CN209870742U - Plant protection unmanned aerial vehicle adjusting device - Google Patents

Plant protection unmanned aerial vehicle adjusting device Download PDF

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Publication number
CN209870742U
CN209870742U CN201822112590.3U CN201822112590U CN209870742U CN 209870742 U CN209870742 U CN 209870742U CN 201822112590 U CN201822112590 U CN 201822112590U CN 209870742 U CN209870742 U CN 209870742U
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China
Prior art keywords
adjusting
plate
unmanned aerial
aerial vehicle
hole
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CN201822112590.3U
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Chinese (zh)
Inventor
孟娜
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Tianjin Lingzhi Haoyue Aviation Technology Co Ltd
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Tianjin Lingzhi Haoyue Aviation Technology Co Ltd
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Priority to CN201822112590.3U priority Critical patent/CN209870742U/en
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Abstract

The utility model belongs to the technical field of plant protection unmanned aerial vehicle, especially, relate to a plant protection unmanned aerial vehicle adjusting device, the first side connecting plate of unmanned aerial vehicle main part one side fixedly connected with, first upper fixed plate, first bottom plate of first side connecting plate side fixedly connected with, first upper fixed plate is equipped with first last fixed orifices, first bottom plate is equipped with first fixed orifices, the quantity of first last fixed orifices, first fixed orifices is 6, be equipped with first regulation wing between first upper fixed plate, the first bottom plate, first regulation wing is equipped with first last regulating plate, first last regulating plate is equipped with first upper adjustment hole, first regulating plate is equipped with first regulation hole, the quantity of first upper adjustment hole, first regulation hole is 6.

