CN109398706A - A kind of unmanned plane during flying is the mechanical structure for extending endurance and leaving battery on horn - Google Patents
A kind of unmanned plane during flying is the mechanical structure for extending endurance and leaving battery on horn Download PDFInfo
- Publication number
- CN109398706A CN109398706A CN201811477786.0A CN201811477786A CN109398706A CN 109398706 A CN109398706 A CN 109398706A CN 201811477786 A CN201811477786 A CN 201811477786A CN 109398706 A CN109398706 A CN 109398706A
- Authority
- CN
- China
- Prior art keywords
- battery
- steering engine
- arm
- unmanned plane
- horn
- 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.)
- Pending
Links
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims abstract description 19
- 229910052744 lithium Inorganic materials 0.000 claims abstract description 19
- 230000007306 turnover Effects 0.000 claims abstract description 7
- 238000009434 installation Methods 0.000 claims abstract description 3
- 238000000034 method Methods 0.000 claims description 5
- 230000005611 electricity Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000006116 polymerization reaction Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Toys (AREA)
Abstract
The invention belongs to unmanned plane instrument field, disclosing a kind of unmanned plane during flying is the mechanical structure for extending endurance and leaving battery on horn；It is provided with lithium battery, position has been bolted steering engine on rotating arm among lithium battery, steering engine has been bolted steering engine swing arm, steering engine swing arm is connect with bolt, left-handed pivoted arm and dextrorotation pivoted arm are provided with long-armed, bolt is connect with the long-armed through-hole being provided with, and left-handed pivoted arm and dextrorotation pivoted arm are provided with spring mounting hole, for installing spring；By rotational axis hole installation rotation axis, rotational axis hole lower part is set with pipe clamp for left-handed pivoted arm and dextrorotation pivoted arm, and pipe clamp suit is fixed on more rotor horns；Turnover panel is welded on long-armed.The present invention can increase the flight time of multi-rotor unmanned aerial vehicle, improve the working efficiency of unmanned plane by being provided with the mechanical structure for leaving battery on horn.
Description
Technical field
Horn is left the invention belongs to unmanned plane instrument field more particularly to a kind of unmanned plane during flying for extension endurance to power on
The mechanical structure in pond.
Background technique
Currently, the prior art commonly used in the trade is such that
Multi-rotor unmanned aerial vehicle has the advantages such as reliable and stable, easy to operate, duties height.It is obtained in recent years in every field
It is widely applied.Consider mechanical reliability, more rotors do not have movable part, its reliability is substantially dependent on brushless motor
Reliability, therefore reliability is higher.Multi-rotor unmanned aerial vehicle do not need runway can VTOL, can be hanged in the sky after taking off
Stop.Its manipulating principle is simple, and four remote sensing of control device operate the front and rear, left and right, up and down and yaw direction of corresponding aircraft
Movement.In terms of automatic pilot, multi-rotor unmanned aerial vehicle autopilot control method is simple, and controller parameter adjusts also very simple.
Multi-rotor unmanned aerial vehicle is because its structure is simple, if motor, electron speed regulator, battery, paddle and rack damage, it is easy to replace.
But relative to helicopter and fixed wing aircraft, multi-rotor unmanned aerial vehicle working efficiency is lower；I.e. relative to helicopter
And fixed wing aircraft, in the case where same load-carrying, the endurance of more rotors is shorter.And multi-rotor unmanned aerial vehicle is mostly using polymerization at present
The weight of object lithium battery, lithium battery can't be reduced with the consumption of electricity, so after dead battery capability, battery can be at
For useless load, it is further reduced the cruise duration of more rotors.
In conclusion problem of the existing technology is:
After dead battery capability, battery can become useless load, be further reduced the cruise duration of more rotors.Endurance
Reduction can be such that the unmanned plane skyborne flight time reduces, and reduce the time that aircraft executes task.
It solves the difficulty and meaning of above-mentioned technical problem: realizing leaving for unmanned plane horn battery, will increase unmanned plane
Cruise duration makes unmanned plane have the looser time to complete task, and can receive more tasks.And the difficulty of the technology
Point is: not leaving in battery is, can be reliably fixed；And battery is when leaving, and needs mechanical structure reliable, guarantees horn
Battery leaves completely.
Summary of the invention
It in view of the problems of the existing technology, is to extend endurance to leave on horn the present invention provides a kind of unmanned plane during flying
The mechanical structure of battery.
