JP2009190712A - Landing method of aircraft - Google Patents
Landing method of aircraft Download PDFInfo
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- JP2009190712A JP2009190712A JP2008061828A JP2008061828A JP2009190712A JP 2009190712 A JP2009190712 A JP 2009190712A JP 2008061828 A JP2008061828 A JP 2008061828A JP 2008061828 A JP2008061828 A JP 2008061828A JP 2009190712 A JP2009190712 A JP 2009190712A
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- landing
- aircraft
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- wheels
- vehicle
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- 238000000034 method Methods 0.000 title claims abstract description 9
- 238000005096 rolling process Methods 0.000 claims description 4
- 238000004904 shortening Methods 0.000 description 1
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Abstract
Description
航空機体の着陸方法であるThe landing method of the aircraft body
現在、色々な航空機が存在するが着陸時には自己の車輪で着地を為すのが、現状であるCurrently, there are various aircraft, but at the time of landing, it is the current situation that you make a landing with your own wheels
そこで、航空機、又は航空体から車輪を除去し着陸時は地上を走行する機体受け台車、又は回転抵抗付き弾性空転体などにより着陸を為さんとするものであるTherefore, when landing after removing the wheels from the aircraft or the air body, the landing is made by the body receiving cart that runs on the ground or the elastic rolling body with rotation resistance.
（特許願・２００６−６８３３５号参考）地上の軌道上を、航空体着陸用の台車を走らせ、台車により航空体を着陸させる方法(Refer to Japanese Patent Application No. 2006-68335) A method of running an aircraft landing truck on a track on the ground and landing the aircraft with the carriage
又、地上に回転抵抗付き弾性空転体を敷設し、航空機を空転体上に着陸させる方法Also, a method of laying an elastic rolling element with rotational resistance on the ground and landing the aircraft on the rolling element
（特許願・２００６−６８３３５参考）の如く曳航される事を特徴とした航空体の場合には軌道上を機体受け台車を同時に牽引走行させる事により、制御確実な着陸が得られる、例、第１図In the case of an aircraft that is towed as shown in (Patent Application No. 2006-68335), a reliable landing can be obtained by simultaneously towing the aircraft receiving carriage on the track. 1 figure
航空機、又は航空体の着陸用の車輪を除去することにより、機体の軽量化が得られ、積載効率が向上し、ランニングコストの低下が得られるRemoval of aircraft or aircraft landing wheels can reduce the weight of the aircraft, improve loading efficiency, and reduce running costs
又、機体受け用台車に対する、地上管制操作により、最適、安全な方策を選択出来る有利さが得られるIn addition, the advantage of being able to select the optimal and safe policy by the ground control operation for the body receiving cart is obtained.
特に、前述の（特許願・２００６−６８３３５参考）の如き曳航される事を特徴とした航空体では対気流、対気候などで有利、安全に機体受け用台車に航空体を着陸させる効果が得られるIn particular, an aircraft that is towed as described above (see Patent Application No. 2006-68335) is advantageous in terms of airflow and climate, and has the effect of safely landing the aircraft on the airframe receiving carriage. Be
地上軌道の走行を為す牽引車と航空体着陸用台車と後部制御車を連結させ走行させる、Connect the tow vehicle, the aircraft landing vehicle, and the rear control vehicle for running on the ground track,
又、着陸用台車と航空体を連結し、航空体の航行高さ、横流れなどの制御を計るIn addition, the landing cart and the aircraft are connected, and the navigational height and lateral flow of the aircraft are controlled.
この為、牽引間隔の伸縮、牽引具の長短などにより航空体の着陸の制御を計れるものであり、着陸用台車と航空体を確実に制御可能な方法を得るものである．For this reason, it is possible to control the landing of the air body by extending or shortening the towing interval, the length of the towing tool, etc., and obtain a method that can reliably control the landing carriage and the air body.
１牽引東 ２航空体 ３着陸台車 ４後部制御車 ５牽引ロープ1 towing east 2 aircraft body 3 landing trolley 4 rear control car 5 towing rope
Claims (2)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2008061828A JP2009190712A (en) | 2008-02-13 | 2008-02-13 | Landing method of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2008061828A JP2009190712A (en) | 2008-02-13 | 2008-02-13 | Landing method of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JP2009190712A true JP2009190712A (en) | 2009-08-27 |
Family
ID=41073095
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2008061828A Pending JP2009190712A (en) | 2008-02-13 | 2008-02-13 | Landing method of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2009190712A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102390543A (en) * | 2011-08-23 | 2012-03-28 | 北京航空航天大学 | Vertical landing track design method for unmanned aerial vehicle |
-
2008
- 2008-02-13 JP JP2008061828A patent/JP2009190712A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102390543A (en) * | 2011-08-23 | 2012-03-28 | 北京航空航天大学 | Vertical landing track design method for unmanned aerial vehicle |
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