CN106394879A - Application of resistance braking device with battery charging buffered and energy saved - Google Patents
Application of resistance braking device with battery charging buffered and energy saved Download PDFInfo
- Publication number
- CN106394879A CN106394879A CN201610908941.4A CN201610908941A CN106394879A CN 106394879 A CN106394879 A CN 106394879A CN 201610908941 A CN201610908941 A CN 201610908941A CN 106394879 A CN106394879 A CN 106394879A
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- CN
- China
- Prior art keywords
- landing gear
- main landing
- cable
- power supply
- connects
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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
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/42—Arrangement or adaptation of brakes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION 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
- B60L7/00—Electrodynamic brake systems for vehicles in general
- B60L7/10—Dynamic electric regenerative braking
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION 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
- B60L2200/00—Type of vehicles
- B60L2200/10—Air crafts
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Power Engineering (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Valves And Accessory Devices For Braking Systems (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
Abstract
The invention discloses application of a resistance braking device with battery charging buffered and energy saved, and relates to the technical field of application of buffering electricity energy conversion. A distribution box is connected to an electronic equipment compartment through a control cable; the distribution box is connected to a power supply cable, and the power supply cable is connected to a storage battery set; and the distribution box is connected to the power supply cable, the power supply cable is provided with a super capacitor, and the power supply cable is connected to the storage battery set through the super capacitor. The device is characterized in that when an aircraft is landed at the airport, enters a taxiway and slides, main landing gear aircraft wheels drive gears inside gear boxes to rotate through main landing gear wheel axles; the gears transmit the kinetic energy to electro-motors, the electro-motors convert the kinetic energy into the electric energy, the electric energy is transmitted to the super capacitor through the power supply cable and then transmitted to the storage battery set to be stored through the super capacitor, and the stored electric energy can be provided for the aircraft; and when the aircraft takes off, the electro-motors can select power sources according to the power supply priority of the aircraft, and a branch cable has the power supply effect and can supply power to the aircraft.
Description
Technical field
The application of buffering charging energy-conservation resistance braking device, is related to braking equipment applied technical field.
Background technology
With the fast development of information industry, travel industry, the transport service being adapted therewith is also in fast development.Trip,
The speed of logistics all occurs to change with rapid changepl. never-ending changes and improvements, and the radius of action of people is increasing, the scope of logistics
More and more wider.Air-transport industry quickly grows, and in recent years for domestic, constantly expands newly-increased course line, expands airport.
Airborne vehicle on ground or takes off or lands different from automobile, (the wheel and attached of drop during aircraft lands
Mechanism), then with airborne vehicle engine (turbofan, if will be bigger using turbojet oil consumption) for power
Slide into airplane parking area, therefore oil consumption big (particularly oil consumption is especially huge when airborne vehicle low speed is moved below 80 section), noise big,
Easily Foreign body aspiration causes fault, and walking about if there are personnel also has the danger being inhaled into.As " aerial liner of numbering AI619, at that time
To fly to Hyderabad from Mumbai, because signal is got in airborne vehicle copilot wrong, when starting engine, a ground crew is inhaled
Enter in engine.”
Ground installation related to shipping increasingly highlights and develops rapidly the incompatible of shipping.
Content of the invention
Airborne vehicle is required to when taking off or land slide.The flight frequency of increasingly increase takies taxiway so that many
Airport has to extend increases taxiway.Increase airport construction expense, ground maintenance expense.
For overcoming the shortcomings of prior art presence：
One of purpose of the application is to reduce the ground run distance of airborne vehicle；
Braking under abnormal condition for the two extra increases of the purpose of the application；
The three of the purpose of the application are the safeties improving airborne vehicle landing and sliding race stage.
The four of the purpose of the application are save energies.
The application adopts the following technical scheme that for achieving the above object：
First, buffer charging energy-conservation resistance braking device
1st, buffer charging energy-conservation resistance braking device, including：Gear-box 1, branch cable 4, junction box 5, motor 8, axle
Hold case 11, main landing gear wheel shaft 12, main landing gear wheel 13, main landing gear crane span structure 14, main unit of landing gear 16, electronics bay
91st, cable 92, service cable 93, super capacitor 94, accumulator battery 95 are controlled；
It is characterized in that：
Main landing gear is symmetrical parallel two group, and every group of main landing gear is equipped with four duplicate main landing gear wheels
13, before two main landing gear wheels and two main landing gear wheels below；
It is connected with gear-box 1, gear-box 1 connects main landing gear wheel shaft 12, bearing housing 11 is even inside main landing gear below
Connect main landing gear wheel shaft 12, main landing gear wheel shaft 12 connects main landing gear wheel 13；
Motor 8 connects branch cable 4, and branch cable 4 connects junction box 5；Junction box 5 passes through to control cable 92 to be connected to
Electronics bay 91；
Junction box 5 connects service cable 93, and equipped with super capacitor 94 on service cable 93, service cable 93 passes through super electricity
Hold 94 connection accumulator batteries 95.
