CN108408029A - A kind of center of gravity controllable type unmanned plane - Google Patents
A kind of center of gravity controllable type unmanned plane Download PDFInfo
- Publication number
- CN108408029A CN108408029A CN201810094859.1A CN201810094859A CN108408029A CN 108408029 A CN108408029 A CN 108408029A CN 201810094859 A CN201810094859 A CN 201810094859A CN 108408029 A CN108408029 A CN 108408029A
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- CN
- China
- Prior art keywords
- accumulator
- center
- gravity
- unmanned plane
- controllable type
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- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C17/00—Aircraft stabilisation not otherwise provided for
- B64C17/02—Aircraft stabilisation not otherwise provided for by gravity or inertia-actuated apparatus
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of center of gravity controllable type unmanned planes, belong to robot device field, including accumulator and center of gravity regulating box, the center of gravity regulating box is arranged in the both sides and bottom of the accumulator, the internal storage battery is provided with control module, it is provided with unmanned plane main body above the accumulator, it is provided with lift bar at the top of the accumulator, it is provided with screw blade on the lift bar, it is provided with signal antenna at the top of the lift bar, the accumulator tail portion is provided with tail vane, the bottom of storage battery is provided with floor stand, the center of gravity regulating box is by water injection pipe, filter screen, seperated case and drain valve composition, the filter screen setting is between the water injection pipe and the seperated case, the fission bottom portion is provided with the drain valve.The present invention can realize the flight attitude traveling function of plurality of stable according to the real-time center-of-gravity regulating of actual demand, and by the cooperation with the tail vane, and use is more flexible, more convenient operation.
Description
Technical field
The invention belongs to robot device fields, and in particular to a kind of center of gravity controllable type unmanned plane.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned aircraft that presetting apparatus manipulates, 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, unmanned plane+sector application are
Unmanned plane has really just needed；It taking photo by plane at present, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observing wild move
The application in object, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, greatly
The big purposes for having expanded unmanned plane itself, developed country is also in actively extension sector application and development unmanned air vehicle technique.
The position of centre of gravity of unmanned plane has the flight attitude of unmanned plane an important influence, and unmanned plane currently on the market
Generally do not have function of regulating center of gravity, flight attitude is also more single, it is difficult to control.
Invention content
The purpose of the present invention is that solve the above-mentioned problems and provides a kind of center of gravity controllable type unmanned plane.
The present invention is achieved through the following technical solutions above-mentioned purpose：
A kind of center of gravity controllable type unmanned plane, including accumulator and center of gravity regulating box, the center of gravity regulating box are arranged described
The both sides and bottom of accumulator, the internal storage battery are provided with control module, unmanned owner are provided with above the accumulator
Body, the accumulator top are provided with lift bar, screw blade are provided on the lift bar, is provided at the top of the lift bar
Signal antenna, the accumulator tail portion are provided with tail vane, and the bottom of storage battery is provided with floor stand, the center of gravity regulating box by
Water injection pipe, filter screen, seperated case and drain valve composition, the filter screen are arranged between the water injection pipe and the seperated case,
The fission bottom portion is provided with the drain valve, and the drain valve is made of solenoid valve and drainpipe.
Further, the accumulator is electrically connected with the unmanned plane main body, and the accumulator passes through with the lift bar
Bolts assemblies connect.
Further, the accumulator is electrically connected with the screw blade, and the accumulator is electrically connected with the signal antenna
It connects.
Further, the accumulator is electrically connected with the control module, the control module and the center of gravity regulating box
Electrical connection.
Further, the accumulator is electrically connected with the tail vane, and the accumulator passes through spiral shell with the center of gravity regulating box
Bolt twist-on, the accumulator pass through bolt twist-on with the floor stand.
Further, the water injection pipe and the filter screen nested encryptions, the fission case pass through pipe with the drain valve
Hoop sealing twist-on.
Further, the solenoid valve is connected to the drainpipe by pipeline.
Advantageous effect is：The present invention can be according to the real-time center-of-gravity regulating of actual demand, and by matching with the tail vane
It closes, realizes the flight attitude traveling function of plurality of stable, use is more flexible, more convenient operation.
Description of the drawings
Fig. 1 is a kind of front view of center of gravity controllable type unmanned plane of the present invention；
Fig. 2 is a kind of enlarged view of the center of gravity regulating box of center of gravity controllable type unmanned plane of the present invention；
Fig. 3 is a kind of enlarged view of the drain valve of center of gravity controllable type unmanned plane of the present invention.
