JPH07149295A - Aircraft landing time tire same speed rotating method and device therefor - Google Patents
Aircraft landing time tire same speed rotating method and device thereforInfo
- Publication number
- JPH07149295A JPH07149295A JP36151491A JP36151491A JPH07149295A JP H07149295 A JPH07149295 A JP H07149295A JP 36151491 A JP36151491 A JP 36151491A JP 36151491 A JP36151491 A JP 36151491A JP H07149295 A JPH07149295 A JP H07149295A
- Authority
- JP
- Japan
- Prior art keywords
- tire
- motor
- aircraft
- landing
- wheel
- 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
Links
Landscapes
- Tires In General (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】この発明は航空機の着陸時のタイ
ヤ保護による安全装置に関するものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a safety device for protecting tires when an aircraft lands.
【0002】[0002]
【従来の技術】航空機は着陸時であっても、かなりの高
速で地面と接地することになる。その場合、従来の技術
ではタイヤは全く回転をしていない。その為着陸時に於
てタイヤは急に地面と接地するため、その速度差による
ショックによりタイヤはかなりいたみ、時によってはタ
イヤはバーストをして、人命に関わる大事故を起こし
て、乗客乗員を、危険におとしいれるのである。2. Description of the Related Art An aircraft will land on the ground at a fairly high speed even when landing. In that case, in the conventional technique, the tire is not rotating at all. Therefore, at the time of landing, the tire suddenly contacts the ground, so the shock due to the speed difference caused the tire to be considerably damaged, and in some cases the tire bursts, causing a serious accident involving human life, You are in danger.
【0003】[0003]
【発明が解決しようとする課題】航空機が安全に着陸で
きるかということは、人命に関わる極めて大切な事であ
る。上記のようなタイヤのいたみや、それに関わる着地
時のショックによる、タイヤのバーストなどの事故や航
空機が着陸してからアイスバーンの滑走路からはみ出す
ことなどを、未然に防ぐことが大きな課題である。[Problems to be Solved by the Invention] Whether or not an aircraft can land safely is extremely important for human life. It is a major issue to prevent accidents such as tire bursts and accidents such as tire bursts and sticking out of the ice burn runway after the aircraft has landed due to the above-mentioned tire damage and related shocks on landing. .
【0004】[0004]
【課題を解決するための手段】安全のための処置とし
て、航空機が着陸時にタイヤ(2)を航空機の速さと同
じ速さで、モーター(25)などにより回転させ着陸さ
せる。As a measure for safety, when the aircraft lands, the tire (2) is rotated at the same speed as the aircraft by a motor (25) or the like to land.
【0005】[0005]
【作用】航空機の着睦時にモーター(25)や風力や航
空機の動力によりタイヤ(2)を回転させるという考え
方により、航空機の速度とタイヤ(2)の回転による速
度を同速にする為、大変着地がスムーズになり着地時に
起きる摩擦によるショックが激減し又、タイヤ(2)も
傷まない。結果として航空機はきわめて、安全な着陸が
出釆る。The function of rotating the tire (2) by the motor (25), wind force or power of the aircraft when the aircraft is landing is the same because the speed of the aircraft and the speed of rotation of the tire (2) are the same. The landing will be smooth and the shock due to friction during landing will be greatly reduced, and the tire (2) will not be damaged. As a result, the aircraft is extremely safe to land.
【0006】[0006]
【実施例】モーターの動力伝達装置によるタイヤ回転の
説明[Example] Description of tire rotation by a power transmission device of a motor
【図2】[Fig. 2]
【図3】[Figure 3]
【図7】[Figure 7]
【図8】に示すように、着陸時にまずモーター(25)
が回転することにより動力はモーター回転軸(14)に
伝わり、モーターギィア(15)は回転する。それによ
り[Fig. 8] As shown in Fig. 8, when landing, first the motor (25)
The power is transmitted to the motor rotating shaft (14) by rotating the motor, and the motor gear (15) rotates. Thereby
【図2】[Fig. 2]
【図4】[Figure 4]
【図7】に示す様に空転輪(6)が矢印のように回転
し、止め軸(5)で回転自在で装着している空転リブ
(4)が車軸(1)を中心に回転すると遠心力で先が中
心に向いてくるため、引き掛けギィア(3)と噛み合
い、引き掛けギィア(3)は回転する。As shown in FIG. 7, the idle wheel (6) rotates as shown by the arrow, and the idle rib (4) rotatably mounted on the stop shaft (5) rotates about the axle (1), causing centrifugal force. Since the tip of the hook moves toward the center due to the force, it engages with the hooking gear (3), and the hooking gear (3) rotates.
【図7】に示すように引き掛けギィア突起(27)は全
て車軸(1)を中心に回転し、引き掛けギィア突起(2
7)とAs shown in FIG. 7, all of the hooking gear projections (27) rotate around the axle (1), and the hooking gear projections (2) are rotated.
