CN108657240A - A kind of helicopter multifunctional redundant electrical power - Google Patents

A kind of helicopter multifunctional redundant electrical power Download PDF

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Publication number
CN108657240A
CN108657240A CN201810823716.XA CN201810823716A CN108657240A CN 108657240 A CN108657240 A CN 108657240A CN 201810823716 A CN201810823716 A CN 201810823716A CN 108657240 A CN108657240 A CN 108657240A
Authority
CN
China
Prior art keywords
wall
installing frame
helicopter
hinged
reel
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.)
Withdrawn
Application number
CN201810823716.XA
Other languages
Chinese (zh)
Inventor
何伟
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
XIANGYANG SANPENG AVIATION SCIENCE & TECHNOLOGY Co Ltd
Original Assignee
XIANGYANG SANPENG AVIATION SCIENCE & TECHNOLOGY Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by XIANGYANG SANPENG AVIATION SCIENCE & TECHNOLOGY Co Ltd filed Critical XIANGYANG SANPENG AVIATION SCIENCE & TECHNOLOGY Co Ltd
Priority to CN201810823716.XA priority Critical patent/CN108657240A/en
Publication of CN108657240A publication Critical patent/CN108657240A/en
Withdrawn legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62BHAND-PROPELLED VEHICLES, e.g. HAND CARTS OR PERAMBULATORS; SLEDGES
    • B62B1/00Hand carts having only one axis carrying one or more transport wheels; Equipment therefor
    • B62B1/10Hand carts having only one axis carrying one or more transport wheels; Equipment therefor in which the load is intended to be transferred totally to the wheels
    • B62B1/12Hand carts having only one axis carrying one or more transport wheels; Equipment therefor in which the load is intended to be transferred totally to the wheels involving parts being adjustable, collapsible, attachable, detachable, or convertible
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L53/00Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/10Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
    • B60L53/14Conductive energy transfer
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F21LIGHTING
    • F21VFUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
    • F21V33/00Structural combinations of lighting devices with other articles, not otherwise provided for
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02SGENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
    • H02S20/00Supporting structures for PV modules
    • H02S20/30Supporting structures being movable or adjustable, e.g. for angle adjustment
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2200/00Type of vehicles
    • B60L2200/10Air crafts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62BHAND-PROPELLED VEHICLES, e.g. HAND CARTS OR PERAMBULATORS; SLEDGES
    • B62B2202/00Indexing codes relating to type or characteristics of transported articles
    • B62B2202/61Batteries
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/50Photovoltaic [PV] energy
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/60Other road transportation technologies with climate change mitigation effect
    • Y02T10/70Energy storage systems for electromobility, e.g. batteries
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/60Other road transportation technologies with climate change mitigation effect
    • Y02T10/7072Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/10Technologies relating to charging of electric vehicles
    • Y02T90/14Plug-in electric vehicles

Landscapes

  • Engineering & Computer Science (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Photovoltaic Devices (AREA)

Abstract

The invention discloses a kind of helicopter multifunctional redundant electrical powers, including installing frame, the installing frame inner wall bottom position is connected with reel, described reel one end has been bolted the first drive plate across installing frame side outer wall, the installing frame both sides outer wall bottom position is connected with wheel, one of wheel is equipped with the second drive plate close to installing frame side outer wall, and first drive plate and the second drive plate pass through transmission belt and form transmission cooperation, the installing frame inner wall has been bolted arc-shaped cover at reel position, the installing frame inner wall has been bolted battery case at arc-shaped cover apical position.The present invention is convenient to wind cable, easy to operate, enriches the function of redundant electrical power, is conducive to improve working efficiency, reel can be driven to rotate, more laborsaving, facilitates carrying, is conducive to improve generating effect, is suitble to use under emergency case.

Description

A kind of helicopter multifunctional redundant electrical power
Technical field
The present invention relates to redundant electrical power technical field more particularly to a kind of helicopter multifunctional redundant electrical powers.
Background technology
The helicopter creation one of very characteristic as 20th century aeronautical technology, greatly expand aircraft applies model It encloses.Helicopter is typical dual-use product, can be widely applied to the multiple fields such as transport, patrol, tourism, rescue.
Scooter 300km/h the or more when maximum of helicopter, the nearly 400km/h of underriding limit velocity, practical ceiling are reachable 6000 meters (world record 12450m), general voyage is up to 600~800km or so.The inside and outside auxiliary fuel tank ferry range of portable machine Up to 2000km or more.Helicopter is needed to have different take-off weights according to different.The heavy type to come into operation on our times It is the rice -26 of Russia that helicopter is maximum (maximum take-off weight reaches 56t, payload 20t).Currently practical application is machine The single-rotor helicopter and twin-rotor helicopter of tool drive-type, wherein again most with single-rotor helicopter quantity.Helicopter needs Redundant electrical power is used, assistant starting, existing redundant electrical power function power supply are carried out, it has not been convenient to retractable cable, so existing propose one kind Helicopter multifunctional redundant electrical power.
Invention content
Technical problems based on background technology, the present invention propose a kind of helicopter multifunctional redundant electrical power.
A kind of helicopter multifunctional redundant electrical power proposed by the present invention, including installing frame, installing frame inner wall bottom end position It sets and is connected with reel, described reel one end has been bolted the first drive plate across installing frame side outer wall, The installing frame both sides outer wall bottom position is connected with wheel, and one of wheel is equipped with close to installing frame side outer wall Second drive plate, and the first drive plate and the second drive plate form transmission cooperation by transmission belt, the installing frame inner wall is close Arc-shaped cover is bolted at reel position, the installing frame inner wall is solid by bolt at arc-shaped cover apical position Surely there is battery case, and battery chamber interior wall is connected with lithium-cell plate, battery case side outer wall is hinged with solar panel, institute It states solar panel both sides outer wall and is hinged with the first damping telescopic bar, and two the first damping telescopic bars are far from solar-electricity Pond plate one end is hinged with battery case both sides outer wall respectively, and battery case top outer wall has been bolted hinged seat, and cuts with scissors Joint chair inner wall is hinged with headlamp, and the installing frame is hinged with holder, the holder two far from solar panel side outer wall Side outer wall is hinged with the second damping telescopic bar, and two the second damping telescopic bars far from holder one end respectively with installing frame both sides Outer wall is hinged.
Preferably, the installing frame top is welded with handle frame, and handle frame side wall is provided with non-slip texture.
Preferably, the reel inner wall is around having a cable, and reel one end is equipped with rotation electric contact, cable one end with Electric contact connection is rotated, rotation electric contact is connect by conducting wire with lithium-cell plate.
Preferably, the solar panel is connected with inverter, and inverter is connect with lithium-cell plate.
Preferably, the headlamp is connected with switch, and switch is connected with microprocessor.
Preferably, the rack inner wall has been bolted kit bag.
Advantageous effect in the present invention:
1, convenient that cable is wound by the reel of installation, it is easy to operate, the function of redundant electrical power is enriched, is had Conducive to working efficiency is improved, coordinates the wheel, the second drive plate and the first drive plate of installation, reel can be driven to rotate, more Add laborsaving, facilitates carrying.
2, by the solar panel of installation, coordinate the first damping telescopic bar and holder, facilitate adjusting, can adjust too Positive energy solar panel is conducive to improve generating effect to suitable position, is suitble to use under emergency case.
Description of the drawings
Fig. 1 is a kind of structural schematic diagram of helicopter multifunctional redundant electrical power proposed by the present invention;
Fig. 2 is a kind of structural schematic diagram of helicopter multifunctional redundant electrical power holder proposed by the present invention.
In figure:1 wheel, 2 first drive plates, 3 arc-shaped covers, 4 cables, 5 first damping telescopic bars, 6 solar panels, 7 Battery case, 8 headlamps, 9 hinged seats, 10 handle frames, 11 second damping telescopic bars, 12 holders, 13 reels, 14 installing frames, 15 Kit bag.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.
Referring to Fig.1-2, a kind of helicopter multifunctional redundant electrical power, including installing frame 14,14 inner wall bottom position of installing frame It is connected with reel 13,13 one end of reel has been bolted the first drive plate 2 across 14 side outer wall of installing frame, 14 both sides outer wall bottom position of installing frame is connected with wheel 1, and one of wheel 1 is set close to 14 side outer wall of installing frame There is the second drive plate, and the first drive plate and the second drive plate form transmission cooperation by transmission belt, 14 inner wall of installing frame is close Arc-shaped cover 3 is bolted at 13 position of reel, 14 inner wall of installing frame passes through bolt at 3 apical position of arc-shaped cover It being fixed with battery case 7, and 7 inner wall of battery case is connected with lithium-cell plate, 7 side outer wall of battery case is hinged with solar panel 6, 6 both sides outer wall of solar panel is hinged with the first damping telescopic bar 5, and two the first damping telescopic bars 5 are far from solar energy 6 one end of solar panel is hinged with 7 both sides outer wall of battery case respectively, and 7 top outer wall of battery case has been bolted hinged seat 9, and 9 inner wall of hinged seat is hinged with headlamp 8, and installing frame 14 is hinged with holder 12, holder 12 far from 6 side outer wall of solar panel Both sides outer wall is hinged with the second damping telescopic bar 11, and two the second damping telescopic bars 11 far from 12 one end of holder respectively with peace The 14 both sides outer walls that frame up are hinged.
In the present invention, 14 top of installing frame is welded with handle frame 10, and 10 side wall of handle frame is provided with non-slip texture, reel 13 inner walls are around having a cable 4, and 13 one end of reel is equipped with rotation electric contact, and 4 one end of cable is connect with rotation electric contact, rotation Electric contact is connect by conducting wire with lithium-cell plate, and solar panel 6 is connected with inverter, and inverter is connect with lithium-cell plate, Headlamp 8 is connected with switch, and switch is connected with microprocessor, and microprocessor model is ARM9TDMI, and 12 inner wall of holder passes through bolt It is fixed with kit bag 15.
In use, in the case where two wheels 1 coordinate, by holding handle frame 10, dragging redundant electrical power is to suitable position, then Holder 12 is unfolded under the cooperation of two the second damping telescopic bars 11 to proper angle, redundant electrical power is supported, cable is taken out 4, helicopter is powered, power supply terminates, and removes cable 4, by pushing redundant electrical power, wheel 1 to rotate, drives reel 13 Winding to cable 4 is realized in rotation, and deploying solar energy solar panel 6 is to suitable angular under the action of two the first damping telescopic bars 5 Degree, generates electricity, by adjusting illuminating lamp 8 to proper angle, can be illuminated.
The foregoing is only a preferred embodiment of the present invention, but scope of protection of the present invention is not limited thereto, Any one skilled in the art in the technical scope disclosed by the present invention, according to the technique and scheme of the present invention and its Inventive concept is subject to equivalent substitution or change, should be covered by the protection scope of the present invention.

Claims (6)

1. a kind of helicopter multifunctional redundant electrical power, including installing frame (14), which is characterized in that installing frame (14) the inner wall bottom End position is connected with reel (13), and described reel (13) one end passes through installing frame (14) side outer wall solid by bolt There are the first drive plate (2), installing frame (14) both sides outer wall bottom position to be connected with wheel (1) surely, one of them Wheel (1) is equipped with the second drive plate close to installing frame (14) side outer wall, and the first drive plate and the second drive plate pass through transmission Band forms transmission cooperation, and installing frame (14) inner wall has been bolted arc-shaped cover (3) at reel (13) position, Installing frame (14) inner wall has been bolted battery case (7), and battery case (7) at arc-shaped cover (3) apical position Inner wall is connected with lithium-cell plate, and battery case (7) side outer wall is hinged with solar panel (6), the solar cell Plate (6) both sides outer wall is hinged with the first damping telescopic bar (5), and two the first damping telescopic bars (5) are far from solar cell Plate (6) one end is hinged with battery case (7) both sides outer wall respectively, and battery case (7) top outer wall has been bolted hinged Seat (9), and hinged seat (9) inner wall is hinged with headlamp (8), the installing frame (14) is far from outside solar panel (6) side Wall is hinged with holder (12), and holder (12) both sides outer wall is hinged with the second damping telescopic bar (11), and two second resistances Buddhist nun's telescopic rod (11) is hinged with installing frame (14) both sides outer wall respectively far from holder (12) one end.
2. a kind of helicopter multifunctional redundant electrical power according to claim 1, which is characterized in that installing frame (14) top End is welded with handle frame (10), and handle frame (10) side wall is provided with non-slip texture.
3. a kind of helicopter multifunctional redundant electrical power according to claim 1, which is characterized in that in the reel (13) Wall is around having a cable (4), and reel (13) one end is equipped with rotation electric contact, and cable (4) one end is connect with rotation electric contact, rotation Switching dateline is connect by conducting wire with lithium-cell plate.
4. a kind of helicopter multifunctional redundant electrical power according to claim 1, which is characterized in that the solar panel (6) it is connected with inverter, and inverter is connect with lithium-cell plate.
5. a kind of helicopter multifunctional redundant electrical power according to claim 1, which is characterized in that the headlamp (8) is even There is switch, and switch is connected with microprocessor.
6. a kind of helicopter multifunctional redundant electrical power according to claim 1, which is characterized in that holder (12) inner wall It has been bolted kit bag (15).
CN201810823716.XA 2018-07-25 2018-07-25 A kind of helicopter multifunctional redundant electrical power Withdrawn CN108657240A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810823716.XA CN108657240A (en) 2018-07-25 2018-07-25 A kind of helicopter multifunctional redundant electrical power

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810823716.XA CN108657240A (en) 2018-07-25 2018-07-25 A kind of helicopter multifunctional redundant electrical power

Publications (1)

Publication Number Publication Date
CN108657240A true CN108657240A (en) 2018-10-16

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Family Applications (1)

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CN201810823716.XA Withdrawn CN108657240A (en) 2018-07-25 2018-07-25 A kind of helicopter multifunctional redundant electrical power

Country Status (1)

Country Link
CN (1) CN108657240A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111404223A (en) * 2020-03-25 2020-07-10 赛特立科技有限公司 Lithium battery mobile power supply

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111404223A (en) * 2020-03-25 2020-07-10 赛特立科技有限公司 Lithium battery mobile power supply

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WW01 Invention patent application withdrawn after publication
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Application publication date: 20181016