounting panel, a dead lever is passed by the through-hole from last in proper order from down the second bolster the mounting panel and screw behind the first bolster in the link.
On the basis of the above scheme and as a preferable scheme of the scheme: the connecting frames are provided with four connecting frames which are respectively positioned at four corners of the mounting plate.
On the basis of the above scheme and as a preferable scheme of the scheme: each connecting frame comprises wing plates which are symmetrically arranged.
On the basis of the above scheme and as a preferable scheme of the scheme: the cross section of the rack is rectangular, the clamping groove is matched with the rack so that the rack is accommodated in the clamping groove, and the bottom surface and two side surfaces of the clamping groove are both contacted with the rack.
Compared with the prior art, the utility model has the outstanding and beneficial technical effects that: in the application, the installation part of the connecting frame adopts a clamping groove structure, and is positioned and installed with the rack in an embedding mode, so that the installation is quicker, the evidence is not required to be found, and the operation is convenient and quick; and the first shock absorption pad and the second shock absorption pad are added to further absorb the energy of the vibration.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic perspective view of the present invention;
fig. 3 is another angle structure diagram of the present invention.
Detailed Description
In order to make the purpose, technical solutions and advantages of the present application clearer, the technical solutions in the embodiments will be clearly and completely described below with reference to the drawings in the embodiments, and it is obvious that the described embodiments are only a part of the embodiments of the present application, and not all the embodiments. All other embodiments obtained by a person skilled in the art without making any inventive step, based on the given embodiments, fall within the scope of protection of the present application.
In the description of the present application, it is to be understood that the terms "upper", "lower", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are only for convenience in describing the present application and simplifying the description, and do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present application.
In the description of the present application, the terms "first", "second", and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implying any number of technical features indicated.
An unmanned aerial vehicle engine hanger is used for fixedly mounting an engine on a frame 10 of an unmanned aerial vehicle and comprises a mounting plate 20; the mounting plate 20 is formed by processing a whole metal, and is provided with an engine mounting hole 21 and necessary hollowed-out weight reduction; preferably, the material is stainless steel.
A connecting frame 30; the mounting plate 20 is connected to the lower end of the connecting frame 30, and the upper end of the connecting frame 30 is fixedly connected with the rack 10; the link 30 is provided with a plurality ofly, the link 30 with frame 10 fixed connection's one end is provided with installation department 32, the orientation of installation department 32 frame 10 place side is opened and is equipped with draw-in groove 321, frame 10 part accept in the draw-in groove 321, a plurality of bolts pass behind the frame 10 screw in on the installation department 32. In this embodiment, the cross section of the rack 10 is preferably rectangular, the slot 321 is matched with the rack 10, so that the rack 10 is received in the slot 321, and the bottom surface and the two side surfaces 322 of the slot 321 are both in contact with the rack 10. The installation part of the connecting frame 30 adopts a clamping groove structure, and is positioned and installed with the rack 10 in an embedded mode, so that the installation is quicker, the evidence is not required to be found, and the operation is convenient and quick; and in the process of engine operation after installation, when the front and back swing appears, the stability and the intensity of whole link can also be improved through the cooperation of the side of draw-in groove 321 and frame.
A buffer member 40; the buffer member is located at a connection end between the connection frame 30 and the mounting plate 20, and buffers the mounting plate 20. Specifically, the buffer member 40 includes a first buffer member 41 and a second buffer member 42, the first buffer member 41 is located between the lower end of the connecting frame 30 and the upper end of the mounting plate 20, the second buffer member 42 is located at the lower end of the mounting plate 20, and a fixing rod is sequentially passed through a through hole 43 from the top to the bottom of the second buffer member 42, the mounting plate 20 and the first buffer member 41 and then screwed to the connecting frame 30. In the present embodiment, the first buffer member 41 and the second buffer member 42 are preferably made of rubber, and are made into a cylindrical shape with a circular hole in the middle, so that the fixing rod can pass through the cylindrical shape conveniently to be fixed with the connecting frame 30; and preferably, the inner diameter of the hole on the mounting plate 20 for the fixed rod to pass through is larger than that of the fixed rod; from this, have added first shock pad and the energy of second shock pad further absorption vibration in through this embodiment, improve whole unmanned aerial vehicle's stability.
It is further preferred that the connecting frame 30 is provided with four, respectively located at four corners of the mounting plate 20. In order to enhance the strength of the connecting frames 30 in the present embodiment, each of the connecting frames 30 preferably includes symmetrically arranged wings 31, and the strength and stability of the connecting frame 30 are enhanced by the arrangement of the wings 31.
The above embodiments are only preferred embodiments of the present invention, and the protection scope of the present invention is not limited thereby, so: equivalent changes made according to the structure, shape and principle of the utility model shall be covered by the protection scope of the utility model.
Claims (5)
1. The utility model provides an unmanned aerial vehicle engine stores pylon for with engine fixed mounting in unmanned aerial vehicle's frame (10), its characterized in that: comprises a mounting plate (20);
a connecting frame (30); the mounting plate (20) is connected to the lower end of the connecting frame (30), and the upper end of the connecting frame (30) is fixedly connected with the rack (10); the connecting frame (30) is provided with a plurality of connecting frames, one end of each connecting frame (30) fixedly connected with the rack (10) is provided with an installation part (32), the side, facing the rack (10), of each installation part (32) is provided with a clamping groove (321), part of the rack (10) is accommodated in the clamping groove (321), and a plurality of bolts penetrate through the rack (10) and are screwed on the installation parts (32) and buffer parts (40); the buffer piece is positioned at the connecting end of the connecting frame (30) and the mounting plate (20) and buffers the mounting plate (20).
2. The unmanned aerial vehicle engine pylon of claim 1, wherein: bolster (40) include first bolster (41) and second bolster (42), first bolster (41) are located the lower extreme of link (30) with between the upper end of mounting panel (20), second bolster (42) are located the lower extreme of mounting panel (20), a dead lever is passed by through-hole (43) from last in proper order under by second bolster (42) mounting panel (20) and screw behind first bolster (41) in link (30).
3. The unmanned aerial vehicle engine pylon of claim 1, wherein: the connecting frames (30) are four and are respectively positioned at four corners of the mounting plate (20).
4. The unmanned aerial vehicle engine pylon of claim 3, wherein: each connecting frame (30) comprises symmetrically arranged wing plates (31).
5. The unmanned aerial vehicle engine pylon of claim 1, wherein: the cross section of the rack (10) is rectangular, the clamping groove (321) is matched with the rack (10) so that the rack (10) is received in the clamping groove (321), and the bottom surface and two side surfaces (322) of the clamping groove (321) are in contact with the rack (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220046240.5U CN216734786U (en) | 2022-01-05 | 2022-01-05 | Unmanned aerial vehicle engine stores pylon |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220046240.5U CN216734786U (en) | 2022-01-05 | 2022-01-05 | Unmanned aerial vehicle engine stores pylon |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216734786U true CN216734786U (en) | 2022-06-14 |
Family
ID=81912483
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220046240.5U Active CN216734786U (en) | 2022-01-05 | 2022-01-05 | Unmanned aerial vehicle engine stores pylon |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216734786U (en) |
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2022
- 2022-01-05 CN CN202220046240.5U patent/CN216734786U/en active Active
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