7) and
【図2】[Fig. 2]
【図8】に示す様に、タイヤホイール(23)とタイヤ
(2)は矢印の方向に回転する。そして長い矢印は航空
機の進路方向を示している。As shown in FIG. 8, the tire wheel (23) and the tire (2) rotate in the direction of the arrow. And the long arrow shows the course of the aircraft.
【0007】モーター動力切り離し装置説明1 タイヤ
(2)の方がモーター(25)よりも回転による速度が
速く成った場合、Description of motor power disconnecting device 1 When the speed of rotation of the tire (2) is faster than that of the motor (25),
【図4】[Figure 4]
【図7】に示す様に、引き掛けギィア(3)は空転リブ
(4)により片方向にしか回転しない、例えば着陸時に
航空機の速度の方がモーター(25)の回転による速度
よりも速く成った場合は、空転輪(6)の回りを引き掛
けギィア(3)が空回りをし、タイヤ(2)からの過剰
な回転力による本機構への負担を無くしているのであ
る。As shown in FIG. 7, the hooking gear (3) rotates only in one direction due to the idling rib (4). For example, the speed of the aircraft during landing is faster than the speed due to the rotation of the motor (25). In this case, the gear (3) spins around the idle wheel (6) and spins around the idle wheel (6), thereby eliminating the load on the mechanism due to the excessive rotational force from the tire (2).
【0008】モーター動力切り離し装置説明2 反対に
着陸時に航空機の速度の方がモーター(25)の回転に
よる速度よりも遅く成った場合は、Motor power disconnection device explanation 2 On the contrary, when the speed of the aircraft becomes slower than the speed due to the rotation of the motor (25) at the time of landing,
【図1】[Figure 1]
【図2】に示す様に、タイヤ(2)が着陸時に持ち上が
ると、スプリング(10)に取り付いている部品は全て
上に持ち上がる。その為車軸(1)車軸止め具(17)
などが持ち上がり止め軸(19)に取り付いている押し
下げロット受け(20)ち持ち上がる。その時に押し下
げロット(12)は、押し下げロット受け(20)と当
たる。結果的に押し下げロット(12)により、押し下
げロット受け(20)が押し下げられ、押し下げロット
受け(20)は止め軸(19)を中心に失印方向に押し
回されて、そしてそれがスライドロット(9)を矢印の
方向に押し出す。As shown in FIG. 2, when the tire (2) is lifted at landing, all parts attached to the spring (10) are lifted up. Therefore axle (1) axle stop (17)
The lifted down lot holder (20) attached to the lifting stop shaft (19) lifts. At that time, the depressed lot (12) hits the depressed lot receiver (20). As a result, the push-down lot (12) pushes down the push-down lot receiver (20), and the push-down lot receiver (20) is pushed around the stop shaft (19) in the unmarked direction, and the slide lot ( Push out 9) in the direction of the arrow.
【図2】[Fig. 2]
【図4】[Figure 4]
【図7】に示す様にスライドロット(9)は、回転して
いる空転リブ(4)の外側に当たり、空転リブ(4)と
引き掛けギィア(3)は、空回りするのである。これも
またAs shown in FIG. 7, the slide lot (9) hits the outside of the rotating idle rib (4), and the idle rib (4) and the hooking gear (3) idle. This too
【0007】と同様に、タイヤ(2)からの回転力によ
る本機構への負担を無くしているのである。Similarly to the above, the load on this mechanism due to the rotational force from the tire (2) is eliminated.
【0009】複数並列タイヤ伝達動力説明Description of multiple parallel tire transmission power
【図11】に示すように並列タイヤになる場合、モータ
ー(25)の動力により回された内側のタイヤ(2)か
ら外側のタイヤ(2)への動力伝達を行い回転させる。
内側ホイールに回転体受けスライド管(33)をボルト
により取り付けWhen a parallel tire is formed as shown in FIG. 11, power is transmitted from the inner tire (2) rotated by the power of the motor (25) to the outer tire (2) and rotated.
Attach the rotating body receiving slide tube (33) to the inner wheel with bolts
【図9】〜FIG. 9
【図11】に示すようにその先端に回転体(29)を取
り付けその回りにある回転体軟質羽根(32)をタイヤ
ホイール突起(30)に当てゆっくりと回すと外側のタ
イヤ(2)は動力を受け回る。またいずれかのタイヤ
(2)が大きな外力を受ける事により回転による速度が
各々違つてくる場合、回転体軟質羽根(32)は弾力が
ある物質で作られているため、有る一定の力以上でタイ
ヤホイール突起(30)と当たるとき、回転体軟質羽根
(32)の先端は曲がりそして回転体軟質羽根(32)
はタイヤホイール突起(30)で滑り、タイヤ(2)は
各々独立をした回転により回るのである。[Fig. 11] As shown in Fig. 11, the rotor (29) is attached to the tip of the tire and the rotor soft blades (32) around the rotor are applied to the tire wheel protrusions (30) and slowly rotated, so that the outer tire (2) is powered. Go around. Also, if any of the tires (2) receives a large external force and the speeds due to the rotations are different, the rotor soft blades (32) are made of an elastic material, so that the force is not less than a certain force. When hitting the tire wheel protrusion (30), the tip of the rotor soft blade (32) bends and the rotor soft blade (32)
Slips on the tire wheel protrusions (30), and the tires (2) rotate by independent rotation.