The invention is realized in this way a kind of unmanned plane during flying is to extend endurance to leave the mechanical structure of battery on horn and set
It is equipped with lithium battery, position has been bolted steering engine among lithium battery, and steering engine has been bolted steering engine swing arm, steering engine pendulum
Arm is connect with bolt, and left-handed pivoted arm and dextrorotation pivoted arm are provided with long-armed, and bolt is connect with the long-armed through-hole being provided with, left-handed pivoted arm and
Dextrorotation pivoted arm is provided with spring mounting hole, for installing spring；
Further, the left-handed pivoted arm and dextrorotation pivoted arm pass through rotational axis hole installation rotation axis, rotational axis hole lower part suit
There is pipe clamp, pipe clamp suit is fixed on more rotor horns.
Further, turnover panel is welded on long-armed.
In conclusion advantages of the present invention and good effect are as follows: the present invention is by being provided with the machine for leaving battery on horn
Tool structure can increase the flight time of multi-rotor unmanned aerial vehicle, improve the working efficiency of unmanned plane.
And technology reduces unmanned plane weight in addition to simplifying unmanned plane structure at present, other than Lai Zengjia unmanned plane cruise duration,
It is main to pass through the electric hybrid technology of oil (such as patent publication No. CN207120892U " mixed dynamic unmanned plane ") and solar energy (such as patent disclosure
Number CN106972612A " a method of improve the power supply structure in four-axle aircraft cruise duration ") etc. introduce the supply of other abilities
Improve unmanned plane cruise duration, in this way the power supply mode of two or more energy will be unmanned plane structure, power supply system more
Add cumbersome, and this patent only passes through lithium battery power supply, more succinctly, reliably.
Detailed description of the invention
Fig. 1 is that unmanned plane during flying provided in an embodiment of the present invention is to extend endurance to leave the mechanical structure of battery on horn and show
It is intended to；
Fig. 2 is swing boom configuration schematic diagram in right side provided in an embodiment of the present invention；
In figure: 1, more rotor horns；2, steering engine swing arm；3, pipe clamp；4, steering engine；5, left-handed pivoted arm；6, lithium battery；7, dextrorotation
Pivoted arm；8, bolt；9, rotation axis；10, spring mounting hole；11, through-hole；12, turnover panel；13, long-armed；14, steering engine bearing is (wherein
10,11,12,13,14 be the part-structure on cursor).
Specific embodiment
In order to make the objectives, technical solutions, and advantages of the present invention clearer, with reference to embodiments, to the present invention
It is further elaborated.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, it is not used to
Limit the present invention.
Application principle of the invention is explained in detail with reference to the accompanying drawing.
As Figure 1-Figure 2, unmanned plane during flying provided in an embodiment of the present invention is to extend endurance to leave battery on horn
Mechanical structure includes: more rotor horns 1, steering engine swing arm 2, pipe clamp 3, steering engine 4, left-handed pivoted arm 5, lithium battery 6, dextrorotation pivoted arm 7, inserts
Pin 8, rotation axis 9, spring mounting hole 10, through-hole 11, turnover panel 12, long-armed 13, steering engine bearing 14.
There are two pipe clamps 3 for suit on more rotor horns 1, are fixed by screws on horn, are located at 6 liang of lithium battery
Side；Steering engine 4 is fixed by screws in the steering engine bearing 14 of left-handed pivoted arm, is fixed with steering engine swing arm by screw on steering engine 4
2；Have rotational axis hole on pipe clamp 3, rotation axis 9 connects left-handed pivoted arm 5 and dextrorotation pivoted arm 7 by rotational axis hole, wherein rotation axis with
Rotational axis hole is fixed by interference fit, is clearance fit between rotation axis and cursor；Pipe clamp is fixed, and left-handed pivoted arm
5 and dextrorotation pivoted arm 7 can be rotated around rotation axis 9, the longer arm on left-handed pivoted arm 5 and dextrorotation pivoted arm 7 is designated as 13, and (i.e. long-armed 13 be to turn
A part of swing arm part)；Bolt 8 and steering engine swing arm 2 pass through split pin connection, and the through-hole 11 on long-armed 13 is for being inserted into bolt
8, left/right rotation swing arm is connected by bolt 8, thus fixed battery；Left-right rotary pivoted arm is provided with spring mounting hole 10, for pacifying
Shock mount, turnover panel 12 are also long-armed 13 last points, for overthrowing battery, complete to leave.
The operation principle of the present invention is that:
When not leaving battery, bolt 8 is inserted into the through-hole 11 of left and right rotating arm 5/7, therefore is mounted on left and right rudder horn spring
The spring of mounting hole 10 cannot be such that left-right rotary pivoted arm overturns, so that lithium battery 6 is fixed by left and right rotating arm,；In steering engine 4
It receives after leaving the order of battery, the steering engine disk rotation on steering engine, steering engine disk drives steering engine arm 2 to rotate, the rotation of steering engine arm 2
Movement pulls out bolt 8, and spring tension makes left-right rotary pivoted arm rotate the rotation of moving axis 9 at this time, while rotating arm flap 12 being driven to touch
Lithium battery is hit, lithium battery is made to turn on one's side, completion leaves movement.
