CN1557678A - Airplane inertial taking off and landing technology - Google Patents
Airplane inertial taking off and landing technology Download PDFInfo
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- CN1557678A CN1557678A CNA2004100395591A CN200410039559A CN1557678A CN 1557678 A CN1557678 A CN 1557678A CN A2004100395591 A CNA2004100395591 A CN A2004100395591A CN 200410039559 A CN200410039559 A CN 200410039559A CN 1557678 A CN1557678 A CN 1557678A
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Abstract
The present invention is inertial taking-off and landing technology for aeroplane and is one new technology in aeronautics. Unlike the traditional taking-off and landing technology, in which horizontal runway is adopted, the new inertial taking-off and landing technology realizes taking-off and landing via calculating and controlling the taking-off and landing process. The new technology can reach the aims of saving energy, reducing noise, shortening taking-off and landing distance, prolonging aeroplane life, etc.
Description
1. the present mode of taking off has running take off and the dual mode that takes off vertically, and this inertia landing technology is mainly used on the aircraft of running take off mode.
2. the difference of this technology and the common mode of taking off is the design of airstrip; Common airstrip is a level, when aircraft takes off on this runway without any external force can by, take-off process need consume a large amount of fuel oils from the zero-speed to the built on stilts, produce huge noise; And adopt the airstrip of inertia landing technology can adopt two kinds of designs:
A) inclination (Dan Po) type runway (Fig. 1, Fig. 2): this runway is made up of two parts, one section is that the inclined-plane is a horizontal surface for one section, aircraft on this runway, take off (Fig. 1), be parked in the top, slope before taking off earlier, slide the slope when taking off and come hoisting speed by self inertia, built on stilts is finished and is taken off when reaching takeoff speed.Land at horizontal segment during aircraft landing (Fig. 2), slide to slope, high slope and push up, utilizing rises produces the huge potential energy deceleration in ground, can reduce the aircraft wearing and tearing.
B) another kind is two sloping types (Fig. 3), this runway has two slopes of height, aircraft also is to slide from top, high slope when taking off on this runway, utilizes the aircraft self inertia to quicken to take off, and two kinds of methods are then arranged during landing, a kind of is to land at horizontal segment, with last a kind of identical, another kind is to land on the inclined-plane on short slope, and aircraft fuselage when landing is a bevelled, substantially parallel with the inclined-plane, slope, when landing, can reduce the vibrations of aircraft like this.
3. description of drawings book:
A) Fig. 1 is the scheme drawing that aircraft takes off on (Dan Po) runway that tilts, among the figure 1. indication be shown airstrip (tilting section), 2. indicated dotted line is represented the path of motion of aircraft, 4. is the aircraft that quickens to take off under the high hill wash, is the stage of this runway advantage of performance at this moment; 3. and 5. being the aircraft of built on stilts of having taken off, just representing their takeoff setting difference, 3. is to reach the aircraft that speed is taken off on the slope, 5. is to reach the aircraft that takeoff speed is taken off on horizontal segment.
B) Fig. 2 is that aircraft is at the scheme drawing of (Dan Po) runway landing that tilts, among the figure 1. indication be shown airstrip (tilting section), 2. indicated dotted line is represented the path of motion of aircraft, 3. be the aircraft that just lands at horizontal segment, 4. be the aircraft that rushes at the top, slope at the horizontal segment taxi in, when rushing at the top, slope, utilize the potential energy that continues to increase suitably to slow down, stop top, slope, a left side at last.
C) Fig. 3 is aircraft (aircraft is similar in the principle of taking off on two sloping type airstrips and process and the principle and the process of taking off on single sloping type airstrip at the scheme drawing that lands on two sloping type airstrips, the Therefore, omited), among the figure 1. indication be shown airstrip (tilting section), 2. indicated dotted line is represented the path of motion of aircraft, 3. be the aircraft that lands on the short sloping inclined-plane of two sloping type airstrips, this moment, the bevelled fuselage was substantially parallel with the inclined-plane of runway, vibration in the time of can reducing aircraft landing, 4. be that the landing backlash is to the aircraft on top, high slope on short slope, also be the process of regulating the speed this moment.
