CN104058091A - New scheme for airplane braking - Google Patents
New scheme for airplane braking Download PDFInfo
- Publication number
- CN104058091A CN104058091A CN201310086083.6A CN201310086083A CN104058091A CN 104058091 A CN104058091 A CN 104058091A CN 201310086083 A CN201310086083 A CN 201310086083A CN 104058091 A CN104058091 A CN 104058091A
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- CN
- China
- Prior art keywords
- braking
- aircraft
- airplane
- new scheme
- motor
- 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
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- Braking Arrangements (AREA)
- Regulating Braking Force (AREA)
- Braking Systems And Boosters (AREA)
Abstract
The invention relates to a new scheme for airplane braking. A motor is mounted in a tail wheel of an airplane and is used for emergency braking. During braking, power generated by the motor is delivered to a battery of the airplane.
Description
Technical field
Patent aircraft braking new departure of the present invention, relates to a kind of category of transforming aircraft manufacturing.
Background technology
At present, the aircraft that countries in the world produce, all is not equipped with the facility of emergency braking " machine of stopping ", while causing and have the event that aircraft guns off the runway to occur, causes many human world tragedy! Follow its reason, be exactly, aviator, dare not suddenly step on " machine of stopping " and carry out emergency braking, otherwise very easily somersaults of aircraft causes blast, fatal crass's miserable consequence!
Summary of the invention
This invention, be to seem impossible mistaken ideas in order to overcome this, the function of being stopped machine, be placed on the trailing wheel of aircraft, when aircraft nose wheel is at the beginning when kiss the earth, at once the rear wing flap on wing up turned over, also make the rear wing flap of horizontal tail vane stick up upward, now stepping on the machine of stopping just can be harmless simultaneously.Because what installed tail wheel the inside is motor, electricity consumption is braked.The electricity sending when its braking, feeds back in the battery in body.
Have again, if patent of invention of aircraft process employing " improvement project of aircraft tail vane design " (patent No. is: method 201210042518.2), improve vertical tail vane, and it is perfectly safe more can to protect.
Brief description of the drawings
Fig. 1: the lateral plan of airframe
A---fuselage
B---wing
C---the wing flap up turning over
D---horizontal tail vane
E---the horizontal tail vane up turning over
Detailed description of the invention
1, transformation tail wheel, adds a motor in wheel.
Claims (1)
1. patent aircraft braking new departure of the present invention, is characterized in that, in the tail wheel of aircraft, a motor is installed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310086083.6A CN104058091A (en) | 2013-03-18 | 2013-03-18 | New scheme for airplane braking |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310086083.6A CN104058091A (en) | 2013-03-18 | 2013-03-18 | New scheme for airplane braking |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104058091A true CN104058091A (en) | 2014-09-24 |
Family
ID=51546088
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310086083.6A Pending CN104058091A (en) | 2013-03-18 | 2013-03-18 | New scheme for airplane braking |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104058091A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1906082A (en) * | 2003-12-15 | 2007-01-31 | 史蒂文·沙利文 | Method and apparatus for braking and maneuvering |
| CN102083686A (en) * | 2008-07-07 | 2011-06-01 | 空中客车营运有限公司 | Wheel drive system for an aircraft comprising a fuel cell as an energy source |
| CN102232039A (en) * | 2008-12-02 | 2011-11-02 | 梅西耶-道提股份有限公司 | Multifunctional electromechanical device for landing gear |
| CN102570894A (en) * | 2010-12-06 | 2012-07-11 | 梅西耶-布加蒂-道提公司 | Method of controlling brushless DC motor |
-
2013
- 2013-03-18 CN CN201310086083.6A patent/CN104058091A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1906082A (en) * | 2003-12-15 | 2007-01-31 | 史蒂文·沙利文 | Method and apparatus for braking and maneuvering |
| CN102083686A (en) * | 2008-07-07 | 2011-06-01 | 空中客车营运有限公司 | Wheel drive system for an aircraft comprising a fuel cell as an energy source |
| CN102232039A (en) * | 2008-12-02 | 2011-11-02 | 梅西耶-道提股份有限公司 | Multifunctional electromechanical device for landing gear |
| CN102570894A (en) * | 2010-12-06 | 2012-07-11 | 梅西耶-布加蒂-道提公司 | Method of controlling brushless DC motor |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20140924 |