Description

Plant protection unmanned aerial vehicle adjusting device
Technical Field
The utility model belongs to the technical field of plant protection unmanned aerial vehicle, especially, relate to a plant protection unmanned aerial vehicle adjusting device.
Background
Plant protection unmanned aerial vehicle, also called unmanned vehicles, as the name implies is the unmanned aircraft who is used for agriculture and forestry plant protection operation, and this type unmanned aircraft comprises flight platform (fixed wing, helicopter, multiaxis aircraft), navigation flight control, spraying mechanism triplex, flies through ground remote control or navigation and controls, realizes spraying the operation, can spray medicament, seed, powder etc..
According to statistics, the reserved quantity of the plant protection unmanned aerial vehicle in China in 2014 is 695 frames and 426 ten thousand mu of total operation area, the reserved quantity of the plant protection unmanned aerial vehicle in China in 2015 is 2324 frames (31 provinces statistics), the total operation area is 1152.8 ten thousand mu, and the increase range is 234% and 170.6% respectively. Although the amplitude is obvious, the plant protection unmanned aerial vehicle system in China is not mature on the whole. At present, the technology of domestic plant protection unmanned aerial vehicles is different from the product performance, and at least of a plurality of products can meet the requirement of large-area high-strength plant protection spraying.
At present practical application's the flank of plant protection unmanned aerial vehicle both sides is fixed knot structure, and length can not adjust, and the suitability is not strong.
Disclosure of Invention
The utility model provides a plant protection unmanned aerial vehicle adjusting device to the flank that proposes in solving above-mentioned background art can not carry out the problem of adjusting.
The utility model provides a technical problem adopt following technical scheme to realize:
a plant protection unmanned aerial vehicle adjusting device comprises an unmanned aerial vehicle main body;
the unmanned aerial vehicle comprises an unmanned aerial vehicle body, and is characterized in that a first side connecting plate is fixedly connected to one side of the unmanned aerial vehicle body, a first upper fixing plate and a first lower fixing plate are fixedly connected to the side of the first side connecting plate, a first upper fixing hole is formed in the first upper fixing plate, a first lower fixing hole is formed in the first lower fixing plate, 6 first upper fixing holes and 6 first lower fixing holes are formed in the first upper fixing plate and the first lower fixing plate, a first adjusting wing is arranged between the first upper fixing plate and the first lower fixing plate, a first upper adjusting plate and a first lower adjusting plate are arranged on the first adjusting wing, a first upper adjusting hole is formed in the first upper adjusting plate, a first lower adjusting hole is formed in the first lower adjusting plate, 6 first upper adjusting holes and 6 first lower adjusting holes are formed in the first adjusting wing, a first fixing column is arranged on the upper surface of the first adjusting wing, a first motor is, the top end of the first rotating shaft is connected with a first propeller;
the other side of the unmanned aerial vehicle main body is fixedly connected with a second side connecting plate, the side surface of the second side connecting plate is fixedly connected with a second upper fixing plate and a second lower fixing plate, the second upper fixing plate is provided with a second upper fixing hole, the second lower fixing plate is provided with a second lower fixing hole, the number of the second upper fixing hole and the number of the second lower fixing hole are both 6, a second adjusting wing is arranged between the second upper fixing plate and the second lower fixing plate, the second adjusting wing is provided with a second upper adjusting plate and a second lower adjusting plate, the second upper adjusting plate is provided with a second upper adjusting hole, the second lower adjusting plate is provided with a second lower adjusting hole, the number of the second upper adjusting hole and the second lower adjusting hole are both 6, the upper surface of the second adjusting wing is provided with a second fixing column, a second motor is arranged in the second fixing column, and the top end of the second motor is connected with a second rotating shaft, the top end of the second rotating shaft is connected with a second propeller;
bottom surface fixedly connected with first foot rest, second foot rest under the unmanned aerial vehicle main part.
Still include first fastening bolt, second fastening bolt, first fastening bolt top is run through first last regulation hole, first last fixed orifices and is equipped with first fastening nut, first fastening bolt bottom is run through first regulation hole, first fixed orifices and is equipped with first fastening nut, second fastening bolt top is run through on the second regulation hole, the second fixed orifices and is equipped with second fastening nut, second fastening bolt bottom is run through under the second fixed orifices and the second and is equipped with second fastening nut.
Be equipped with the battery in the unmanned aerial vehicle main part, first motor, second motor all are connected with the battery electricity.
The utility model has the advantages that:
this technical scheme is through the setting of fixed plate, regulating plate, adjusts the length of regulating plate to be applicable to the operation of spraying in the region of different areas, during the adjustment, with the regulating plate remove between the fixed plate, confirm the length of regulating plate after, fix the regulating plate on the fixed plate through regulation hole and fixed orifices with fastening bolt, simple structure, convenient operation implements the effect very ideal.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
Detailed Description
A plant protection unmanned aerial vehicle adjusting device comprises an unmanned aerial vehicle main body 1;
a first side connecting plate 2 is fixedly connected to one side of an unmanned aerial vehicle main body 1, a first upper fixing plate 3 and a first lower fixing plate 4 are fixedly connected to the side surface of the first side connecting plate 2, a first upper fixing hole 5 is formed in the first upper fixing plate 3, a first lower fixing hole 6 is formed in the first lower fixing plate 4, the number of the first upper fixing hole 5 and the number of the first lower fixing hole 6 are 6, a first adjusting wing 7 is arranged between the first upper fixing plate 3 and the first lower fixing plate 4, the first adjusting wing 7 is provided with a first upper adjusting plate 8 and a first lower adjusting plate 9, the first upper adjusting plate 8 is provided with a first upper adjusting hole 10, the first lower adjusting plate 9 is provided with a first lower adjusting hole 11, the number of the first upper adjusting hole 10 and the first lower adjusting hole 11 is 6, a first fixing column 15 is arranged on the upper surface of the first adjusting wing 7, a first motor 16 is arranged in the first fixing column 15, and the top end, the top end of the first rotating shaft 17 is connected with a first propeller 18;
a second side connecting plate 19 is fixedly connected to the other side of the main body 1 of the unmanned aerial vehicle, a second upper fixing plate 20 and a second lower fixing plate 21 are fixedly connected to the side surface of the second side connecting plate 19, a second upper fixing hole 22 is formed in the second upper fixing plate 20, a second lower fixing hole 23 is formed in the second lower fixing plate 21, the number of the second upper fixing hole 22 and the number of the second lower fixing hole 23 are 6, a second adjusting wing 24 is arranged between the second upper fixing plate 20 and the second lower fixing plate 21, the second adjusting wing 24 is provided with a second upper adjusting plate 24 and a second lower adjusting plate 25, the second upper adjusting plate 24 is provided with a second upper adjusting hole 26, the second lower adjusting plate 25 is provided with a second lower adjusting hole 27, the number of the second upper adjusting hole 26 and the second lower adjusting hole 27 are 6, a second fixing column 31 is arranged on the upper surface of the second adjusting wing 24, a second motor 32 is arranged in the second fixing column 31, and the top end of the second motor 32 is connected with, the top end of the second rotating shaft 33 is connected with a second propeller 34;
the lower bottom surface of the unmanned aerial vehicle main body 1 is fixedly connected with a first foot rest 35 and a second foot rest 36.
The top of the first fastening bolt 12 penetrates through a first upper adjusting hole 10 and a first upper fixing hole 5 and is provided with a first upper fastening nut 13, the bottom of the first fastening bolt 12 penetrates through a first lower adjusting hole 11 and a first lower fixing hole 6 and is provided with a first lower fastening nut 14, the top of the second fastening bolt 28 penetrates through a second upper adjusting hole 26 and a second upper fixing hole 22 and is provided with a second upper fastening nut 29, and the bottom of the second fastening bolt 28 penetrates through a second lower adjusting hole 27 and a second lower fixing hole 23 and is provided with a second lower fastening nut 30.
Be equipped with battery 37 in the unmanned aerial vehicle main part 1, first motor 16, second motor 32 all are connected with battery 37 electricity.
The above detailed description of the embodiments of the present invention is only the preferred embodiments of the present invention, and the embodiments of the present invention should not be considered as limiting the scope of the present invention, and all the equivalent changes and improvements made in the application scope of the present invention should still belong to the scope of the present invention.

Claims (3)

1. The utility model provides a plant protection unmanned aerial vehicle adjusting device which characterized in that:
the unmanned aerial vehicle comprises an unmanned aerial vehicle main body;
the unmanned aerial vehicle comprises an unmanned aerial vehicle body, and is characterized in that a first side connecting plate is fixedly connected to one side of the unmanned aerial vehicle body, a first upper fixing plate and a first lower fixing plate are fixedly connected to the side of the first side connecting plate, a first upper fixing hole is formed in the first upper fixing plate, a first lower fixing hole is formed in the first lower fixing plate, 6 first upper fixing holes and 6 first lower fixing holes are formed in the first upper fixing plate and the first lower fixing plate, a first adjusting wing is arranged between the first upper fixing plate and the first lower fixing plate, a first upper adjusting plate and a first lower adjusting plate are arranged on the first adjusting wing, a first upper adjusting hole is formed in the first upper adjusting plate, a first lower adjusting hole is formed in the first lower adjusting plate, 6 first upper adjusting holes and 6 first lower adjusting holes are formed in the first adjusting wing, a first fixing column is arranged on the upper surface of the first adjusting wing, a first motor is, the top end of the first rotating shaft is connected with a first propeller;
the other side of the unmanned aerial vehicle main body is fixedly connected with a second side connecting plate, the side surface of the second side connecting plate is fixedly connected with a second upper fixing plate and a second lower fixing plate, the second upper fixing plate is provided with a second upper fixing hole, the second lower fixing plate is provided with a second lower fixing hole, the number of the second upper fixing hole and the number of the second lower fixing hole are both 6, a second adjusting wing is arranged between the second upper fixing plate and the second lower fixing plate, the second adjusting wing is provided with a second upper adjusting plate and a second lower adjusting plate, the second upper adjusting plate is provided with a second upper adjusting hole, the second lower adjusting plate is provided with a second lower adjusting hole, the number of the second upper adjusting hole and the second lower adjusting hole are both 6, the upper surface of the second adjusting wing is provided with a second fixing column, a second motor is arranged in the second fixing column, and the top end of the second motor is connected with a second rotating shaft, the top end of the second rotating shaft is connected with a second propeller;
bottom surface fixedly connected with first foot rest, second foot rest under the unmanned aerial vehicle main part.
2. The plant protection unmanned aerial vehicle adjusting device of claim 1, characterized in that: still include first fastening bolt, second fastening bolt, first fastening bolt top is run through first last regulation hole, first last fixed orifices and is equipped with first fastening nut, first fastening bolt bottom is run through first regulation hole, first fixed orifices and is equipped with first fastening nut, second fastening bolt top is run through on the second regulation hole, the second fixed orifices and is equipped with second fastening nut, second fastening bolt bottom is run through under the second fixed orifices and the second and is equipped with second fastening nut.
3. The plant protection unmanned aerial vehicle adjusting device of claim 2, characterized in that: be equipped with the battery in the unmanned aerial vehicle main part, first motor, second motor all are connected with the battery electricity.
CN201822112590.3U 2018-12-17 2018-12-17 Plant protection unmanned aerial vehicle adjusting device Active CN209870742U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201822112590.3U CN209870742U (en) 2018-12-17 2018-12-17 Plant protection unmanned aerial vehicle adjusting device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201822112590.3U CN209870742U (en) 2018-12-17 2018-12-17 Plant protection unmanned aerial vehicle adjusting device

Publications (1)

Publication Number Publication Date
CN209870742U true CN209870742U (en) 2019-12-31

Family

ID=68944922

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201822112590.3U Active CN209870742U (en) 2018-12-17 2018-12-17 Plant protection unmanned aerial vehicle adjusting device

Country Status (1)

Country Link
CN (1) CN209870742U (en)

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