CN214690163U - Unmanned vehicles with throw function - Google Patents
Unmanned vehicles with throw function Download PDFInfo
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- CN214690163U CN214690163U CN202023224481.4U CN202023224481U CN214690163U CN 214690163 U CN214690163 U CN 214690163U CN 202023224481 U CN202023224481 U CN 202023224481U CN 214690163 U CN214690163 U CN 214690163U
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Abstract
The utility model provides an unmanned vehicles with throw function, include: the device comprises a machine body, a flight driving mechanism, a foot seat, a throwing barrel, a throwing cover and an opening and closing control mechanism; the two flight driving mechanisms are respectively and fixedly arranged on two sides of the machine body and comprise a support frame, a propeller and a driving motor, the support frame is fixedly provided with the driving motor, and an output shaft of the driving motor is fixedly connected with the center of the propeller; foot seat fixed connection is in the bottom of fuselage, puts in bucket and foot seat fixed connection, and the dog-house has been seted up to one side of putting in the bucket, puts in the lid and articulates in the dog-house, switching control mechanism and put in lid control connection. The utility model has the advantages that: the throwing barrel is installed at the bottom end of the machine body, after the unmanned aerial vehicle flies to the designated position, the throwing cover is controlled to be opened, and articles in the throwing barrel drop, so that the throwing function is realized.
Description
Technical Field
The utility model relates to an unmanned vehicles, concretely relates to unmanned vehicles with throw function.
Background
Unmanned aerial vehicles or pilotless planes, unmanned aerial vehicles; is an unmanned aircraft operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an on-board computer. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; the method is currently 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, movie and television shooting, romantic manufacturing and the like. Most of the existing unmanned aerial vehicles are used for shooting and transporting.
SUMMERY OF THE UTILITY MODEL
The to-be-solved technical problem of the utility model lies in providing an unmanned vehicles with throw function, can throw at the flight in-process.
The utility model discloses a realize like this: an unmanned aerial vehicle with a throwing function, comprising: the device comprises a machine body, a flight driving mechanism, a foot seat, a throwing barrel, a throwing cover and an opening and closing control mechanism;
the two flight driving mechanisms are fixedly arranged on two sides of the airplane body respectively and comprise a support frame, a propeller and a driving motor, the driving motor is fixedly arranged on the support frame, and an output shaft of the driving motor is fixedly connected with the center of the propeller;
the foot stool fixed connection in the bottom of fuselage, put in the bucket with foot stool fixed connection, the dog-house has been seted up to one side of putting in the bucket, put in the lid articulate in the dog-house, switching control mechanism with put in lid control connection.
Further, the opening and closing control mechanism comprises a steering engine, a rocker, a lock arm, a coil spring, a flexible steel wire and a rubber band ring, a first claw is arranged on one side of the foot base, a lock part is arranged on the other side of the foot base, the head end of the lock arm is hinged to the lock part and provided with the coil spring, a second claw is arranged in the middle of the lock arm, the tail end of the lock arm is fixedly connected with one end of the flexible steel wire, the engine body of the steering engine is fixedly connected with the engine body, the output shaft of the steering engine is fixedly connected with one end of the rocker, the other end of the rocker is fixedly connected with the other end of the flexible steel wire, the first claw can hook one end of the rubber band ring, the rubber band ring bypasses and supports the feeding cover, and the second claw can hook the other end of the rubber band ring.
Furthermore, the foot stool further comprises lengthened supporting plates, and the lengthened supporting plates are fixedly arranged on two sides of the foot stool.
Furthermore, the device also comprises a camera which is fixedly arranged at the front end of the machine body.
Furthermore, each support frame is provided with two duct rings, and the driving motor is fixedly arranged in each duct ring.
Furthermore, the rear end of the machine body is provided with a lock hole.
