CN205554566U - Innovative small -size unmanned vehicles - Google Patents
Innovative small -size unmanned vehicles Download PDFInfo
- Publication number
- CN205554566U CN205554566U CN201620266405.4U CN201620266405U CN205554566U CN 205554566 U CN205554566 U CN 205554566U CN 201620266405 U CN201620266405 U CN 201620266405U CN 205554566 U CN205554566 U CN 205554566U
- Authority
- CN
- China
- Prior art keywords
- steering gear
- motor
- air jet
- jet system
- switch
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Landscapes
- Toys (AREA)
Abstract
The utility model discloses an innovative small -size unmanned vehicles includes screw, organism and steering gear, the screw is installed in the top of drive shaft, and is provided with the spiral leaf on the screw, the below of drive shaft is provided with the motor, the below of motor is provided with the counter roll, the top of counter roll is provided with the support, the organism is installed on the support, the inside of organism is provided with the battery, the left side of battery is provided with the inductor, the below at the organism is installed in the steering gear. Compared with the prior art, the beneficial effects of the utility model are that: the utility model relates to an innovative small -size unmanned vehicles structure scientific and reasonable, the operation is safe convenient, is provided with the steering gear in the below of organism, and the below of steering gear is provided with the air jet system, and through the jet -propelled orientation of control air jet system and then the orientation of adjustment machine flight, and the air jet system can also quicken the flying speed of machine, makes aircraft speed faster, sensitiveer.
Description
Technical field
This utility model relates to vehicle technology field, a kind of innovative small-sized unmanned aircraft.
Background technology
The mankind have the ideal aloft flown as birds very early, and the mechanical Columba livia manufactured by the A Erxitasi of ancient Greek, boomerang, the hot balloon of China and kite as far as Australia have relation.At ancient Chinese, someone describes the ideal of flight in literature works, and somebody devises the flight of kites device that some are large-scale, attempt to realize this ideal departing from the earth constraint, ten thousand families of the Ming Dynasty, just devising one and tie up on chair by tens powder rockets, hand-held kite carries out the test flown.Aircraft the most the earliest is the kite of Chinese invention.The 15th century, the Lie Aonaduo Leonardo da Vinci of Italy the most once designed aircraft.The development of contemporary aircraft, has benefited from the huge leap forward of the Science and Technology that the industrial revolution of 19th century brings.In 19th century, constantly attempt to break through the constraint of air, but all have failed.Along with invention and the extensively application of internal combustion engine, aerial flight is increasingly becoming possibility.1903, the Lai Te brother of the U.S. took the lead at the US-built aircraft produced and can fly, and achieves the dream of flight.Subsequently, aircraft and relevant Science and Technology thereof, developed rapidly.A lot of scientific research institutions or even individual has been had to have deeper research about aerodynamic vehicle.But in the most individual remote dream of China, along with the step of era development also has some courageously to propose some methods, but we do not see as substantial progress, LMT of the U.S. releases a applicable manned single aerodynamic vehicle the most to a high-profile, four-axle aircraft is the one of which of minute vehicle, is also a kind of intelligent robot.Being initially to be made by oneself successfully by model airplane fan, manufacturer of a lot of automatization found that it may be used for multiple use and actively originates in development later.It utilizes has four rotors as flight engine to carry out airflight, and its size is less, lighter in weight, be suitable for that the unmanned vehicle that carries with use is the same can carry certain mission payload, possesses independent navigation flight performance.Specific aerial mission is completed in the environment of complexity, danger.Can be used for amusement equally, such as play the piano the virtual games such as song, augmented reality.Its construction features of four-axle aircraft are respectively equipped with a rotor on its four angles, motor drive respectively, and blade can rotate forward, it is also possible to reversion.In order to keep the stabilized flight of aircraft, equipped with gyroscope and the 3 axle acceleration sensors composition inertial navigation module in 3 directions on four-axle aircraft, it ensures its rapid flight also by electronic adjusting controller.Aircraft has nowadays had become as a kind of recreational facilities in people's daily life.
In use there are some defects in existing small-sized unmanned aircraft, such as, flight speed is the slowest, and in flight course, steering reaction is insensitive.
Utility model content
The purpose of this utility model is to provide a kind of innovative small-sized unmanned aircraft, with the flight speed that solves to propose in above-mentioned background technology compared with the slow and insensitive problem of steering reaction.