Wherein：1, accumulator；2, unmanned plane main body；3, lift bar；4, screw blade；5, signal antenna；6, tail vane；7, again
Heart regulating box；8, floor stand；9, control module；701, water injection pipe；702, filter screen；703, seperated case；704, drain valve；705、
Solenoid valve；706, drainpipe.
Specific implementation mode
The invention will be further described below in conjunction with the accompanying drawings：
As shown in Figs. 1-3, a kind of center of gravity controllable type unmanned plane, including accumulator 1 and center of gravity regulating box 7, center of gravity regulating box 7
It is arranged in the both sides and bottom of accumulator 1, accumulator 1 is internally provided with control module 9, and 1 top of accumulator is provided with unmanned plane
Main body 2,1 top of accumulator are provided with lift bar 3, and screw blade 4 is provided on lift bar 3, and 3 top of lift bar is provided with signal
Antenna 5,1 tail portion of accumulator are provided with tail vane 6, and 1 bottom of accumulator is provided with floor stand 8, center of gravity regulating box 7 by water injection pipe 701,
Filter screen 702, seperated case 703 and drain valve 704 form, and the setting of filter screen 702 divides between water injection pipe 701 and seperated case 703
703 bottom of body case is provided with drain valve 704, and drain valve 704 is made of solenoid valve 705 and drainpipe 706.
In above structure, before take-off, center of gravity regulating box 7 is filled into water, in flight, the present invention by screw blade 4,
Lift bar 3 provides lift, and the present invention is driven to fly, and provides flight control by tail vane 6, when the center of gravity for needing the adjusting present invention
When, staff sends out wireless working signal, and the present invention receives wireless signal by signal antenna 5, and by wireless signal feedback
It is handled to control module 9, control module 9 controls solenoid valve 705 according to the wireless signal of reception and opens and closes, thus will
Water in corresponding fission case 703 is emitted by drainpipe 706, to adjust the center of gravity of the present invention.
Accumulator 1 is electrically connected with unmanned plane main body 2, and accumulator 1 can provide flying power for the present invention, accumulator 1 with
Lift bar 3 is connected by bolts assemblies, and lift bar 3 can connect screw blade 4 and unmanned plane main body 2, accumulator 1 and propeller
Leaf 4 is electrically connected, and accumulator 1 is electrically connected with signal antenna 5, and signal antenna 5 can receive wireless control signal, accumulator 1 and control
Molding block 9 is electrically connected, and control module 9 is electrically connected with center of gravity regulating box 7, and control module 9 can control the center of gravity of center of gravity regulating box 7
Distribution, accumulator 1 are electrically connected with tail vane 6, and tail vane 6 can adjust the flight attitude of the present invention, accumulator 1 and center of gravity regulating box 7
By bolt twist-on, with floor stand 8 by bolt twist-on, floor stand 8 can provide accumulator 1 for the takeoff and landing of the present invention
Bradyseism, water injection pipe 701 and 702 nested encryptions of filter screen, seperated case 703 seal twist-on, solenoid valve with drain valve 704 by pipe collar
705 are connected to drainpipe 706 by pipeline, and solenoid valve 705 can control the opening and closing of drainpipe 706, are divided to adjust
Water in body case 703 achievees the purpose that adjust center of gravity of the present invention.
It should be noted that the above embodiments are merely illustrative of the technical solutions of the present invention, rather than its limitations；Although ginseng
According to previous embodiment, invention is explained in detail, it will be understood by those of ordinary skill in the art that：It still can be with
Technical scheme described in the above embodiments is modified or equivalent replacement of some of the technical features；And
These modifications or replacements, the spirit and model of various embodiments of the present invention technical solution that it does not separate the essence of the corresponding technical solution
It encloses.
Claims (7)
1. a kind of center of gravity controllable type unmanned plane, it is characterised in that：Including accumulator and center of gravity regulating box, the center of gravity regulating box is set
It sets in the both sides and bottom of the accumulator, the internal storage battery is provided with control module, is provided with above the accumulator
Unmanned plane main body, the accumulator top are provided with lift bar, screw blade, lift bar top are provided on the lift bar
Portion is provided with signal antenna, and the accumulator tail portion is provided with tail vane, and the bottom of storage battery is provided with floor stand, the center of gravity
Regulating box is made of water injection pipe, filter screen, seperated case and drain valve, and the filter screen is arranged in the water injection pipe and the fission
Between case, the fission bottom portion is provided with the drain valve, and the drain valve is made of solenoid valve and drainpipe.
2. a kind of center of gravity controllable type unmanned plane according to claim 1, it is characterised in that：The accumulator with it is described nobody
Owner's body is electrically connected, and the accumulator is connect with the lift bar by bolts assemblies.