In 4 direction side of steering engine, long-armed the 13 of left-handed pivoted arm 5 and dextrorotation pivoted arm 7 are longer, in 4 position of steering engine, two rotating arms
It is connected by long-armed through-hole 11 with bolt 8, has spring mounting hole 10 in left-right rotary pivoted arm, for installing spring.Pass through
Bolt 8 fixes left-right rotary pivoted arm, and left-right rotary pivoted arm is fixed together at this time, and spring tension cannot play the dynamic of overturning rotating arm
Make；And then by the fixed battery of left-right rotary pivoted arm, it is fixed on battery on round horn.It is consumed in 6 electricity of horn lithium battery
After to the greatest extent, steering engine 4, which receives, leaves cell commands, and steering engine 4 drives steering engine swing arm 2 to rotate, and rotates left and right so that bolt 8 be driven to be detached from
The long-armed through-hole of arm, left-right rotary pivoted arm rotate under the pulling force of spring around rotation axis 9, and battery is turned on one's side under the action of turnover panel 12,
Completion leaves movement.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all in essence of the invention
Made any modifications, equivalent replacements, and improvements etc., should all be included in the protection scope of the present invention within mind and principle.
Claims (5)
1. a kind of unmanned plane during flying is to extend endurance to leave the mechanical structure of battery on horn, which is characterized in that described nobody
Machine flight leaves the mechanical structure of battery on horn for extension endurance and is provided with
Lithium battery；
Position has been bolted steering engine on rotating arm among lithium battery, and steering engine has been bolted steering engine swing arm, rudder
Machine swing arm is connect with bolt, and left-handed pivoted arm and dextrorotation pivoted arm are provided with long-armed, and bolt is connect with the long-armed through-hole being provided with, anticlockwise
Arm and dextrorotation pivoted arm are provided with spring mounting hole, for installing spring.
2. unmanned plane during flying as described in claim 1 is the mechanical structure for extending endurance and leaving battery on horn, feature exists
In by rotational axis hole installation rotation axis, rotational axis hole lower part is set with pipe clamp, pipe clamp set for the left-handed pivoted arm and dextrorotation pivoted arm
Dress is fixed on more rotor horns.
3. unmanned plane during flying as described in claim 1 is the mechanical structure for extending endurance and leaving battery on horn, feature exists
In, it is described it is long-armed on be welded with turnover panel.
4. a kind of unmanned plane during flying as described in claim 1 is the user for extending endurance and leaving the mechanical structure of battery on horn
Method, which is characterized in that the unmanned plane during flying is to extend endurance and leave the application method of the mechanical structure of battery on horn to include:
When not leaving battery, bolt is inserted into the through-hole of left and right rotating arm 5/7, fixes lithium battery by left and right rotating arm；?
Steering engine receives leave the order of battery after, steering engine disk on steering engine rotation, steering engine disk drives the rotation of steering engine arm, the rotation of steering engine arm
Transhipment is dynamic to pull out bolt, and spring tension makes left-right rotary pivoted arm rotate moving axis rotation at this time, while rotating arm flap being driven to collide
Lithium battery makes lithium battery turn on one's side, and completion leaves movement.
It using unmanned plane during flying described in claims 1 to 3 any one is to extend endurance to leave the machine of battery on horn 5. a kind of
The unmanned plane of tool structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811477786.0A CN109398706A (en) | 2018-12-05 | 2018-12-05 | A kind of unmanned plane during flying is the mechanical structure for extending endurance and leaving battery on horn |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811477786.0A CN109398706A (en) | 2018-12-05 | 2018-12-05 | A kind of unmanned plane during flying is the mechanical structure for extending endurance and leaving battery on horn |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109398706A true CN109398706A (en) | 2019-03-01 |
Family
ID=65457233
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811477786.0A Pending CN109398706A (en) | 2018-12-05 | 2018-12-05 | A kind of unmanned plane during flying is the mechanical structure for extending endurance and leaving battery on horn |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109398706A (en) |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103963974A (en) * | 2013-01-30 | 2014-08-06 | 中国科学院沈阳自动化研究所 | Automatic dispenser |
| US20140339371A1 (en) * | 2012-03-30 | 2014-11-20 | W. Morrison Consulting Group, Inc. | Long Range Electric Aircraft and Method of Operating Same |
| CN205524989U (en) * | 2016-01-27 | 2016-08-31 | 厦门大学 | Load air -drop unmanned aerial vehicle's input device |
| CN205952319U (en) * | 2016-08-04 | 2017-02-15 | 广州习疆电子科技有限公司 | Can put in unmanned aerial vehicle of life buoy |
| CN107600439A (en) * | 2017-09-26 | 2018-01-19 | 上海重塑能源科技有限公司 | A kind of long endurance unmanned aircraft electrical source of power device and unmanned plane |
| CN207045715U (en) * | 2017-06-27 | 2018-02-27 | 重庆市亿飞智联科技有限公司 | A kind of novel and multifunctional unmanned plane |
| CN108287496A (en) * | 2017-12-28 | 2018-07-17 | 中国航天系统科学与工程研究院 | A kind of UAV Intelligent battery leaves control system |
| CN108341066A (en) * | 2018-03-30 | 2018-07-31 | 贵州大鸟创新科技有限公司 | Unmanned plane falling protecting device |
| CN209305842U (en) * | 2018-12-05 | 2019-08-27 | 智灵飞（北京）科技有限公司 | A kind of unmanned plane during flying is the mechanical structure for extending endurance and leaving battery on horn |
-
2018
- 2018-12-05 CN CN201811477786.0A patent/CN109398706A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20140339371A1 (en) * | 2012-03-30 | 2014-11-20 | W. Morrison Consulting Group, Inc. | Long Range Electric Aircraft and Method of Operating Same |
| CN103963974A (en) * | 2013-01-30 | 2014-08-06 | 中国科学院沈阳自动化研究所 | Automatic dispenser |
| CN205524989U (en) * | 2016-01-27 | 2016-08-31 | 厦门大学 | Load air -drop unmanned aerial vehicle's input device |
| CN205952319U (en) * | 2016-08-04 | 2017-02-15 | 广州习疆电子科技有限公司 | Can put in unmanned aerial vehicle of life buoy |
| CN207045715U (en) * | 2017-06-27 | 2018-02-27 | 重庆市亿飞智联科技有限公司 | A kind of novel and multifunctional unmanned plane |
| CN107600439A (en) * | 2017-09-26 | 2018-01-19 | 上海重塑能源科技有限公司 | A kind of long endurance unmanned aircraft electrical source of power device and unmanned plane |
| CN108287496A (en) * | 2017-12-28 | 2018-07-17 | 中国航天系统科学与工程研究院 | A kind of UAV Intelligent battery leaves control system |
| CN108341066A (en) * | 2018-03-30 | 2018-07-31 | 贵州大鸟创新科技有限公司 | Unmanned plane falling protecting device |
| CN209305842U (en) * | 2018-12-05 | 2019-08-27 | 智灵飞（北京）科技有限公司 | A kind of unmanned plane during flying is the mechanical structure for extending endurance and leaving battery on horn |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205891232U (en) | Urgent safe launching appliance of four rotor unmanned aerial vehicle | |
| CN106414238B (en) | Drone configuration and battery augmentation for drone internal combustion engine, and related systems and methods | |
| US20200062383A1 (en) | Aircraft convertible between fixed-wing and hovering orientations | |
| CN109153447B (en) | Stop-and-rotate type rotor aircraft | |
| KR101895366B1 (en) | the improved hybrid drone | |
| US11738868B2 (en) | Aircraft with wingtip positioned propellers | |
| US20230056695A1 (en) | Hover and thrust control assembly for dual-mode aircraft | |
| WO2018163171A1 (en) | Vertical takeoff and landing light aircraft | |
| CN102285450A (en) | Pitch control three-axis aircraft | |
| CN105667780A (en) | Multi-rotor aircraft | |
| US20210139138A1 (en) | Methods and systems for reducing rotor acoustics of an aircraft | |
| CN106494291B (en) | A kind of military vehicle and its self-adjusting method carrying multi-rotor unmanned aerial vehicle | |
| CN104494820A (en) | Oil-driven four-rotor-wing unmanned aerial vehicle | |
| CN104743107A (en) | Multi-rotor type aircraft | |
| US20230159160A1 (en) | Hover and thrust control assembly for dual-mode aircraft | |
| CN204433050U (en) | The hardware platform of dynamic four rotor unmanned aircrafts of oil | |
| CN213414216U (en) | Vertical take-off and landing fixed wing unmanned aerial vehicle | |
| CN209305842U (en) | A kind of unmanned plane during flying is the mechanical structure for extending endurance and leaving battery on horn | |
| WO2022033305A1 (en) | Method and apparatus for controlling unmanned aerial vehicle, and storage medium | |
| US12043377B2 (en) | Rotatable thruster aircraft | |
| CN109398706A (en) | A kind of unmanned plane during flying is the mechanical structure for extending endurance and leaving battery on horn | |
| CN109250095A (en) | A kind of VTOL fixed wing aircraft | |
| CN214190099U (en) | Locking device of rotor propeller of vertical take-off and landing fixed wing unmanned aerial vehicle | |
| CN208360499U (en) | A kind of electronic empennage mechanism of agricultural plant protection unmanned plane | |
| CN214493340U (en) | Flapping wing aircraft with parachute function |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |