CN211719075U - Teaching VTOL fixed wing unmanned aerial vehicle rapid disassembly structure - Google Patents

Abstract

The utility model belongs to the technical field of the unmanned aerial vehicle teaching is used, specifically disclose a teaching VTOL fixed wing unmanned aerial vehicle rapid disassembly structure, by the fixed subassembly of model main part, and the fixed subassembly of model wing that cooperatees and use with the fixed subassembly of model main part constitutes. The utility model discloses a teaching VTOL fixed wing unmanned aerial vehicle rapid disassembly structure's beneficial effect lies in: the model body fixing assembly and the model wing fixing assembly which are matched for use are connected with the model body and the model wing respectively, when training operation is carried out, quick separation, disassembly and accurate assembly (initial assembly state recovery) are completed, the intuitiveness of teaching display is improved, and the training effect is improved.

Description

Teaching VTOL fixed wing unmanned aerial vehicle rapid disassembly structure

Technical Field

The utility model belongs to the technical field of the unmanned aerial vehicle teaching is used, concretely relates to teaching VTOL fixed wing unmanned aerial vehicle rapid disassembly structure.

Background

An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.

Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicle divide into reconnaissance aircraft and target drone, and in civilian aspect, unmanned aerial vehicle + trade are used, are the real just needs of unmanned aerial vehicle. At present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.

Along with the rapid development of unmanned aerial vehicles in China, the related requirements are correspondingly and rapidly increased, many operators who use unmanned aerial vehicles for production and equipment are very short of talents, and meanwhile, the corresponding training requirements are very huge. In the aspect of unmanned aerial vehicle training, teaching, because unmanned aerial vehicle also has certain manufacturing cost, so train in class its adopt be the model machine come supplementary completion, traditional unmanned aerial vehicle training model machine is because of its inconvenient dismantlement and equipment, teaching effect is poor when leading to the training, when needs are dismantled promptly, with model machine fuselage and model machine wing separation, unable quick realization, can not audio-visual show teaching.

Therefore, based on the above problem, the utility model provides a teaching VTOL fixed wing unmanned aerial vehicle rapid disassembly structure.

SUMMERY OF THE UTILITY MODEL

Utility model purpose: the utility model aims at providing a teaching VTOL fixed wing unmanned aerial vehicle rapid disassembly structure, its reasonable in design, the fixed subassembly of model main part, the fixed subassembly of model wing that cooperate to use are connected with the model main part respectively, the model wing is connected, when training the operation, accomplish quick separation, dismantlement and accurate equipment (resume initial equipment state), improve the nature directly perceived of teaching show, improve the training effect.

The technical scheme is as follows: the utility model provides a rapid disassembly structure of a fixed-wing unmanned aerial vehicle for teaching vertical take-off and landing, which consists of a model main body fixing component and a model wing fixing component matched with the model main body fixing component for use; the model main body fixing assembly comprises a first strip-shaped positioning plate, a model main body connecting plate arranged on the outer wall of one side of the first strip-shaped positioning plate, vertical positioning clamping columns symmetrically arranged on the end faces of two ends of one side of the model main body connecting plate, a transverse positioning rod arranged on the outer wall of the other side of the first strip-shaped positioning plate, a wire through groove arranged in the first strip-shaped positioning plate and positioned on one side of the transverse positioning rod, and limiting clamping plates symmetrically arranged on two ends of the outer wall of the other side of the first strip-shaped positioning plate; the model wing fixing assembly comprises a second strip-shaped positioning plate, transverse positioning rod through holes, auxiliary lead through grooves, positioning plates, limiting clamping plate through grooves and limiting clamping plate positioning through holes, wherein the transverse positioning rod through holes are formed in the second strip-shaped positioning plate and are matched with the transverse positioning rods for use, the auxiliary lead through grooves are formed in the second strip-shaped positioning plate and are matched with the lead through grooves for use, the through grooves are symmetrically formed in the end faces of the two ends of the second strip-shaped positioning plate and are matched with the limiting clamping plates for use, the positioning plates are symmetrically arranged on the outer wall of one side of the second strip-shaped positioning plate and are matched with the limiting clamping; the diameter size of the transverse positioning rod is smaller than that of the through hole of the transverse positioning rod.

This technical scheme, teaching VTOL fixed wing unmanned aerial vehicle rapid disassembly structure still sets up the first auxiliary positioning groove at first bar locating plate both ends terminal surface including the symmetry, and sets up the spacing otic placode of perpendicular in first auxiliary positioning groove respectively, and sets up the spacing otic placode through-hole of perpendicular in the spacing otic placode of perpendicular respectively.