4. nextpage is the airstrip and the takeoff and landing process scheme drawing of aircraft inertia landing technology:
Claims (1)
1. this technology is that aircraft moves on banked track and utilized the aircraft its own inertial to come hoisting speed.In the inclined design of the principal character airstrip of this technology,, all belong to the application protection domain of this patent so no matter aircraft is to rely on nature physical features or the apsacline runway of manually building to utilize self inertia to take off.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2004100395591A CN1557678A (en) | 2004-02-10 | 2004-02-10 | Airplane inertial taking off and landing technology |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2004100395591A CN1557678A (en) | 2004-02-10 | 2004-02-10 | Airplane inertial taking off and landing technology |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1557678A true CN1557678A (en) | 2004-12-29 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNA2004100395591A Pending CN1557678A (en) | 2004-02-10 | 2004-02-10 | Airplane inertial taking off and landing technology |
Country Status (1)
| Country | Link |
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| CN (1) | CN1557678A (en) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102556361A (en) * | 2012-02-22 | 2012-07-11 | 北京科实医学图像技术研究所 | All-weather environment-friendly airport |
| CN102619151A (en) * | 2012-04-13 | 2012-08-01 | 大连海事大学 | Special runway for wing-in-ground-effect vehicles |
| WO2013034054A1 (en) * | 2011-09-07 | 2013-03-14 | Liu Jianping | Assisted takeoff system for aircraft |
| WO2014032295A1 (en) * | 2012-09-01 | 2014-03-06 | Zhao Tianshuo | Slope downward-sliding takeoff platform for carrier-based aircraft, application aircraft carrier and realization method |
| CN104002982A (en) * | 2013-02-26 | 2014-08-27 | 邓先勇 | Rapid taking-off device for aircraft carrier plane |
| CN104229153A (en) * | 2013-06-12 | 2014-12-24 | 贺健元 | Automatic acceleration and deceleration sloping runway for aircraft carrier |
| CN104554750A (en) * | 2014-08-24 | 2015-04-29 | 李浩昌 | Land-based, sea-based and seaborne civil airports capable of realizing takeoff on slideway and landing on rampway |
| CN104963251A (en) * | 2015-07-03 | 2015-10-07 | 贡茅 | Runway and hangar integrated mushroom umbrella type slope airport |
| CN105015789A (en) * | 2014-08-25 | 2015-11-04 | 韩淮生 | Potential-energy runway |
| CN106292685A (en) * | 2015-05-20 | 2017-01-04 | 优利科技有限公司 | The model of an airplane and flight control method thereof and system |
| CN110616610A (en) * | 2019-09-12 | 2019-12-27 | 青岛度丘新能源技术有限公司 | Land flight platform |
-
2004
- 2004-02-10 CN CNA2004100395591A patent/CN1557678A/en active Pending
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2013034054A1 (en) * | 2011-09-07 | 2013-03-14 | Liu Jianping | Assisted takeoff system for aircraft |
| CN102556361A (en) * | 2012-02-22 | 2012-07-11 | 北京科实医学图像技术研究所 | All-weather environment-friendly airport |
| CN102619151A (en) * | 2012-04-13 | 2012-08-01 | 大连海事大学 | Special runway for wing-in-ground-effect vehicles |
| WO2014032295A1 (en) * | 2012-09-01 | 2014-03-06 | Zhao Tianshuo | Slope downward-sliding takeoff platform for carrier-based aircraft, application aircraft carrier and realization method |
| CN104002982A (en) * | 2013-02-26 | 2014-08-27 | 邓先勇 | Rapid taking-off device for aircraft carrier plane |
| CN104229153A (en) * | 2013-06-12 | 2014-12-24 | 贺健元 | Automatic acceleration and deceleration sloping runway for aircraft carrier |
| CN104554750A (en) * | 2014-08-24 | 2015-04-29 | 李浩昌 | Land-based, sea-based and seaborne civil airports capable of realizing takeoff on slideway and landing on rampway |
| CN105015789A (en) * | 2014-08-25 | 2015-11-04 | 韩淮生 | Potential-energy runway |
| CN106292685A (en) * | 2015-05-20 | 2017-01-04 | 优利科技有限公司 | The model of an airplane and flight control method thereof and system |
| CN106292685B (en) * | 2015-05-20 | 2019-11-26 | 优利科技有限公司 | The model of an airplane and its flight control method and system |
| CN104963251A (en) * | 2015-07-03 | 2015-10-07 | 贡茅 | Runway and hangar integrated mushroom umbrella type slope airport |
| CN110616610A (en) * | 2019-09-12 | 2019-12-27 | 青岛度丘新能源技术有限公司 | Land flight platform |
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| 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 |