3. a kind of center of gravity controllable type unmanned plane according to claim 1, it is characterised in that：The accumulator and the spiral
Blade is electrically connected, and the accumulator is electrically connected with the signal antenna.
4. a kind of center of gravity controllable type unmanned plane according to claim 1, it is characterised in that：The accumulator and the control
Module is electrically connected, and the control module is electrically connected with the center of gravity regulating box.
5. a kind of center of gravity controllable type unmanned plane according to claim 1, it is characterised in that：The accumulator and the tail vane
Electrical connection, for the accumulator with the center of gravity regulating box by bolt twist-on, the accumulator passes through bolt with the floor stand
Twist-on.
6. a kind of center of gravity controllable type unmanned plane according to claim 1, it is characterised in that：The water injection pipe and the filtering
Net nested encryptions, the fission case seal twist-on with the drain valve by pipe collar.
7. a kind of center of gravity controllable type unmanned plane according to claim 1, it is characterised in that：The solenoid valve and the draining
Pipe is connected to by pipeline.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810094859.1A CN108408029A (en) | 2018-01-31 | 2018-01-31 | A kind of center of gravity controllable type unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810094859.1A CN108408029A (en) | 2018-01-31 | 2018-01-31 | A kind of center of gravity controllable type unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108408029A true CN108408029A (en) | 2018-08-17 |
Family
ID=63127353
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810094859.1A Pending CN108408029A (en) | 2018-01-31 | 2018-01-31 | A kind of center of gravity controllable type unmanned plane |
Country Status (1)
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| CN (1) | CN108408029A (en) |
Citations (8)
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|---|---|---|---|---|
| CN203876985U (en) * | 2014-06-05 | 2014-10-15 | 长沙威航农业科技有限公司 | Remote control pesticide spraying helicopter with automatic balancing function |
| CN104875877A (en) * | 2015-06-11 | 2015-09-02 | 上海优伟斯智能***有限公司 | Automatic balancing system for unmanned aerial vehicle |
| CN105129045A (en) * | 2015-07-02 | 2015-12-09 | 初君年 | No incline and no sink ship |
| CN105752354A (en) * | 2016-04-21 | 2016-07-13 | 捷西迪（广州）光学科技有限公司 | Gravity center change compensation device and method for unmanned aircraft |
| WO2016119065A1 (en) * | 2015-01-29 | 2016-08-04 | Rocky Mountain Equipment Canada Ltd. | Uav navigation and sensor system configuration |
| CN105966610A (en) * | 2016-06-29 | 2016-09-28 | 南京信息工程大学 | Centre-of-gravity shift and yaw single-rotor helicopter |
| CN106608349A (en) * | 2015-10-23 | 2017-05-03 | 中国飞行试验研究院 | Airborne vertical liquid storage tank for gravity centre adjustment of large transport aircraft |
| CN106744361A (en) * | 2016-12-23 | 2017-05-31 | 深圳市福田区青少年科技教育协会 | One kind automatically adjusts head mast device |
-
2018
- 2018-01-31 CN CN201810094859.1A patent/CN108408029A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203876985U (en) * | 2014-06-05 | 2014-10-15 | 长沙威航农业科技有限公司 | Remote control pesticide spraying helicopter with automatic balancing function |
| WO2016119065A1 (en) * | 2015-01-29 | 2016-08-04 | Rocky Mountain Equipment Canada Ltd. | Uav navigation and sensor system configuration |
| CN104875877A (en) * | 2015-06-11 | 2015-09-02 | 上海优伟斯智能***有限公司 | Automatic balancing system for unmanned aerial vehicle |
| CN105129045A (en) * | 2015-07-02 | 2015-12-09 | 初君年 | No incline and no sink ship |
| CN106608349A (en) * | 2015-10-23 | 2017-05-03 | 中国飞行试验研究院 | Airborne vertical liquid storage tank for gravity centre adjustment of large transport aircraft |
| CN105752354A (en) * | 2016-04-21 | 2016-07-13 | 捷西迪（广州）光学科技有限公司 | Gravity center change compensation device and method for unmanned aircraft |
| CN105966610A (en) * | 2016-06-29 | 2016-09-28 | 南京信息工程大学 | Centre-of-gravity shift and yaw single-rotor helicopter |
| CN106744361A (en) * | 2016-12-23 | 2017-05-31 | 深圳市福田区青少年科技教育协会 | One kind automatically adjusts head mast device |
Non-Patent Citations (1)
| Title |
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| 贺天鹏: "《无人直升机***设计》", 31 December 2016 * |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180817 |
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| RJ01 | Rejection of invention patent application after publication |