CN205952333U - A hemisphere buckler for having more rotor unmanned aerial vehicle - Google Patents

Abstract

The utility model discloses a hemisphere buckler for having more rotor unmanned aerial vehicle, the buckler includes hemisphere waterproof case, base, adjusting device and linking bridge, the inside holding cavity that is equipped with of hemisphere waterproof case, hemisphere waterproof case with base sealing connection, linking bridge connects the outside of base install in the linking bridge adjusting device, the utility model discloses a hemisphere buckler that the design comprises the multicomponent carries an ordinary camera with the machine and places in the device's hemisphere buckler, and the device can fix at many rotor unmanned aerial vehicle cloud bench through mechanical means, device possesses that mechanical structure is simple, the dead weight gently, among the firm in connection, high wind even characteristics of atress. Under the prerequisite that does not influence unmanned aerial vehicle stabilized flight, the device can effectively protect the camera of installing at unmanned aerial vehicle cloud bench to avoid the rainwater invasion and attack.

Description

Hemispherical bucker for many rotor wing unmanned aerial vehicles

Technical field

This utility model is related to a kind of hemispherical bucker for many rotor wing unmanned aerial vehicles.

Background technology

Due to using unmanned plane（UAV）With low cost, in recent years unmanned plane using all presenting explosive growth Situation.The potential user of unmanned plane presents multifarious feature, and the concrete application field of unmanned plane includes field exploration, map Drafting, media report, delivery, military surveillance, protection, field searching and rescue etc..

Common flight device is typically divided into fixed-wing, helicopter and many rotors.Many rotors are rapid because of excellent handling Become the nova taken photo by plane with model plane Sports Field.At present, many rotors have become as the main flow of Small and micro-satellite or model plane.Unmanned Multi-rotor aerocraft：The flying platform being made up of multigroup dynamical system, typically common are four rotors, six rotors, eight rotors very To more rotor compositions.Many rotors frame for movement is very simple, and dynamical system only needs to motor and is directly connected to propeller just.Excellent Point is that machinery is simple, can VTOL.For many rotors product at present, typically point semi-autonomous control mode and full Autonomous Control side Formula.At handling aspect, the manipulation of many rotors is simplest.Do not need the runway just can be with VTOL, can be in sky after taking off Middle hovering.Its manipulating principle is simple, and four remote sensing of control device operate around corresponding to aircraft, upper and lower and driftage side To motion.In terms of automatic pilot, the autocontrol method of many rotor wing unmanned aerial vehicles is simple, and controller parameter is adjusted also relatively Easily；But many rotors also has the development bottleneck of itself, such as：The up-down vibration of propeller can lead to the big propeller of rigidity very Easily snap off.In order that many rotor wing unmanned aerial vehicles complete preferably to fly, avoidance technology undoubtedly can be more stable for its offer Navigation performance.New technology can serve as " the eye of unmanned plane from vision and radar angular completely using common photographic head Eyeball " simultaneously develops cognitive disorders software, so that many rotor wing unmanned aerial vehicles can possess the ability of cognitive disorders, and then realizes self Navigation.Visual Tracking aspect, present increasing income flies the demand that control application can make aircraft follow user, and user is protected Hold at photographic head center.OpenCV open source software similarly has a lot of positioning and track algorithm to supply aircraft to develop.But current nothing Still in initial stage, for the designer and developer of unmanned plane, wanting to throw in market has competition for man-machine application The product of power simultaneously allows their work well, still in the face of many challenges.

Motor in unmanned aerial vehicle body and the waterproof of the electronic equipments such as sensor, can be added using correlation technique in engineering To solve.The waterproof of camera is sufficiently complex, and the manufacturer of current unmanned aerial vehicle onboard waterproof camera is less, and almost needs completely Want the price of import, waterproof camera high.Generally domestic unmanned plane manufacturer is to hang to the method for monopod video camera waterproof Carry and install square waterproof cover additional, on the commonly used waterproof unmanned plane at home of the type waterproof cover, the subject matter that exists Be shape be irregularly easily caused unmanned plane unbalance stress in the case of high wind, thus causing the unstable of unmanned plane during flying.

Content of the invention

For above-mentioned problem, this utility model aims to provide a kind of hemispherical waterproof for many rotor wing unmanned aerial vehicles Cover, the video camera that hemispherical bucker of the present utility model can be arranged on unmanned machine head with effective protection avoids rainwater and invades Attack, due to the profile of dome-type make unmanned plane in high wind still can with uniform force so that the flight of many rotor wing unmanned aerial vehicles relatively It is stable.

To achieve these goals, the technical scheme that this utility model is adopted is as follows：

For the hemispherical bucker of many rotor wing unmanned aerial vehicles, described bucker includes hemispherical waterproof case, base, regulation Device and connecting bracket, are provided with accommodating cavity inside described hemispherical waterproof case, described hemispherical waterproof case with described Base is tightly connected, and described connecting bracket is connected to the outside of described base, installs described regulation and fill in described connecting bracket Put.

Preferably, described hemispherical waterproof case is made up of hyaline test and plastic ring two parts, described plastic ring and institute State thread seal between base to connect.

