CN213200086U - Undercarriage repacking external member based on M600 Pro unmanned aerial vehicle - Google Patents
Undercarriage repacking external member based on M600 Pro unmanned aerial vehicle Download PDFInfo
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- CN213200086U CN213200086U CN202021881181.0U CN202021881181U CN213200086U CN 213200086 U CN213200086 U CN 213200086U CN 202021881181 U CN202021881181 U CN 202021881181U CN 213200086 U CN213200086 U CN 213200086U
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- horn
- undercarriage
- flight control
- control cabin
- pole
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Abstract
The utility model discloses an undercarriage repacking external member based on M600 Pro unmanned aerial vehicle, including flight control cabin, signal antenna, horn, roll adjustment slide, screw, undercarriage, balance controller, carry pole, connecting plate, three signal antenna are installed to angles such as flight control cabin top, four angle such as horn is installed around the flight control cabin, the roll adjustment slide is seted up at the horn top, the screw is installed at the horn front end, undercarriage sliding connection is in horn center department, balance controller installs in flight control cabin bottom, carry the pole and install in balance controller bottom center department, connecting plate fixed connection is in carry pole bottom, the utility model discloses fully considered real operation safety and operating efficiency, established flight speed restriction and landing operation restriction. Simultaneously, the efficiency of the operation dismouting of this neotype design fully considered can realize quick assembly disassembly at the operation scene.
Description
Technical Field
The utility model relates to an undercarriage repacking external member based on M600 Pro unmanned aerial vehicle.
Background
According to different engineering demands, carry different load devices during unmanned aerial vehicle operation, like camera, atmospheric monitoring sensor etc.. These equipment forms are often less, do not influence unmanned aerial vehicle's rising and falling. However, some devices are too large and exceed the design of the unmanned aerial vehicle, for example, the height of the devices exceeds the height of the landing gear, so that the devices cannot be mounted.
With the increasing practice of unmanned aerial vehicle application scenarios, it is not haphazard to encounter such problems, and there is no shelf product solution that can be chosen conveniently. The main reason is that the demand is different and the demand is limited.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an undercarriage repacking external member based on M600 Pro unmanned aerial vehicle to solve above-mentioned technical problem.
In order to realize the purpose, the utility model adopts the following technical scheme:
the utility model provides an undercarriage repacking external member based on M600 Pro unmanned aerial vehicle, includes flight control cabin, signal antenna, horn, roll adjustment slide, screw, undercarriage, balance controller, carry pole, connecting plate, three signal antenna, four are installed to angle such as flight control cabin top the horn is installed all around in the flight control cabin, the roll adjustment slide is seted up at the horn top, the screw is installed at the horn front end, undercarriage sliding connection is in horn center department, balance controller installs in flight control cabin bottom, carry the pole and install in balance controller bottom center department, connecting plate fixed connection is in carry pole bottom.
On the basis of the technical scheme, the undercarriage includes flexible sill bar, cushion collar, pole setting fixed orifices, pole setting, horn go-between, the slip perforation, flexible sill bar front end and rear end fixedly connected with cushion collar respectively, two the pole setting fixed orifices equidistance is seted up at flexible sill bar top, pole setting bolted connection is inside the pole setting fixed orifices, horn go-between fixed connection is at the pole setting top, the slip perforation is seted up in the inside center department of horn go-between.
On the basis of the technical scheme, the length of the double vertical rods is about 70cm, the height of the double vertical rods is increased by about 35cm, and through tests, the telescopic bottom rods are designed to be 100cm so as to meet the requirement of landing stability.
Compared with the prior art, the utility model has the advantages of it is following: the utility model discloses an extension of M600 Pro unmanned aerial vehicle mounting capacity makes the space of mounting equipment promote from about 30X 35cm to 45X 60 cm. The utility model discloses fully considered real operation safety and operating efficiency, established the operating limitation of airspeed limit and landing. Simultaneously, the efficiency of the operation dismouting of this neotype design fully considered can realize quick assembly disassembly at the operation scene.
Drawings
Fig. 1 is a schematic view of the appearance structure of the present invention.
Fig. 2 is the structural schematic diagram of the landing gear of the present invention.
Fig. 3 is a schematic diagram comparing the improved effect of the present invention.
In the figure: 1. the airplane comprises a flight control cabin, 2 signal antennas, 3 booms, 4 distance-adjusting slideways, 5 propellers, 6 landing gears, 7 balance controllers, 8 mounting rods, 9 connecting plates, 10 telescopic bottom rods, 11 buffer sleeves, 12 vertical rod fixing holes, 13 vertical rods, 14 boom connecting rings and 15 sliding through holes.