2nd, described buffering charging energy-conservation resistance braking device it is characterised in that：Described, accumulator battery is ni-mh electric power storage
Pond group.
3rd, described buffering charging energy-conservation resistance braking device it is characterised in that：Described accumulator battery is lithium-ion electric
Pond group.
4th, described buffering charging energy-conservation resistance braking device it is characterised in that：Described junction box is can be at minus 85 DEG C
Junction box to 55 DEG C of environmental works.
5th, described buffering charging energy-conservation resistance braking device it is characterised in that：Described motor 8 is direct current drive
Machine.
2nd, buffer the application of charging energy-conservation resistance braking device
1st, buffer the application of charging energy-conservation resistance braking device, buffering charging energy-conservation resistance braking device includes：Gear-box
1st, branch cable 4, junction box 5, motor 8, bearing housing 11, main landing gear wheel shaft 12, main landing gear wheel 13, main landing gear bridge
Frame 14, main unit of landing gear 16, electronics bay 91, control cable 92, service cable 93, accumulator battery 95；
Main landing gear is symmetrical parallel two group, and every group of main landing gear is equipped with four duplicate main landing gear wheels
13, before two main landing gear wheels and two main landing gear wheels below；
It is connected with gear-box 1, gear-box 1 connects main landing gear wheel shaft 12, bearing housing 11 is even inside main landing gear below
Connect main landing gear wheel shaft 12, main landing gear wheel shaft 12 connects main landing gear wheel 13；
Motor 8 connects branch cable 4, and branch cable 4 connects junction box 5；Junction box 5 passes through to control cable 92 to be connected to
Electronics bay 91；
Junction box 5 connects service cable 93, and equipped with super capacitor 94 on service cable 93, service cable 93 passes through super electricity
Hold 94 connection accumulator batteries 95；
It is characterized in that：
When airborne vehicle lands on the airport, when entrance taxiway slides, main landing gear wheel 13 passes through main landing gear wheel shaft 12
Drive the pinion rotation in gear-box 1；
Kinetic energy is passed to motor 8 by gear, and motor 8 converts kinetic energy into electric energy, by service cable 93 by electric energy
Reach super capacitor 94, then accumulator battery 95 is reached by super capacitor 94 and store, the electric energy of storage can be powered for airborne vehicle.
The application of the 2nd, described buffering charging energy-conservation resistance braking device it is characterised in that：When aircraft takeoff, electronic
Machine 8 can select power supply according to the power supply priority of airborne vehicle, and branch cable 4 has power supply function.
Beneficial effect
1st, because " motor 8 connects branch cable 4, and branch cable 4 connects junction box 5 ... ... junction box 5 and connects power supply
Cable 93, service cable 93 connects accumulator battery 95 " ground run distance of airborne vehicle can be reduced；
2nd, because " motor 8 connects branch cable 4, and branch cable 4 connects junction box 5 ... ... junction box 5 and connects power supply
Cable 93, service cable 93 connect accumulator battery 95 " can effectively utilize aircraft slide power be accumulator battery electric power storage, section
The about energy；
3rd, the application can additionally increase the braking under abnormal condition, if the one of which brake fault when airborne vehicle
When, the buffering charging energy-conservation resistance braking device of the application can use as a kind of standby brake unit；
4th, " equipped with super capacitor 94 on service cable 93, service cable 93 connects accumulator battery 95 by super capacitor 94 "
Accumulator can be made to rush electric protection accumulator, improve service life；
5th, improve the safety of airborne vehicle landing phases, the particularly safety in the improper landing of airborne vehicle, example
As when the brake gear of prior art is unavailable, the present invention, as a kind of independent system, can work independently and realize aviation
The braking of device landing ground taxi.
6th, due to increased motor 8, when airborne vehicle is in ground motion, electromotor can be substituted and push away for airborne vehicle offer
Power
7th, due to the invention enables airborne vehicle can drive airborne vehicle by motor 8, driving compared with the engine type of prior art
Move and can greatly save Aviation Fuel.