This technical scheme, teaching VTOL fixed wing unmanned aerial vehicle rapid disassembly structure still sets up at first bar locating plate, second bar locating plate both ends opposite face outer wall and a set of second assistance-localization real-time recess, a set of assistance-localization real-time lug that cooperatees and use including the symmetry, and wherein, a set of second assistance-localization real-time recess, a set of assistance-localization real-time lug are circular structure respectively, and the diameter size of second assistance-localization real-time recess is greater than the diameter size of assistance-localization real-time lug.

Compared with the prior art, the utility model discloses a teaching VTOL fixed wing unmanned aerial vehicle rapid disassembly structure's beneficial effect lies in: the model body fixing assembly and the model wing fixing assembly which are matched for use are connected with the model body and the model wing respectively, when training operation is carried out, quick separation, disassembly and accurate assembly (initial assembly state recovery) are completed, the intuitiveness of teaching display is improved, and the training effect is improved.

Drawings

Fig. 1 is a schematic structural view of a top view portion of a rapid disassembly structure of a fixed-wing unmanned aerial vehicle for teaching vertical take-off and landing of the present invention;

fig. 2 is a schematic diagram of a right-view structure of a model main body fixing assembly of the rapid dismounting structure of the vertical take-off and landing fixed wing unmanned aerial vehicle for teaching of the present invention;

fig. 3 is a left side view structural diagram of a model wing fixing component of the rapid disassembly structure of the vertical take-off and landing fixed wing unmanned aerial vehicle of the utility model;

FIG. 4 is the utility model discloses a teaching VTOL fixed wing unmanned aerial vehicle rapid disassembly structure's first bar locating plate, the main structure sketch map of looking at of spacing cardboard.

Detailed Description

The invention will be further elucidated with reference to the drawings and the specific embodiments.

As shown in fig. 1, fig. 2, fig. 3 and fig. 4, the fast dismounting structure for teaching vertical take-off and landing fixed-wing unmanned aerial vehicle is composed of a model main body fixing component and a model wing fixing component used in cooperation with the model main body fixing component; the model main body fixing assembly comprises a first strip-shaped positioning plate 1, a model main body connecting plate 7 arranged on the outer wall of one side of the first strip-shaped positioning plate 1, vertical positioning clamping columns 8 symmetrically arranged on the end faces of two ends of one side of the model main body connecting plate 7, a transverse positioning rod 5 arranged on the outer wall of the other side of the first strip-shaped positioning plate 1, a wire through groove 6 arranged in the first strip-shaped positioning plate 1 and positioned on one side of the transverse positioning rod 5, and limiting clamping plates 9 symmetrically arranged on two ends of the outer wall of the other side of the first strip-shaped positioning plate 1; the model wing fixing assembly comprises a second strip-shaped positioning plate 11, transverse positioning rod through holes 12 which are arranged in the second strip-shaped positioning plate 11 and are matched with transverse positioning rods 5 for use, auxiliary wire through grooves 14 which are arranged in the second strip-shaped positioning plate 11 and are matched with wire through grooves 6 for use, through grooves 15 which are symmetrically arranged in the end faces of the two ends of the second strip-shaped positioning plate 11 and are matched with limiting clamping plates 9 for use, positioning plates 17 which are symmetrically arranged on the outer wall of one side of the second strip-shaped positioning plate 11 and are matched with limiting clamping plates 9 for use, limiting clamping plate through grooves 18 which are respectively arranged in the positioning plates 17 and are matched with the limiting clamping plates 9 for use, and limiting clamping plate positioning through holes 19; the diameter size of the transverse positioning rod 5 is smaller than that of the through hole 12 of the transverse positioning rod.

Wherein, logical groove 15 is passed through to the one end of spacing cardboard 9 during the equipment, spacing cardboard leads to groove 18 and is located locating plate 17 bottom surface below, and the tip of spacing cardboard 9 passes through 19 protrusion locating plate 17 of spacing cardboard positioning hole, realize the positioning action who blocks, the effect that spacing cardboard leads to groove 17 is when dismantling, at first the finger inserts in the spacing cardboard leads to groove 17 and with the contact in the middle part of spacing cardboard 9, apply pressure this moment one end and spacing cardboard positioning hole 19 of spacing cardboard 9 again, locating plate 17 separates, transversely take out to one side at last and can accomplish the dismantlement action from first bar locating plate 1, otherwise then the equipment.