The utility model has the advantages that: the bottom end of the machine body is provided with a throwing barrel, after the unmanned aerial vehicle flies to a designated position, a throwing cover is controlled to be opened, and non-aggressive weapons such as flash bombs and smoke bombs or aggressive weapons, rescue goods and materials and other articles in the throwing barrel fall off to realize a throwing function; the lengthened support plate is used for being placed on a plane and stably supporting the machine body; the camera of installation is convenient for the accurate control of remote control personnel and is thrown.
Drawings
The invention will be further described with reference to the following examples with reference to the accompanying drawings.
Fig. 1 is a schematic perspective view of the structure of the unmanned aerial vehicle with a throwing function according to the present invention.
Fig. 2 is a schematic perspective view of the structure of the unmanned aerial vehicle with a throwing function of the present invention.
Fig. 3 is a schematic view of the connection between the middle elastic ring and the first and second fingers.
Fig. 4 is a schematic view of the position of the rudder machine in the fuselage according to the present invention.
Fig. 5 is a schematic structural view of the middle foot stool of the present invention.
Fig. 6 is a schematic structural diagram of the locking arm of the present invention.
Fig. 7 is a schematic view of the bolt inserted into the middle lock hole of the present invention.
Reference numerals: a body 1; a lock hole 11; a foot seat 2; a first finger 21; a lock portion 22; lengthening the support plate 23; a throwing barrel 3; a throwing cover 4; a support frame 5; a bypass ring 51; a propeller 6; a drive motor 7; a steering engine 8; a rocker 9; a lock arm 10; a second finger 101; a flexible steel wire 20; a leather band 30; a camera 40; a latch 50.
Detailed Description
The embodiment of the utility model provides a through providing an unmanned vehicles with throw function, solved the technical problem that unmanned vehicles can't throw among the prior art, realized the technological effect of convenient throw.
The embodiment of the utility model provides an in technical scheme for solving above-mentioned problem, the general thinking is as follows: the bottom installation of fuselage is put in the bucket, flies to the assigned position after unmanned vehicles, and the lid is opened in the control, drops in smog bullet etc. in the bucket, realizes throwing the function.
For better understanding of the above technical solutions, the following detailed descriptions will be provided in conjunction with the drawings and the detailed description of the embodiments.
Referring to fig. 1 to 7, the preferred embodiment of the unmanned aerial vehicle with throwing function of the present invention.
The utility model discloses a: the device comprises a machine body 1, a flight driving mechanism, a foot base 2, a throwing barrel 3, a throwing cover 4 and an opening and closing control mechanism; the two flight driving mechanisms are fixedly arranged on two sides of the fuselage 1 respectively, each flight driving mechanism comprises a support frame 5, a propeller 6 and a driving motor 7, each support frame 5 is provided with two duct rings 51, the driving motor 7 is fixedly arranged in each duct ring 51, and an output shaft of each driving motor 7 is fixedly connected with the center of the propeller 6;
The opening and closing control mechanism comprises a steering engine 8, a rocker 9, a locking arm 10, a coil spring (not shown), a flexible steel wire 20 and a rubber band 30, one side of the foot seat 2 is provided with a first claw 21, the other side of the foot seat 2 is provided with a lock part 22, the head end of the locking arm 10 is hinged with the lock part 22 and is provided with the coil spring, the middle of the locking arm 10 is provided with a second claw 101, the tail end of the locking arm 10 is fixedly connected with one end of the flexible steel wire 20, the body of the steering engine 8 is fixedly connected with the body 1, an output shaft of the steering engine 8 is fixedly connected with one end of the rocker 9, the other end of the rocker 9 is fixedly connected with the other end of the flexible steel wire 20, the first claw 21 can hook one end of the leather band 30, the leather band 30 bypasses and props against the throwing cover 4, and the second claw 101 can hook the other end of the leather band 30. The two throwing covers 4 are provided, and the rubber band ring 30 is in a stretching state when being pressed against the throwing cover 4. The foot stool is characterized by further comprising lengthened supporting plates 23, wherein the lengthened supporting plates 23 are fixedly arranged on two sides of the foot stool 2.