Detailed Description
The invention is explained in further detail below with reference to the figures and the embodiments.
As shown in fig. 1-3, an undercarriage modification kit based on an M600 Pro unmanned aerial vehicle comprises a flight control cabin 1, signal antennas 2, a horn 3, a distance-adjusting slideway 4, a propeller 5, an undercarriage 6, a balance controller 7, a mounting rod 8 and a connecting plate 9, wherein three signal antennas 2 and four are installed at the top of the flight control cabin 1 at equal angles, the horn 3 is installed around the flight control cabin 1 at equal angles, the distance-adjusting slideway 4 is arranged at the top of the horn 3, the propeller 5 is installed at the front end of the horn 3, the undercarriage 6 is slidably connected at the center of the horn 3, the balance controller 7 is installed at the bottom of the flight control cabin 1, the mounting rod 8 is installed at the center of the bottom of the balance controller 7, and the connecting plate 9 is fixedly connected to the bottom of the mounting rod 8.
Undercarriage 6 is including flexible sill bar 10, cushion collar 11, pole setting fixed orifices 12, pole setting 13, horn go-between 14, the perforation 15 that slides, flexible sill bar 10 front end and rear end fixedly connected with cushion collar 11 respectively, two the 10 tops at flexible sill bar are seted up to pole setting fixed orifices 12 equidistance, pole setting 13 bolted connection is inside pole setting fixed orifices 12, 14 fixed connections of horn go-between are at the 13 tops of pole setting, the perforation 15 that slides is seted up in 14 inside centers of horn go-between department.
The length of the double vertical rods is about 70cm, the height of the double vertical rods is increased by about 35cm, and through tests, the telescopic bottom rods are designed to be 100cm so as to meet the requirement of landing stability.
The utility model discloses a theory of operation: this is novel according to carry equipment size in actual operation, through the distance between two undercarriage of roll adjustment slide and the horn go-between adjustment of horn on the horn, provides the loading space for equipment in the at utmost in the scope of bearing. Simultaneously, the efficiency of the operation dismouting of this neotype design fully considered can realize quick assembly disassembly at the operation scene.
The foregoing is a preferred embodiment of the present invention, and for those skilled in the art to understand the teaching of the present invention, the changes, modifications, replacements and variations to the embodiments will still fall within the protection scope of the present invention without departing from the principle and spirit of the present invention.
Claims (3)
1. The utility model provides an undercarriage repacking external member based on M600 Pro unmanned aerial vehicle, includes flight control cabin (1), signal antenna (2), horn (3), roll adjustment slide (4), screw (5), undercarriage (6), balance controller (7), carry pole (8), connecting plate (9), its characterized in that: three signal antenna (2) are installed to angles such as flight control cabin (1) top, four angles such as horn (3) are installed around flight control cabin (1), roll adjustment slide (4) are seted up at horn (3) top, screw (5) are installed at horn (3) front end, undercarriage (6) sliding connection is located at horn (3) center, install in flight control cabin (1) bottom balance controller (7), install in balance controller (7) bottom center department carry pole (8), connecting plate (9) fixed connection is in carry pole (8) bottom.
2. The landing gear retrofit kit based on an M600 Pro drone of claim 1, wherein: undercarriage (6) are including flexible sill bar (10), cushion collar (11), pole setting fixed orifices (12), pole setting (13), horn go-between (14), slip perforation (15), fixedly connected with cushion collar (11) respectively, two in flexible sill bar (10) front end and rear end pole setting fixed orifices (12) equidistance is seted up at flexible sill bar (10) top, pole setting (13) bolted connection is inside pole setting fixed orifices (12), horn go-between (14) fixed connection is at pole setting (13) top, slip perforation (15) are seted up at horn go-between (14) inside center department.
3. The landing gear retrofit kit based on an M600 Pro drone of claim 1, wherein: the length of the double vertical rods is about 70cm, the height of the double vertical rods is increased by about 35cm, and through tests, the telescopic bottom rods are designed to be 100cm so as to meet the requirement of landing stability.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021881181.0U CN213200086U (en) | 2020-09-02 | 2020-09-02 | Undercarriage repacking external member based on M600 Pro unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021881181.0U CN213200086U (en) | 2020-09-02 | 2020-09-02 | Undercarriage repacking external member based on M600 Pro unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213200086U true CN213200086U (en) | 2021-05-14 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021881181.0U Active CN213200086U (en) | 2020-09-02 | 2020-09-02 | Undercarriage repacking external member based on M600 Pro unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213200086U (en) |
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2020
- 2020-09-02 CN CN202021881181.0U patent/CN213200086U/en active Active
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