For achieving the above object, this utility model following technical scheme of offer: a kind of innovative small-sized unmanned aircraft, including propeller, body and steering gear, described propeller is arranged on the top of drive shaft, and on propeller, it is provided with helical-blade, the lower section of described drive shaft is provided with motor, the lower section of described motor is provided with fulcrum, described fulcrum be provided above support, described body is rack-mount, described body be internally provided with battery, the left side of described battery is provided with induction apparatus, described steering gear is arranged on the lower section of body, and the lower section of steering gear is provided with air jet system, described induction apparatus and controller wireless connections, it is provided with motor switch on described controller, air jet system switch and steering gear switch, and motor switch, air jet system switch and steering gear switch are all electrically connected with controller.
Preferably, described fulcrum is provided with four altogether.
Preferably, described motor is provided with four altogether, and four motors are separately mounted to the top of four fulcrums.
Preferably, described helical-blade is provided with eight altogether, and eight helical-blades are arranged on four propellers the most uniformly.
Preferably, connected by bearing between described propeller and drive shaft.
Compared with prior art, the beneficial effects of the utility model are: a kind of innovative small-sized unmanned aircraft of this utility model is scientific and reasonable for structure, easy-to-operate, the lower section of body is provided with steering gear, and the lower section of steering gear is provided with air jet system, by controlling the direction of air jet system jet and then adjusting the direction of machine flight, and air jet system can also accelerate the flight speed of machine, make aircraft speed faster, sensitiveer.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model；
Fig. 2 is the structural representation of controller of the present utility model；
In figure: 1-propeller, 2-motor, 3-body, 4-support, 5-fulcrum, 6-drive shaft, 7-battery, 8-steering gear, 9-air jet system, 10-helical-blade, 11-induction apparatus, 12-controller, 121-motor switch, 122-air jet system switch, 123-steering gear switch.
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is clearly and completely described, it is clear that described embodiment is only a part of embodiment of this utility model rather than whole embodiments.Based on the embodiment in this utility model, the every other embodiment that those of ordinary skill in the art are obtained under not making creative work premise, broadly fall into the scope of this utility model protection.
nullRefer to Fig. 1 and Fig. 2，This utility model a kind of innovative small-sized unmanned aircraft technical scheme of offer: a kind of innovative small-sized unmanned aircraft，Including propeller 1、Body 3 and steering gear 8，Propeller 1 is arranged on the top of drive shaft 5，And on propeller 1, it is provided with helical-blade 10，The lower section of drive shaft 5 is provided with motor 2，The lower section of motor 2 is provided with fulcrum 6，Fulcrum 6 be provided above support 4，Body 3 is arranged on support 4，Body 3 be internally provided with battery 7，The left side of battery 7 is provided with induction apparatus 11，Steering gear 8 is arranged on the lower section of body 3，And the lower section of steering gear 8 is provided with air jet system 9，Induction apparatus 11 and controller 12 wireless connections，Motor switch 121 it is provided with on controller 12、Air jet system switch 122 and steering gear switch 123，And motor switch 121、Air jet system switch 122 and steering gear switch 123 are all electrically connected with controller 12.
Fulcrum 6 is provided with four altogether.Motor 2 is provided with four altogether, and four motors 2 are separately mounted to the top of four fulcrums 6.Helical-blade 10 is provided with eight altogether, and eight helical-blades 10 are arranged on four propellers 1 the most uniformly.Connected by bearing between propeller 1 and drive shaft 5.
Operation principle: after this utility model installs, open the motor switch 121 on controller 12, air jet system switch 122 and steering gear to switch 123 machines and start working, at this moment propeller 1 meeting high speed rotating under the drive of motor 2, the rise of high speed rotating band movement machine, owing to being provided with steering gear 8 on machine, so air jet system switch 122 can be controlled carry out adjustment direction, adjusting the direction of machine flight, flight finishing control machine slowly lands.
Embodiment the most of the present utility model, for the ordinary skill in the art, being appreciated that in the case of without departing from principle of the present utility model and spirit and these embodiments can carry out multiple change, revise, replace and modification, scope of the present utility model is defined by the appended claims and the equivalents thereof.
Claims (5)
- null1. an innovative small-sized unmanned aircraft，Including propeller (1)、Body (3) and steering gear (8)，It is characterized in that: described propeller (1) is arranged on the top of drive shaft (5)，And on propeller (1), it is provided with helical-blade (10)，The lower section of described drive shaft (5) is provided with motor (2)，The lower section of described motor (2) is provided with fulcrum (6)，Described fulcrum (6) be provided above support (4)，Described body (3) is arranged on support (4)，Described body (3) be internally provided with battery (7)，The left side of described battery (7) is provided with induction apparatus (11)，Described steering gear (8) is arranged on the lower section of body (3)，And the lower section of steering gear (8) is provided with air jet system (9)，Described induction apparatus (11) and controller (12) wireless connections，Motor switch (121) it is provided with on described controller (12)、Air jet system switch (122) and steering gear switch (123)，And motor switch (121)、Air jet system switch (122) and steering gear switch (123) are all electrically connected with controller (12).