Further preferably, the rapid dismounting structure for the teaching vertical take-off and landing fixed-wing unmanned aerial vehicle further comprises first auxiliary positioning grooves 2 symmetrically arranged on end surfaces of two ends of the first strip-shaped positioning plate 1, vertical limiting lug plates 3 respectively arranged in the first auxiliary positioning grooves 2, and vertical limiting lug plate through holes 4 respectively arranged in the vertical limiting lug plates 3; and teaching VTOL fixed wing unmanned aerial vehicle rapid disassembly structure still sets up at first bar locating plate 1, 11 both ends opposite face outer walls of second bar locating plate and a set of second assistance-localization real-time recess 10, a set of assistance-localization real-time lug 16 that cooperate and use including the symmetry, and wherein, a set of second assistance-localization real-time recess 10, a set of assistance-localization real-time lug 16 are circular structure respectively, and the diameter size of second assistance-localization real-time recess 10 is greater than the diameter size of assistance-localization real-time lug 16.

The teaching VTOL fixed wing unmanned aerial vehicle rapid disassembly structure of this structure, model main part fixed subassembly, model wing fixed subassembly make for integrated into one piece's plastic construction respectively (model main part, model wing in figure 1 are foamed plastic and make).

The foregoing is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, a plurality of modifications can be made without departing from the principle of the present invention, and these modifications should also be regarded as the protection scope of the present invention.

Claims (3)

1. The utility model provides a teaching VTOL fixed wing unmanned aerial vehicle rapid disassembly structure which characterized in that: the model wing fixing component is matched with the model main body fixing component; the model main body fixing assembly comprises a first strip-shaped positioning plate (1), a model main body connecting plate (7) arranged on the outer wall of one side of the first strip-shaped positioning plate (1), vertical positioning clamp columns (8) symmetrically arranged on the end faces of two ends of one side of the model main body connecting plate (7), a transverse positioning rod (5) arranged on the outer wall of the other side of the first strip-shaped positioning plate (1), a lead through groove (6) arranged in the first strip-shaped positioning plate (1) and positioned on one side of the transverse positioning rod (5), and limiting clamp plates (9) symmetrically arranged on two ends of the outer wall of the other side of the first strip-shaped positioning plate (1); the model wing fixing assembly comprises a second strip-shaped positioning plate (11), transverse positioning rod through holes (12) which are arranged in the second strip-shaped positioning plate (11) and matched with transverse positioning rods (5) for use, auxiliary lead through grooves (14) which are arranged in the second strip-shaped positioning plate (11) and matched with lead through grooves (6) for use, through grooves (15) which are symmetrically arranged in end faces at two ends of the second strip-shaped positioning plate (11) and matched with limiting clamping plates (9) for use, positioning plates (17) which are symmetrically arranged on the outer wall at one side of the second strip-shaped positioning plate (11) and matched with limiting clamping plates (9) for use, limiting clamping plate through grooves (18) and limiting clamping plate positioning through holes (19) which are respectively arranged in the positioning plates (17) and matched with the limiting clamping plates (9) for use; the diameter size of the transverse positioning rod (5) is smaller than that of the through hole (12) of the transverse positioning rod.

2. The rapid disassembly structure of the teaching VTOL fixed wing UAV of claim 1, characterized in that: teaching VTOL fixed wing unmanned aerial vehicle rapid disassembly structure still sets up first auxiliary positioning recess (2) at first bar locating plate (1) both ends terminal surface including the symmetry, and sets up perpendicular spacing otic placode (3) in first auxiliary positioning recess (2) respectively, and sets up perpendicular spacing otic placode through-hole (4) in perpendicular spacing otic placode (3) respectively.

3. The rapid disassembly structure of the teaching VTOL fixed wing UAV of claim 1 or 2, characterized in that: teaching VTOL fixed wing unmanned aerial vehicle rapid disassembly structure still sets up at first bar locating plate (1), second bar locating plate (11) both ends opposite face outer wall and a set of second auxiliary positioning recess (10), a set of auxiliary positioning lug (16) that cooperate and use including the symmetry, and wherein, a set of second auxiliary positioning recess (10), a set of auxiliary positioning lug (16) are circular structure respectively, and the diameter size of second auxiliary positioning recess (10) is greater than the diameter size of auxiliary positioning lug (16).

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