The utility model discloses an unmanned vehicles's control system makes the telelever swing after receiving throwing signal control steering wheel 8, through taut flexible steel wire 20 and then pulling locking arm 10, the wind spring is for tightening up the state, and the one end of rubber band circle 30 just breaks away from second hook 101, and rubber band circle 30 contracts and no longer supports and puts in lid 4, puts in lid 4 and opens, realizes throwing the function. The steering engine 8 enables the rocker 9 to swing reversely, the flexible steel wire 20 is in a relaxed and soft state, and the coil spring resets to enable the locking arm 10 to rotate back to the initial position; facilitating the next installation of the leather ring 30.
Still include camera 40, camera 40 sets firmly in the front end of fuselage 1. The information that camera 40 will shoot passes to the remote control personnel through wireless mode, and the remote control personnel of being convenient for know the utility model discloses an environment that unmanned vehicles located to be convenient for accurate throwing.
The rear end of the machine body 1 is provided with a lock hole 11. When will the utility model discloses an unmanned vehicles arranges the transportation equipment in on, inserts lockhole 11 with bolt 50, just so can with the utility model discloses an unmanned vehicles pins, convenient transportation.
Although specific embodiments of the present invention have been described, it will be understood by those skilled in the art that the specific embodiments described are illustrative only and are not limiting upon the scope of the invention, and that equivalent modifications and variations can be made by those skilled in the art without departing from the spirit of the invention, which is to be limited only by the claims appended hereto.
Claims (6)
1. An unmanned vehicles with throw function, its characterized in that includes: the device comprises a machine body, a flight driving mechanism, a foot seat, a throwing barrel, a throwing cover and an opening and closing control mechanism;
the two flight driving mechanisms are fixedly arranged on two sides of the airplane body respectively and comprise a support frame, a propeller and a driving motor, the driving motor is fixedly arranged on the support frame, and an output shaft of the driving motor is fixedly connected with the center of the propeller;
the foot stool fixed connection in the bottom of fuselage, put in the bucket with foot stool fixed connection, the dog-house has been seted up to one side of putting in the bucket, put in the lid articulate in the dog-house, switching control mechanism with put in lid control connection.
2. The unmanned aerial vehicle with a throwing function according to claim 1, the opening and closing control mechanism comprises a steering engine, a rocker, a locking arm, a coil spring, a flexible steel wire and a rubber band ring, one side of the foot seat is provided with a first claw, the other side of the foot seat is provided with a lock part, the head end of the locking arm is hinged with the lock part and is provided with the coil spring, the middle of the locking arm is provided with a second claw, the tail end of the locking arm is fixedly connected with one end of the flexible steel wire, the body of the steering engine is fixedly connected with the body, the output shaft of the steering engine is fixedly connected with one end of the rocker, the other end of the rocker is fixedly connected with the other end of the flexible steel wire, the first claw can hook one end of the rubber band ring, the rubber band ring bypasses and props against the throwing cover, and the second claw can hook the other end of the rubber band ring.
3. The unmanned aerial vehicle with the throwing function of claim 1, further comprising an elongated support plate, wherein the elongated support plate is fixedly arranged on two sides of the foot seat.
4. The unmanned aerial vehicle with the throwing function of claim 1, further comprising a camera fixedly arranged at the front end of the fuselage.
5. The unmanned aerial vehicle with a pitching function of claim 1, wherein each support frame is provided with two ducted rings, and each ducted ring is fixedly provided with the driving motor.
6. The unmanned aerial vehicle with a throwing function of claim 1, wherein a keyhole is formed at a rear end of the body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023224481.4U CN214690163U (en) | 2020-12-28 | 2020-12-28 | Unmanned vehicles with throw function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202023224481.4U CN214690163U (en) | 2020-12-28 | 2020-12-28 | Unmanned vehicles with throw function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214690163U true CN214690163U (en) | 2021-11-12 |
Family
ID=78560254
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202023224481.4U Active CN214690163U (en) | 2020-12-28 | 2020-12-28 | Unmanned vehicles with throw function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214690163U (en) |
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2020
- 2020-12-28 CN CN202023224481.4U patent/CN214690163U/en active Active
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