- The innovative small-sized unmanned aircraft of one the most according to claim 1, it is characterised in that: described fulcrum (6) is provided with four altogether.
- The innovative small-sized unmanned aircraft of one the most according to claim 1, it is characterised in that: described motor (2) is provided with four altogether, and four motors (2) are separately mounted to the top of four fulcrums (6).
- The innovative small-sized unmanned aircraft of one the most according to claim 1, it is characterised in that: described helical-blade (10) is provided with eight altogether, and eight helical-blades (10) are arranged on four propellers (1) the most uniformly.
- The innovative small-sized unmanned aircraft of one the most according to claim 1, it is characterised in that: connected by bearing between described propeller (1) and drive shaft (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620266405.4U CN205554566U (en) | 2016-04-04 | 2016-04-04 | Innovative small -size unmanned vehicles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620266405.4U CN205554566U (en) | 2016-04-04 | 2016-04-04 | Innovative small -size unmanned vehicles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205554566U true CN205554566U (en) | 2016-09-07 |
Family
ID=56813578
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620266405.4U Expired - Fee Related CN205554566U (en) | 2016-04-04 | 2016-04-04 | Innovative small -size unmanned vehicles |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205554566U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108216585A (en) * | 2018-01-29 | 2018-06-29 | 成都市煜沣科技有限公司 | A kind of jet-propelled undercarriage of civil small-scale unmanned plane |
| CN108516084A (en) * | 2018-03-30 | 2018-09-11 | 贵州大鸟创新科技有限公司 | A kind of unmanned plane |
| CN111096706A (en) * | 2019-12-31 | 2020-05-05 | 四川京航天程科技发展有限公司 | Self-wiping glass aerial work platform |
-
2016
- 2016-04-04 CN CN201620266405.4U patent/CN205554566U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108216585A (en) * | 2018-01-29 | 2018-06-29 | 成都市煜沣科技有限公司 | A kind of jet-propelled undercarriage of civil small-scale unmanned plane |
| CN108516084A (en) * | 2018-03-30 | 2018-09-11 | 贵州大鸟创新科技有限公司 | A kind of unmanned plane |
| CN108516084B (en) * | 2018-03-30 | 2021-06-25 | 贵州大鸟创新科技有限公司 | Unmanned aerial vehicle |
| CN111096706A (en) * | 2019-12-31 | 2020-05-05 | 四川京航天程科技发展有限公司 | Self-wiping glass aerial work platform |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US11603193B2 (en) | Aircraft convertible between fixed-wing and hovering orientations | |
| CN205554566U (en) | Innovative small -size unmanned vehicles | |
| CN104229138B (en) | Split differential tail wing control mechanism of flapping-wing micro air vehicle | |
| CN101879945A (en) | Electric tilting rotor wing unmanned aerial vehicle | |
| CN103318410A (en) | Vertical take-off and landing micro aerial vehicle without control surface | |
| CN106470899A (en) | The elimination torque of propeller type VTOL flying object and compatible device of keeping in balance | |
| CN110857145A (en) | Apparatus and method for improved stall/over-stall condition fixed wing aircraft pitch control | |
| CN204895843U (en) | Multiaxis aircraft | |
| CN113753229A (en) | Foldable fixed-wing four-rotor composite unmanned aerial vehicle and control method thereof | |
| CN107364572A (en) | Fixed-wing vector unmanned plane | |
| US11591084B2 (en) | Cycloidal rotor micro-air vehicle | |
| CN111086634B (en) | Dragonfly-like double-flapping-wing micro aircraft | |
| CN103332292A (en) | 4+4 rotor craft respectively controlled by lift force and navigation | |
| CN105329441B (en) | A kind of four axis all-wing aircraft aircraft of combined type | |
| CN103213681A (en) | Six-degree-of-freedom four-shaft aircraft | |
| CN102582833A (en) | Flying saucer in shape of tai chi | |
| CN106585981B (en) | Dragonfly-imitating double-wing miniature flapping-wing aircraft | |
| CN109050899A (en) | A kind of more helicopters | |
| CN205055430U (en) | But differential steering's high mobility model propeller aircraft | |
| CN206278270U (en) | A kind of VUAV vector puller system | |
| CN202219839U (en) | Omnidirectional flight wing structure of vertically taking-off and landing aircraft | |
| CN104627359B (en) | Multi-axis aircraft | |
| CN205819562U (en) | A kind of heavy－duty depopulated helicopter | |
| CN208882107U (en) | A kind of more helicopters | |
| Khan et al. | A critical analysis of small but heavy-lift multirotor and their flight controllers |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160907 Termination date: 20170404 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |