CN208699039U - Unmanned plane is used in a kind of teaching - Google Patents

Unmanned plane is used in a kind of teaching Download PDF

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Publication number
CN208699039U
CN208699039U CN201821071854.9U CN201821071854U CN208699039U CN 208699039 U CN208699039 U CN 208699039U CN 201821071854 U CN201821071854 U CN 201821071854U CN 208699039 U CN208699039 U CN 208699039U
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China
Prior art keywords
wing
mount plate
spring leaf
fixed
positioning hole
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Expired - Fee Related
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CN201821071854.9U
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Chinese (zh)
Inventor
周松鹤
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Individual
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Individual
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Priority to CN201821071854.9U priority Critical patent/CN208699039U/en
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Publication of CN208699039U publication Critical patent/CN208699039U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of teaching unmanned planes, belong to vehicle technology field, which includes fuselage and wing components, and wing components include wing mount plate and wing-body;Wing mount plate side is fixed on fuselage, the other side offers the mounting groove for connecting with wing-body, mounting groove inner wall two sides are provided with first positioning hole, wing mount plate surface is provided with second location hole, portable pillar is equipped in first positioning hole, portable pillar is T-shape and major diameter one end is located in first positioning hole, and minor diameter one end passes through second location hole, is fixed with pressing pad in portable pillar;Wing-body is connecting one end with wing mount plate equipped with spring leaf, spring leaf includes upper and lower two spring blade units, it is in " V " type that two spring blade units open up and down, positioning column is fixed on spring leaf, positioning column is adapted with first positioning hole, the wing for solving existing unmanned plane model is fixed on fuselage two sides, and the big and not easy to store problem of occupied space is convenient for disassembly and assembly.

Description

Unmanned plane is used in a kind of teaching
Technical field
The utility model relates to vehicle technology field, in particular to unmanned plane is used in a kind of teaching.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself The not manned aircraft of presetting apparatus manipulation, or fully or intermittently automatically operated by car-mounted computer.With someone It drives an airplane and compares, unmanned plane is often more suitable for the task of those too " slow-witted, dirty or dangerous ".Unmanned plane presses application field, Can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, be divided into take photo by plane, agricultural, plant protection, Miniature self-timer, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, is rescued express transportation The fields such as calamity, movies-making, manufacture romance.
Unmanned plane generally includes fuselage and wing, and at present during unmanned plane theory teaching, teacher is usually required nothing Man-machine model is brought into classroom and imparts knowledge to students, and the wing of unmanned plane model in the prior art is all to be fixed on fuselage two sides, accounts for It is big with space, it is not easy to store, and during storage, wing is easy to be pressurized and cause to fracture.
Utility model content
The purpose of the utility model is to provide a kind of teaching unmanned planes, and it is solid which solve the wings of existing unmanned plane model It is scheduled on fuselage two sides, the big and not easy to store problem of occupied space.
The above-mentioned technical purpose of the utility model has the technical scheme that
A kind of teaching unmanned plane, the wing components including fuselage and set on the fuselage two sides, the wing components packet Include wing mount plate and wing-body;
The wing mount plate side is fixed on the fuselage, and the other side is offered for connecting with the wing-body Mounting groove, mounting groove inner wall two sides are provided with first positioning hole, and the wing mount plate surface is provided with second location hole, institute First positioning hole diameter is stated greater than the second location hole, and the first positioning hole is passed through by the second location hole with the external world It is logical, portable pillar is equipped in the first positioning hole, the portable pillar is T-shape and major diameter one end is located at the first positioning hole Interior and slide setting with it, described minor diameter one end passes through the second location hole and extends outwardly, fixed in the portable pillar There is pressing pad, the pressing pad is located at the wing mount plate outer surface and diameter is greater than the second location hole;
The wing-body is connecting one end with the wing mount plate equipped with spring leaf, and the spring leaf includes upper and lower two A spring blade unit, two spring blade unit one end are individually fixed in wing-body end, and the other end opens up and down respectively In " V " type, under natural conditions, maximum distance is greater than the installation groove width, the spring leaf between two spring blade units On be fixed with positioning column, the positioning column is adapted with the first positioning hole.
Using the above structure, when installation, spring leaf is pressed, so that two spring blade units are mutually drawn close in compressive state, When distance is less than installation groove width between upper and lower two positioning column top surfaces, spring leaf is plugged in mounting groove, due to first Location hole is adapted with the positioning column on spring leaf, therefore after spring leaf plugs mounting groove, positioning column will be in spring leaf It is bound in first positioning hole under reset response, so that wing-body is fixed on wing mount plate.When disassembly, pressing pressing Pad, so that portable pillar major diameter one end inwardly pushes positioning column, positioning column will be disengaged from first positioning hole at this time, and spring leaf is in compression Then state pulls out wing-body, so that wing-body be extracted out outward and separated with wing mount plate.It is convenient for disassembly and assembly, Convenient for being disassembled with wing slave, reducing occupied space, convenient for storage and carrying.
It advanced optimizes are as follows: the wing-body is fixed with mounting blocks connecting one end with the wing mount plate, described Mounting blocks are being provided with slot close to the wing mount plate side, and the installation trench bottom is fixed with for being plugged in the slot Interior cutting, the mounting blocks are plugged in the mounting groove.
Using the above structure, mounting blocks can plug in mounting groove, and cutting can plug in slot, enhancing wing-body with Bonding strength between wing mount plate improves overall stability.
It advanced optimizes are as follows: the pressing pad is made of rubber.
Using the above structure, it is pressed convenient for hand, improves pressing comfort level.
Advanced optimize are as follows: the spring leaf be equipped with it is multiple, multiple spring leafs be spaced set.
Using the above structure, enhance the bonding strength between wing-body and wing mount plate, improve overall stability.
It advanced optimizes are as follows: the mounting blocks are located between two spring leafs, and the mounting blocks are at least provided with one.
Using the above structure, enhance the bonding strength between wing-body and wing mount plate, improve overall stability.
In conclusion the utility model has the following beneficial effects: spring leaf is pressed, so that two spring leafs when installing Unit is mutually drawn close in compressive state, when distance is less than installation groove width between upper and lower two positioning column top surfaces, by spring leaf It is plugged in mounting groove with mounting blocks, and cutting is inserted into slot, due to the positioning in first positioning hole and spring leaf Column is adapted, therefore after spring leaf plugs mounting groove, and positioning column will be bound to the first positioning under the reset response of spring leaf In hole, so that wing-body is fixed on wing mount plate.When disassembly, pressing pad is pressed, so that portable pillar major diameter one end Positioning column is inwardly pushed, positioning column will be disengaged from first positioning hole at this time, and spring leaf is in compressive state, then pull out wing sheet Body, so that wing-body be extracted out outward and separated with wing mount plate.It is convenient for disassembly and assembly, convenient for it will be dismantled with wing slave under Come, reduce occupied space, convenient for storage and carries, and the bonding strength between wing-body and wing mount plate is preferable, it is whole Body stability is preferable.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of embodiment, is mainly used for embodying the structure of unmanned plane model;
Fig. 2 is confined explosion's schematic diagram of embodiment, is mainly used for embodying the structure of wing components;
Fig. 3 is the schematic cross-sectional view of embodiment, is mainly used for embodying the structure of wing mount plate;
Fig. 4 is the enlarged drawing of A structure in Fig. 3, is mainly used for embodying the structure of portable pillar;
Fig. 5 is the partial structural diagram of embodiment, is mainly used for embodying the structure of wing-body.
In figure, 1, fuselage;2, wing components;21, wing mount plate;22, wing-body;3, slot;4, mounting groove;5, it inserts Item;6, portable pillar;7, pressing pad;8, first positioning hole;9, spring leaf;10, positioning column;11, mounting blocks;12, second location hole.
Specific embodiment
The utility model is described in further detail below in conjunction with attached drawing.
Embodiment: a kind of teaching unmanned plane as shown in Fig. 1,2,3,4,5, including fuselage 1 and is set to fuselage 1 opposite two The wing components 2 of side, wing components 2 include wing mount plate 21 and wing-body 22.Machine is fixed in 21 side of wing mount plate 1 two sides of body, the other side offer the mounting groove 4 for connecting with wing-body 22, and mounting groove 4 is rectangular-shaped and upper and lower inner wall two Side offers first positioning hole 8, and there are three first positioning hole 8 is set, three first positioning holes 8 are respectively spaced set.Machine The two sides up and down of wing mounting plate 21 are provided with second location hole 12 in place corresponding with 8 position of first positioning hole respectively, and first 8 diameter of location hole is greater than second location hole 12, and first positioning hole 8 passes through second location hole 12 and extraneous perforation.First positioning Portable pillar 6 is equipped in hole 8, portable pillar 6 is T-shape and major diameter one end is located in first positioning hole 8 and slides setting with it, small Diameter end passes through second location hole 12 and extends outwardly.6 small-diameter end portions of portable pillar are fixed with pressing pad 7, and pressing pad 7 is circle It plate-like and is made of rubber, pressing pad 7 is located at 21 outer surface of wing mount plate and diameter is greater than second location hole 12.Wing sheet Body 22 is connecting one end with wing mount plate 21 equipped with spring leaf 9, and spring leaf 9 includes upper and lower two spring blade units.Two bullets Reed unit is integrated setting and one end is individually fixed in 22 end of wing-body, and it is in " V " type that the other end opens up and down respectively, from Under right state, the maximum distance between two spring blade units is greater than 4 width of mounting groove.Spring leaf 9 is close to wing mount plate 21 One end is fixed with positioning column 10, and positioning column 10 is adapted with first positioning hole 8, and positioning column 10 is equipped with upper and lower two, top positioning Column 10 is fixed on upper springs blade unit top surface, and lower part positioning column 10 is fixed on lower springs blade unit bottom surface, and spring leaf 9 plugs When in mounting groove 4, positioning column 10 is corresponding with 8 position of first positioning hole.
Referring to Fig.1,2,3,4,5, there are three spring leaf 9 is set, three spring leafs 9 are spaced set, adjacent springs piece 9 it Between be equipped with mounting blocks 11, mounting blocks 11 are fixed on 21 end of wing mount plate and are adapted with mounting groove 4.Mounting blocks 11 are close 21 side of wing mount plate is provided with slot 3, and 4 bottom of mounting groove is fixed with the cutting 5 for being plugged in slot 3, mounting blocks 11 It is plugged in mounting groove 4.
Disassembly process: when installation, spring leaf 9 is pressed, so that two spring blade units are mutually drawn close in compressive state, when upper When distance is less than 4 width of mounting groove between 10 top surface of lower two positioning columns, spring leaf 9 and mounting blocks 11 are plugged into mounting groove 4 It is interior, and cutting 5 is inserted into slot 3, since first positioning hole 8 is adapted with the positioning column 10 on spring leaf 9, work as After spring leaf 9 plugs mounting groove 4, positioning column 10 will be bound in first positioning hole 8 under the reset response of spring leaf 9, thus Wing-body 22 is fixed on wing mount plate 21.
When disassembly, pressing pad 7 is pressed, so that 6 major diameter one end of portable pillar inwardly pushes positioning column 10, positioning column 10 at this time Will be disengaged from first positioning hole 8, spring leaf 9 is in compressive state, then pull out wing-body 22, thus by wing-body 22 to Outer extraction is simultaneously separated with wing mount plate 21.
This specific embodiment is only the explanation to the utility model, is not limitations of the present invention, ability Field technique personnel can according to need the modification that not creative contribution is made to the present embodiment after reading this specification, but As long as all by the protection of Patent Law in the scope of the claims of the utility model.

Claims (5)

1. a kind of teaching unmanned plane, including fuselage (1) and set on the wing components (2) of the fuselage (1) two sides, feature Be: the wing components (2) include wing mount plate (21) and wing-body (22);
Wing mount plate (21) side is fixed on the fuselage (1), the other side offer for the wing-body (22) mounting groove (4) connected, mounting groove (4) the inner wall two sides are provided with first positioning hole (8), the wing mount plate (21) Surface is provided with second location hole (12), and first positioning hole (8) diameter is greater than the second location hole (12), and described first Location hole (8) is by the second location hole (12) and extraneous perforation, and the first positioning hole (8) is interior to be equipped with portable pillar (6), institute Portable pillar (6) are stated as T-shape and major diameter one end is located in the first positioning hole (8) and slides setting with it, it is described small straight Diameter one end passes through the second location hole (12) and extends outwardly, and is fixed with pressing pad (7) on the portable pillar (6), described to press Pressure pad (7) is located at the wing mount plate (21) outer surface and diameter is greater than the second location hole (12);
The wing-body (22) is connecting one end with the wing mount plate (21) equipped with spring leaf (9), the spring leaf (9) Including upper and lower two spring blade units, two spring blade unit one end are individually fixed in the wing-body (22) end, It is in " V " type that the other end opens up and down respectively, and under natural conditions, maximum distance is greater than the installation between two spring blade units Slot (4) width is fixed with positioning column (10) on the spring leaf (9), the positioning column (10) and the first positioning hole (8) phase Adaptation.
2. it is according to claim 1 it is a kind of teaching use unmanned plane, it is characterized in that: the wing-body (22) with the machine Wing mounting plate (21) connection one end is fixed with mounting blocks (11), and the mounting blocks (11) are close to the wing mount plate (21) one Side is provided with slot (3), and mounting groove (4) bottom is fixed with the cutting (5) for being plugged in the slot (3), the peace Dress block (11) is plugged in the mounting groove (4).
3. a kind of teaching unmanned plane according to claim 1, it is characterized in that: the pressing pad (7) is made of rubber.
4. it is according to claim 2 it is a kind of teaching use unmanned plane, it is characterized in that: the spring leaf (9) be equipped with it is multiple, it is multiple The spring leaf (9) is spaced set.
5. a kind of teaching unmanned plane according to claim 4, it is characterized in that: the mounting blocks (11) are located at described in two Between spring leaf (9), the mounting blocks (11) are at least provided with one.
CN201821071854.9U 2018-07-07 2018-07-07 Unmanned plane is used in a kind of teaching Expired - Fee Related CN208699039U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821071854.9U CN208699039U (en) 2018-07-07 2018-07-07 Unmanned plane is used in a kind of teaching

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821071854.9U CN208699039U (en) 2018-07-07 2018-07-07 Unmanned plane is used in a kind of teaching

Publications (1)

Publication Number Publication Date
CN208699039U true CN208699039U (en) 2019-04-05

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Application Number Title Priority Date Filing Date
CN201821071854.9U Expired - Fee Related CN208699039U (en) 2018-07-07 2018-07-07 Unmanned plane is used in a kind of teaching

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110329489A (en) * 2019-08-19 2019-10-15 中国科学院工程热物理研究所 Parallel unmanned vehicle based on flexible connection technology

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110329489A (en) * 2019-08-19 2019-10-15 中国科学院工程热物理研究所 Parallel unmanned vehicle based on flexible connection technology

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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: 20190405

Termination date: 20190707