CN107444628A - A kind of new unmanned plane with drop resistant abrasion-resistant blade - Google Patents
A kind of new unmanned plane with drop resistant abrasion-resistant blade Download PDFInfo
- Publication number
- CN107444628A CN107444628A CN201710610952.9A CN201710610952A CN107444628A CN 107444628 A CN107444628 A CN 107444628A CN 201710610952 A CN201710610952 A CN 201710610952A CN 107444628 A CN107444628 A CN 107444628A
- Authority
- CN
- China
- Prior art keywords
- blade
- unmanned plane
- base
- lithium battery
- fixed
- 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
- 238000005299 abrasion Methods 0.000 title claims abstract description 17
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims abstract description 30
- 229910052744 lithium Inorganic materials 0.000 claims abstract description 30
- 230000002787 reinforcement Effects 0.000 claims abstract description 15
- 238000003869 coulometry Methods 0.000 claims abstract description 14
- 239000000463 material Substances 0.000 claims abstract description 8
- ZLMJMSJWJFRBEC-UHFFFAOYSA-N Potassium Chemical compound [K] ZLMJMSJWJFRBEC-UHFFFAOYSA-N 0.000 claims abstract description 6
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 6
- 229910052700 potassium Inorganic materials 0.000 claims abstract description 6
- 239000011591 potassium Substances 0.000 claims abstract description 6
- 239000010959 steel Substances 0.000 claims abstract description 6
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical group [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 claims description 4
- 229910001928 zirconium oxide Inorganic materials 0.000 claims description 4
- 230000008878 coupling Effects 0.000 claims description 3
- 238000010168 coupling process Methods 0.000 claims description 3
- 238000005859 coupling reaction Methods 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims description 3
- 238000003466 welding Methods 0.000 claims description 3
- 230000002093 peripheral effect Effects 0.000 claims 1
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 abstract description 4
- 238000010248 power generation Methods 0.000 abstract description 3
- 230000002159 abnormal effect Effects 0.000 abstract description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- VYQRBKCKQCRYEE-UHFFFAOYSA-N ctk1a7239 Chemical compound C12=CC=CC=C2N2CC=CC3=NC=CC1=C32 VYQRBKCKQCRYEE-UHFFFAOYSA-N 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000003912 environmental pollution Methods 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/473—Constructional features
-
- 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
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/473—Constructional features
- B64C2027/4733—Rotor blades substantially made from particular materials
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The present invention discloses a kind of new unmanned plane with drop resistant abrasion-resistant blade, including frame, base and undercarriage, the body bottom surface is provided with the base, the base both sides are provided with the undercarriage, the susceptor surface is provided with display screen, the display screen side is provided with controlling switch, and the chassis interior bottom surface is provided with lithium battery.The unmanned plane blade of the present invention is made of zirconia material, the embedded reinforcement made of potassium steel of blade simultaneously, add the intensity of blade and ensure that wearability, blade is avoided to be broken and influence the use of unmanned plane, it is provided with solar energy film plate simultaneously, it can be stored in by solar power generation in lithium battery and be powered for device, using self-powered mode, it is green, it is provided with coulometric detector simultaneously, information about power can be obtained in real time and is shown on a display screen, avoid abnormal air crash caused by being taken off when not enough power supply.
Description
Technical field
The present invention relates to unmanned plane field, is specifically related to a kind of new unmanned plane with drop resistant abrasion-resistant blade.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, without driving cabin on machine, but the equipment such as automatic pilot, presetting apparatus are installed, on ground, naval vessels or
Machine tool remote control station personnel are tracked to it, positioned, being remotely controlled, remote measurement and Digital Transmission by equipment such as radars, can be in radio
Take off as conventional airplane or launched with booster rocket under remote control, can also take aerial launch to by machine tool and fly, recovery
When, the mode automatic Landing as conventional airplane landing mission can be used, can also be reclaimed by remote control parachute or block, can
Repetitiousness is used repeatedly, and the blade of traditional unmanned plane is typically made of injection, is easily fallen in the improper landing of unmanned plane
It is bad, and blade is due to long-term high-speed rotation, easily abrasion, while unmanned plane is typically powered by the way of power supply is changed,
Battery abandons and easily causes environmental pollution, and is not provided with electric quantity monitoring function, it is impossible to the electricity of power supply is monitored, if
Not enough power supply is directly gone up to the air, and easily causes air crash, it is therefore desirable to a kind of new unmanned plane with drop resistant abrasion-resistant blade.
The content of the invention
The purpose of the present invention is that to solve the above problems and provides a kind of new nothing with drop resistant abrasion-resistant blade
It is man-machine.
The present invention is achieved through the following technical solutions above-mentioned purpose：
A kind of new unmanned plane with drop resistant abrasion-resistant blade, including frame, base and undercarriage, the body bottom surface are set
The base is equipped with, the base both sides are provided with the undercarriage, and the susceptor surface is provided with display screen, the display screen
Side is provided with controlling switch, and the chassis interior bottom surface is provided with lithium battery, and charging circuit, institute are provided with the lithium battery
State charging circuit side and be provided with coulometric detector, the lithium battery side is provided with control main frame, the frame surrounding ends
Mounting seat is provided with, the mounting seat inner bottom surface is provided with electric machine stand, and servomotor, institute are provided with the electric machine stand
Stating servomotor end set has rotating shaft, and the roller end is provided with blade, and the blade surface is provided with solar energy film
Plate, the blade interior are provided with reinforcement.
Further, the base is fixed by screws in the frame, and the undercarriage is fixed by snap in institute
State in frame, the display screen is glued on the base.
Further, the controlling switch is fixed on the base by neck, and the lithium battery is fixed by neck
In the base, the charging circuit is fixed by snap on the lithium battery, and the coulometric detector is consolidated by buckle
It is scheduled on the lithium battery.
Further, the control main frame is fixed in the base by neck, and the mounting seat welding is in the machine
On frame, the electric machine stand is fixed by screws in the mounting seat, and the quantity of the servomotor is four, the servo
Motor is fixed by screws on the electric machine stand.
Further, the rotating shaft is connected with the servomotor by shaft coupling, and the material of the blade is zirconium oxide,
The blade is threadedly secured in the rotating shaft.
Further, the solar energy film plate is glued on the blade, and the material of the reinforcement is potassium steel, institute
Reinforcement is stated to be embedded in the blade.
Further, the control main frame and the charging circuit, the lithium battery, the coulometric detector, described watch
Take motor, the display screen is connected with the controlling switch by wire.
Beneficial effect：The unmanned plane blade of the present invention is made of zirconia material, while blade is embedded by potassium steel system
Into reinforcement, add the intensity of blade and ensure that wearability, avoid blade and broken and influence the use of unmanned plane,
Solar energy film plate is provided with simultaneously, can be stored in by solar power generation in lithium battery and be powered for device, using certainly
The mode of power supply, it is green, while coulometric detector is provided with, information about power can be obtained in real time and be shown in display screen
On, avoid abnormal air crash caused by being taken off when not enough power supply.
Brief description of the drawings
Fig. 1 is the overall diagram of the present invention；
Fig. 2 is the interior view of the present invention；
Fig. 3 is the blade exterior figure of the present invention；
Fig. 4 is the blade interior figure of the present invention.
Description of reference numerals is as follows：
1st, blade；2nd, rotating shaft；3rd, frame；4th, undercarriage；5th, mounting seat；6th, display screen；7th, controlling switch；8th, base；9、
Servomotor；10th, electric machine stand；11st, lithium battery；12nd, control main frame；13rd, charging circuit；14th, coulometric detector；15th, the sun
Can thin web；16th, reinforcement.
Embodiment
The invention will be further described below in conjunction with the accompanying drawings：
As Figure 1-Figure 4, a kind of new unmanned plane with drop resistant abrasion-resistant blade, including frame 3, base 8 and rise and fall
Frame 4, body bottom surface are provided with base 8, and base 8 is used for installing fixed control assembly, and the both sides of base 8 are provided with undercarriage 4, risen and fallen
Frame 4 is used for facilitating unmanned plane landing, and the surface of base 8 is provided with display screen 6, and display screen 6 is used for real-time display information about power, display
To shield 6 sides and be provided with controlling switch 7, controlling switch 7 is used for sending work order, and the inner bottom surface of base 8 is provided with lithium battery 11,
Lithium battery 11 is used for providing electric energy for the consuming parts of device, charging circuit 13 is provided with lithium battery 11, charging circuit 13 is used
To be charged for lithium battery 11, the side of charging circuit 13 is provided with coulometric detector 14, and coulometric detector 14 is used for obtaining lithium in real time
The information about power of battery 11, the side of lithium battery 11 are provided with control main frame 12, and control main frame 12 is the control centre of device, frame
3 surrounding ends are provided with mounting seat 5, and mounting seat 5 is used for installing the fixed component that takes off, and the inner bottom surface of mounting seat 5 is provided with motor
Support 10, electric machine stand 10 are used for installing fixed servomotor 9, and servomotor 9, servomotor 9 are provided with electric machine stand 10
For driving rotating shaft 2 to rotate, the end set of servomotor 9 has rotating shaft 2, and rotating shaft 2 is used for band movable vane piece 1 and rotated, and the end of rotating shaft 2 is set
Blade 1 is equipped with, blade 1 carries out the operation such as take off by rotating, and the surface of blade 1 is provided with solar energy film plate 15, solar energy
Thin web 15 is used for absorbing solar power generation, and blade 1 is internally provided with reinforcement 16, and reinforcement 16 is used for increasing the strong of blade 1
Degree.
In said structure, solar energy film plate 15 is provided with blade 1, the solar energy in the external world can be absorbed and be converted to electricity
Charging circuit 13 can be delivered to by wire, lithium battery 11 is charged by charging circuit 13 by electrical power storage for device
Consuming parts are used, and blade 1 is made of zirconium oxide, are had the wearability of height, can be prevented blade 1 from wearing and influenceing unmanned plane
Use, while reinforcement 16 is provided with blade 1, reinforcement 16 is made of potassium steel, can greatly strengthen the strong of blade 1
Degree, avoids blade 1 from damaging, and when needing to use device, user sends work order, work order by extraneous remote control
Control main frame 12 is sent to by wireless signal, work order is passed to servomotor 9, servo by control main frame 12 by wire
The work of motor 9 drives rotating shaft 2 to rotate, and rotating shaft 2 is rotated with movable vane piece 1 to complete the lifting of unmanned plane, and can be by controlling servo
The working quantity of motor 9 completes turning function, and when needing to use electric quantity monitoring function, user is sent by controlling switch 7
Work order, work order pass to control main frame 12 by wire, and control main frame 12 passes to work order by wire
Coulometric detector 14, the work of coulometric detector 14 are used for obtaining the information about power of lithium battery 11 in real time, and information about power is passed through
Wire passes to control main frame 12, and information about power is passed to display screen 6 by wire and shown in real time above by control main frame 12
Show to observe for user and understand, air crash is caused using unmanned plane when avoiding not enough power supply.
In order to further improve a kind of use function of the new unmanned plane with drop resistant abrasion-resistant blade, base 8 passes through spiral shell
Nail is fixed in frame 3, and undercarriage 4 is fixed by snap in frame 3, and display screen 6 is glued on base 8, and controlling switch 7 is logical
Cross neck to be fixed on base 8, lithium battery 11 is fixed in base 8 by neck, and charging circuit 13 is fixed by snap in lithium
On battery 11, coulometric detector 14 is fixed by snap on lithium battery 11, and control main frame 12 is fixed on base 8 by neck
Interior, in frame 3, electric machine stand 10 is fixed by screws in mounting seat 5 welding of mounting seat 5, and the quantity of servomotor 9 is four
Individual, servomotor 9 is fixed by screws on electric machine stand 10, and rotating shaft 2 is connected with servomotor 9 by shaft coupling, blade 1
Material is zirconium oxide, and blade 1 is threadedly secured in rotating shaft 2, and solar energy film plate 15 is glued on blade 1, reinforcement 16
Material be potassium steel, reinforcement 16 is embedded in blade 1, control main frame 12 and charging circuit 13, lithium battery 11, electric power detection
Device 14, servomotor 9, display screen 6 are connected with controlling switch 7 by wire.
The basic principles, principal features and advantages of the present invention have been shown and described above.The technical staff of the industry should
Understand, the present invention is not limited to the above embodiments, the original for simply illustrating the present invention described in above-described embodiment and specification
Reason, without departing from the spirit and scope of the present invention, various changes and modifications of the present invention are possible, these changes and improvements
It all fall within the protetion scope of the claimed invention.The claimed scope of the invention is by appended claims and its Xiao Wu circle
It is fixed.
Claims (7)
- A kind of 1. new unmanned plane with drop resistant abrasion-resistant blade, it is characterised in that：It is described including frame, base and undercarriage Body bottom surface is provided with the base, and the base both sides are provided with the undercarriage, and the susceptor surface is provided with display screen, The display screen side is provided with controlling switch, and the chassis interior bottom surface is provided with lithium battery, is provided with the lithium battery Charging circuit, the charging circuit side are provided with coulometric detector, and the lithium battery side is provided with control main frame, the machine Frame peripheral end set has mounting seat, and the mounting seat inner bottom surface is provided with electric machine stand, is provided with the electric machine stand Servomotor, the servomotor end set have rotating shaft, and the roller end is provided with blade, and the blade surface is provided with Solar energy film plate, the blade interior are provided with reinforcement.
- A kind of 2. new unmanned plane with drop resistant abrasion-resistant blade according to claim 1, it is characterised in that：The base It is fixed by screws in the frame, the undercarriage is fixed by snap in the frame, and the display screen is glued to On the base.
- A kind of 3. new unmanned plane with drop resistant abrasion-resistant blade according to claim 1, it is characterised in that：The control Switch is fixed on the base by neck, and the lithium battery is fixed in the base by neck, the charging circuit It is fixed by snap on the lithium battery, the coulometric detector is fixed by snap on the lithium battery.
- A kind of 4. new unmanned plane with drop resistant abrasion-resistant blade according to claim 1, it is characterised in that：The control Main frame is fixed in the base by neck, and in the frame, the electric machine stand passes through screw for the mounting seat welding It is fixed in the mounting seat, the quantity of the servomotor is four, and the servomotor is fixed by screws in the electricity On machine support.
- A kind of 5. new unmanned plane with drop resistant abrasion-resistant blade according to claim 1, it is characterised in that：The rotating shaft It is connected with the servomotor by shaft coupling, the material of the blade is zirconium oxide, and the blade is threadedly secured to institute State in rotating shaft.
- A kind of 6. new unmanned plane with drop resistant abrasion-resistant blade according to claim 1, it is characterised in that：The sun Energy thin web is glued on the blade, and the material of the reinforcement is potassium steel, and the reinforcement is embedded in the blade.
- A kind of 7. new unmanned plane with drop resistant abrasion-resistant blade according to claim 1, it is characterised in that：The control Main frame and the charging circuit, the lithium battery, the coulometric detector, the servomotor, the display screen and the control System switch is connected by wire.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710610952.9A CN107444628A (en) | 2017-07-25 | 2017-07-25 | A kind of new unmanned plane with drop resistant abrasion-resistant blade |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710610952.9A CN107444628A (en) | 2017-07-25 | 2017-07-25 | A kind of new unmanned plane with drop resistant abrasion-resistant blade |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107444628A true CN107444628A (en) | 2017-12-08 |
Family
ID=60487606
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710610952.9A Pending CN107444628A (en) | 2017-07-25 | 2017-07-25 | A kind of new unmanned plane with drop resistant abrasion-resistant blade |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107444628A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2006142884A (en) * | 2004-11-16 | 2006-06-08 | Seiko Epson Corp | Flying body |
| CN101013732A (en) * | 2007-01-31 | 2007-08-08 | 黄上立 | Spinned deployable thin film solar battery array and its application in space |
| CN103832591A (en) * | 2012-11-28 | 2014-06-04 | 陈昌志 | Multifunctional new energy airplane |
| CN104401486A (en) * | 2014-11-21 | 2015-03-11 | 吉林大学 | Solar aircraft |
| CN106043673A (en) * | 2016-08-12 | 2016-10-26 | 成都恒胜达科技有限公司 | Unmanned plane landing in random terrain |
| CN205872440U (en) * | 2016-06-08 | 2017-01-11 | 天津市瑞傲特科技发展有限公司 | Screw for unmanned aerial vehicle |
-
2017
- 2017-07-25 CN CN201710610952.9A patent/CN107444628A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2006142884A (en) * | 2004-11-16 | 2006-06-08 | Seiko Epson Corp | Flying body |
| CN101013732A (en) * | 2007-01-31 | 2007-08-08 | 黄上立 | Spinned deployable thin film solar battery array and its application in space |
| CN103832591A (en) * | 2012-11-28 | 2014-06-04 | 陈昌志 | Multifunctional new energy airplane |
| CN104401486A (en) * | 2014-11-21 | 2015-03-11 | 吉林大学 | Solar aircraft |
| CN205872440U (en) * | 2016-06-08 | 2017-01-11 | 天津市瑞傲特科技发展有限公司 | Screw for unmanned aerial vehicle |
| CN106043673A (en) * | 2016-08-12 | 2016-10-26 | 成都恒胜达科技有限公司 | Unmanned plane landing in random terrain |
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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: 20171208 |
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| RJ01 | Rejection of invention patent application after publication |