8th, due to the invention enables airborne vehicle can drive airborne vehicle by motor 8, driving compared with the engine type of prior art
The dynamic probability that can reduce noise, mitigate discharge, prevent the accident generation that engine is hurted sb.'s feelings.
Brief description
Fig. 1：Buffering charging energy-conservation resistance braking device and aircraft position diagrammatic side view
Fig. 2：Buffering charging energy-conservation resistance braking device and aircraft position diagrammatic top view
Fig. 3：Buffering charging energy-conservation resistance braking device side view
Fig. 4：A-A view
In figure：1 gear-box, 4 branch cables, 5 junction boxs, 8 motor, 11 bearing housings, 12 main landing gear wheel shafts, 13 lead
Fall frame wheel, 14 main landing gear crane span structures, 16 main unit of landing gears, 91 electronics bays, 92 control cables, 93 service cables, 94
Super capacitor, 95 accumulator batteries.
Specific embodiment
With reference to the accompanying drawings and examples the application is described further.
Embodiment 1
1st, buffer charging energy-conservation resistance braking device, including：Gear-box 1, branch cable 4, junction box 5, motor 8, axle
Hold case 11, main landing gear wheel shaft 12, main landing gear wheel 13, main landing gear crane span structure 14, main unit of landing gear 16, electronics bay
91st, cable 92, service cable 93, super capacitor 94, accumulator battery 95 are controlled；
It is characterized in that：
Main landing gear is symmetrical parallel two group, and every group of main landing gear is equipped with four duplicate main landing gear wheels
13, before two main landing gear wheels and two main landing gear wheels below；
It is connected with gear-box 1, gear-box 1 connects main landing gear wheel shaft 12, bearing housing 11 is even inside main landing gear below
Connect main landing gear wheel shaft 12, main landing gear wheel shaft 12 connects main landing gear wheel 13；
Motor 8 connects branch cable 4, and branch cable 4 connects junction box 5；Junction box 5 passes through to control cable 92 to be connected to
Electronics bay 91；
Junction box 5 connects service cable 93, and equipped with super capacitor 94 on service cable 93, service cable 93 passes through super electricity
Hold 94 connection accumulator batteries 95.
2nd, described buffering charging energy-conservation resistance braking device it is characterised in that：Described, accumulator battery is ni-mh electric power storage
Pond group.
3rd, described buffering charging energy-conservation resistance braking device it is characterised in that：Described accumulator battery is lithium-ion electric
Pond group.
4th, described buffering charging energy-conservation resistance braking device it is characterised in that：Described junction box is can be at minus 85 DEG C
Junction box to 55 DEG C of environmental works.
5th, described buffering charging energy-conservation resistance braking device it is characterised in that：Described motor 8 is direct current drive
Machine.
Embodiment 2
1st, buffer the application of charging energy-conservation resistance braking device, buffering charging energy-conservation resistance braking device includes：Gear-box
1st, branch cable 4, junction box 5, motor 8, bearing housing 11, main landing gear wheel shaft 12, main landing gear wheel 13, main landing gear bridge
Frame 14, main unit of landing gear 16, electronics bay 91, control cable 92, service cable 93, accumulator battery 95；
Main landing gear is symmetrical parallel two group, and every group of main landing gear is equipped with four duplicate main landing gear wheels
13, before two main landing gear wheels and two main landing gear wheels below；
It is connected with gear-box 1, gear-box 1 connects main landing gear wheel shaft 12, bearing housing 11 is even inside main landing gear below
Connect main landing gear wheel shaft 12, main landing gear wheel shaft 12 connects main landing gear wheel 13；
Motor 8 connects branch cable 4, and branch cable 4 connects junction box 5；Junction box 5 passes through to control cable 92 to be connected to
Electronics bay 91；
Junction box 5 connects service cable 93, and equipped with super capacitor 94 on service cable 93, service cable 93 passes through super electricity
Hold 94 connection accumulator batteries 95；
It is characterized in that：
When airborne vehicle lands on the airport, when entrance taxiway slides, main landing gear wheel 13 passes through main landing gear wheel shaft 12
Drive the pinion rotation in gear-box 1；
Kinetic energy is passed to motor 8 by gear, and motor 8 converts kinetic energy into electric energy, by service cable 93 by electric energy
Reach super capacitor 94, then accumulator battery 95 is reached by super capacitor 94 and store, the electric energy of storage can be powered for airborne vehicle.
The application of the 2nd, described buffering charging energy-conservation resistance braking device it is characterised in that：When aircraft takeoff, electronic
Machine 8 can select power supply according to the power supply priority of airborne vehicle, and branch cable 4 has power supply function.
In addition to technical characteristic described herein, remaining is knowledge known to one of ordinary skill in the art, and here does not exist
Repeat.
Claims (2)
1. buffer the application of charging energy-conservation resistance braking device, buffering charging energy-conservation resistance braking device includes：Gear-box, branch
Cable, junction box, motor, bearing housing, main landing gear wheel shaft, main landing gear wheel, main landing gear crane span structure, main landing gear prop up
Post, electronics bay, control cable, service cable, super capacitor, accumulator battery；
Main landing gear is symmetrical parallel two group, every group of main landing gear equipped with four duplicate main landing gear wheels, before
Two main landing gear wheels and below two main landing gear wheels；
It is connected with gear-box, gear-box connects main landing gear wheel shaft, bearing housing connects main landing gear inside main landing gear below
Wheel shaft, main landing gear wheel shaft connects main landing gear wheel；
Motor connects branch cable, and branch cable connects junction box；Junction box passes through to control cable connection to electronics bay；
Junction box connects service cable, and service cable connects accumulator battery；
Junction box connects service cable, and equipped with super capacitor on service cable, service cable connects accumulator by super capacitor
Group；
It is characterized in that：
When airborne vehicle lands on the airport, when entrance taxiway slides, main landing gear wheel passes through main gear wheels shaft driven gear
Pinion rotation in case；
Kinetic energy is passed to motor by gear, and motor converts kinetic energy into electric energy, is reached electric energy by service cable super
Electric capacity, then accumulator battery storage is reached by super capacitor, the electric energy of storage can be powered for airborne vehicle.
2. as claimed in claim 1 buffering charging energy-conservation resistance braking device application it is characterised in that：Work as aircraft takeoff
When, motor can select power supply according to the power supply priority of airborne vehicle, and branch cable has power supply function, is that airborne vehicle is powered.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610908941.4A CN106394879A (en) | 2016-10-18 | 2016-10-18 | Application of resistance braking device with battery charging buffered and energy saved |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610908941.4A CN106394879A (en) | 2016-10-18 | 2016-10-18 | Application of resistance braking device with battery charging buffered and energy saved |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106394879A true CN106394879A (en) | 2017-02-15 |
Family
ID=58012288
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610908941.4A Pending CN106394879A (en) | 2016-10-18 | 2016-10-18 | Application of resistance braking device with battery charging buffered and energy saved |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106394879A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB764788A (en) * | 1954-08-24 | 1957-01-02 | Goodyear Tire & Rubber | Electrical anti-skid mechanism for brakes |
| US20070284939A1 (en) * | 2006-06-12 | 2007-12-13 | Honeywell International | Aircraft electric brake and generator therefor |
| CN102139695A (en) * | 2011-03-02 | 2011-08-03 | 天津市松正电动汽车技术股份有限公司 | Energy management system for electric automobile and management method therefor |
| US20110198439A1 (en) * | 2008-07-07 | 2011-08-18 | Airbus Operations Gmbh | Wheel drive system for an aircraft comprising a fuel cell as an energy source |
| CN103847959A (en) * | 2014-03-22 | 2014-06-11 | 中国科学院电工研究所 | Aircraft braking energy recovery system based on flywheel energy storage |
| US9017219B2 (en) * | 2012-05-03 | 2015-04-28 | Goodrich Corporation | Systems and methods for aircraft braking and taxiing |
-
2016
- 2016-10-18 CN CN201610908941.4A patent/CN106394879A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB764788A (en) * | 1954-08-24 | 1957-01-02 | Goodyear Tire & Rubber | Electrical anti-skid mechanism for brakes |
| US20070284939A1 (en) * | 2006-06-12 | 2007-12-13 | Honeywell International | Aircraft electric brake and generator therefor |
| US20110198439A1 (en) * | 2008-07-07 | 2011-08-18 | Airbus Operations Gmbh | Wheel drive system for an aircraft comprising a fuel cell as an energy source |
| CN102139695A (en) * | 2011-03-02 | 2011-08-03 | 天津市松正电动汽车技术股份有限公司 | Energy management system for electric automobile and management method therefor |
| US9017219B2 (en) * | 2012-05-03 | 2015-04-28 | Goodrich Corporation | Systems and methods for aircraft braking and taxiing |
| CN103847959A (en) * | 2014-03-22 | 2014-06-11 | 中国科学院电工研究所 | Aircraft braking energy recovery system based on flywheel energy storage |
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| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
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| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170215 |
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| WD01 | Invention patent application deemed withdrawn after publication |