Preferably, described base center is provided with installing hole, in described installation in the hole setting hex nut.

Preferably, described connecting bracket is made up of the end of thread, the notch end of lateral opening and bar portion.

Preferably, the described end of thread is fastenedly connected with described hex nut, described adjusting means is horizontally installed on described In the notch end of connecting bracket.

Preferably, described adjusting means is made up of threaded shank and portion of spherical adjustment portion, described threaded shank is located at described company Connect at support notch end side surface opening, and the adjustable side of described adjusting means is screwed.

The beneficial effects of the utility model are：Compared with prior art, the utility model has the advantages that, this utility model prevent The Airborne camera that water cover can be arranged on unmanned machine head with effective protection avoids rainwater invasion and attack, and the profile due to dome-type makes Obtaining unmanned plane still can be with uniform force so that the flight of many rotor wing unmanned aerial vehicles be relatively stable in high wind；And this bucker knot Structure is simple and assembling is easily accomplished, lightweight, adjusts resistance little.

Brief description

Fig. 1 is this utility model structural representation.

Fig. 2 is this utility model hemispherical waterproof case schematic diagram.

Fig. 3 is this utility model base schematic diagram.

Fig. 4 is this utility model connecting bracket schematic diagram.

Fig. 5 is this utility model adjusting means schematic diagram.

Fig. 6 is this utility model hex nut schematic diagram.

Fig. 7 is this utility model assembling schematic diagram.

Wherein：1- hemispherical waterproof case, 2- base, 3- adjusting means, 4- connecting bracket, 5- houses cavity, 6- hexagonal Nut, 7- screw, 8- minitype airborne video camera.

Specific embodiment

In order that those of ordinary skill in the art is better understood on the technical solution of the utility model, with reference to attached Figure and embodiment are further described to the technical solution of the utility model.

A kind of hemispherical bucker for many rotor wing unmanned aerial vehicles shown in 1-7 referring to the drawings, described bucker includes half Spherical waterproof case 1, base 2, adjusting means 3 and connecting bracket 4, described hemispherical waterproof case 1 is by hyaline test and plastics Circle two parts composition, between described plastic ring and described base 2, thread seal is connected, and adopts plastics with base 2 junction, is beneficial to Screw thread is confined with base 2 and is connected, and is provided with accommodating cavity 5, minitype airborne video camera 8 is installed inside described hemispherical waterproof case 1 In accommodating cavity 5, described hemispherical waterproof case 1 is tightly connected with described base 2, and described connecting bracket 4 is connected to described The outside of base 2, installs described adjusting means 3 in described connecting bracket 4.

In this utility model, described base 2 center is provided with installing hole, in described installation in the hole setting hex nut 6, described connecting bracket 4 is made up of the end of thread, the notch end of lateral opening and bar portion, the described end of thread and described hex nut 6 are fastenedly connected, and described adjusting means 3 is horizontally installed in the notch end of described connecting bracket 4,.

In this utility model, described adjusting means 3 is made up of threaded shank and portion of spherical adjustment portion, and described threaded shank is located at At described connecting bracket 4 notch end side surface opening, and the adjustable side of described adjusting means 3 is passed through screw 7 and is fixed.

Using the cooperation of hex nut 6, connecting bracket 4, base 2 all using plastic construction, so can farthest subtract The weight of light bucker, uses adjusting means 3 with unmanned plane junction, and the screw 7 with a fixation is fixing, the program Advantage is that outfit of equipment weight is very light, and structure is simple and assembling is easily accomplished, and the engagement using screw thread can preferably be prevented Water.

Claims (6)

1. be used for many rotor wing unmanned aerial vehicles hemispherical bucker it is characterised in that：Described bucker include hemispherical waterproof case, Base, adjusting means and connecting bracket, are provided with accommodating cavity, outside described hemispherical waterproof inside described hemispherical waterproof case Shell is tightly connected with described base, and described connecting bracket is connected to the outside of described base, installs institute in described connecting bracket State adjusting means.

2. the hemispherical bucker for many rotor wing unmanned aerial vehicles according to claim 1 it is characterised in that：Described hemispherical Waterproof case is made up of hyaline test and plastic ring two parts, and between described plastic ring and described base, thread seal is connected.

3. the hemispherical bucker for many rotor wing unmanned aerial vehicles according to claim 1 it is characterised in that：In described base Heart position is provided with installing hole, in described installation in the hole setting hex nut.

4. the hemispherical bucker for many rotor wing unmanned aerial vehicles according to claim 3 it is characterised in that：Described connection Frame is made up of the end of thread, the notch end of lateral opening and bar portion.

5. the hemispherical bucker for many rotor wing unmanned aerial vehicles according to claim 4 it is characterised in that：The described end of thread It is fastenedly connected with described hex nut, described adjusting means is horizontally installed in the notch end of described connecting bracket.

6. the hemispherical bucker for many rotor wing unmanned aerial vehicles according to claim 5 it is characterised in that：Described regulation fills Put and be made up of threaded shank and portion of spherical adjustment portion, described threaded shank is located at described connecting bracket notch end side surface opening, and The adjustable side of described adjusting means is screwed.