【0010】[0010]
【発明の効果】航空機の事故は大変大惨事に結びつき安
く、特に離陸や着陸の時は極めて事故が起き安い。中で
も悪天候における着陸は、極めて条件が悪く、圧雪やア
イスバーンなどの状況は最悪であり、スリップにより滑
走路からはみ出す事もあり、よりスムーズな着陸が要求
される。木発明により着陸の際、スムーズな着陸が出
来、より速く安定状態に入る事が出来る為、瞬敏な減速
をする事が可能になり、極めて安全な着陸が出来る。ま
たタイヤ(2)の傷みが非常に少なくその事からもより
安全であり、そして経済的な運行が可能となる。EFFECTS OF THE INVENTION Aircraft accidents are extremely catastrophic and cheap, especially when taking off or landing. Above all, landing in bad weather is extremely bad, and conditions such as snowstorms and ice burns are the worst, and slipping can cause the landing to run off the runway, so smoother landing is required. With the invention of wood, when landing, you can land smoothly, and you can enter a stable state faster, so you can decelerate quickly and land extremely safely. In addition, the tire (2) has very few damages, which is also safer and enables economical operation.
【図1】全体正面図1] Overall front view
【図2】全体斜視図FIG. 2 is an overall perspective view
【図3】平面図FIG. 3 is a plan view.
【図4】モーター動力伝達切り離し装置側面図(一部断
面図)FIG. 4 is a side view (partially sectional view) of a motor power transmission disconnecting device.
【図5】空転輪(6)止め軸(5)側面図FIG. 5 is a side view of the idle wheel (6) and the retaining shaft (5).
【図6】空転輪(6)止め軸(5)斜視図FIG. 6 is a perspective view of the idle wheel (6) and the retaining shaft (5).
【図7】モーター動力伝達切り離し装置斜視図FIG. 7 is a perspective view of a motor power transmission disconnecting device.
【図8】全体断面図FIG. 8 is an overall sectional view
【図9】並立タイヤの場合の動力伝達装置の平面図FIG. 9 is a plan view of a power transmission device in the case of parallel tires.
【図10】並立タイヤの場合の動力伝達装置の斜視図FIG. 10 is a perspective view of a power transmission device in the case of parallel tires.
【図11】並立タイヤの場合の動力伝達装置の断面図FIG. 11 is a cross-sectional view of a power transmission device in the case of parallel tires.
1 車軸 2 タイヤ 3 引き掛けギィア 4 空転リブ 5 止め軸 6 空転輪 7 コイルスプリング 8 スライド管 9 スライドロット 10 スプリング 11 スプリング受け板 12 押し下げロット 13 押し下げロット振れ止め 14 モーター回転軸 15 モーターギィア 16 フレーム 17 車軸止め具 18 スプリングスライド管 19 止め軸 20 押し下げロット受け 21 止め軸 22 止め軸 23 タイヤホイール 24 車軸止め具受けプレート 25 モーター 26 モーター受けプレート 27 引き掛けギィヤ突起 28 スライド穴 29 回転体 30 タイヤホイール突起 31 スライド管受けプレート 32 回転体軟質羽根 33 回転体受けスライド管 1 Axle 2 Tire 3 Pulling gear 4 Idling rib 5 Stopping shaft 6 Idling wheel 7 Coil spring 8 Slide tube 9 Slide lot 10 Spring 11 Spring receiving plate 12 Push down lot 13 Push down lot steady rest 14 Motor rotating shaft 15 Motor gear 16 Frame 17 Axle Stopper 18 Spring slide tube 19 Stopper shaft 20 Push-down lot holder 21 Stopper shaft 22 Stopper shaft 23 Tire wheel 24 Axle stopper stop plate 25 Motor 26 Motor receiver plate 27 Hooking gear projection 28 Slide hole 29 Rotating body 30 Tire wheel projection 31 Slide tube receiving plate 32 Rotating body soft blade 33 Rotating body receiving slide tube
Claims (1)
置 引き掛けギィア(3)空転リブ(4)空転輪(6)
スライド管(8)スライドロット(9)押し下げロット
(12)スライド穴(28)モーターギィア(15)タ
イヤホイール突起(30)回転体軟質羽根(32)1. A method and an apparatus for rotating tires at the same speed during landing of an aircraft Hooking gear (3) Idling rib (4) Idling wheel (6)
Slide tube (8) Slide lot (9) Push down lot (12) Slide hole (28) Motor gear (15) Tire wheel protrusion (30) Rotor soft blade (32)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP36151491A JPH07149295A (en) | 1991-12-27 | 1991-12-27 | Aircraft landing time tire same speed rotating method and device therefor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP36151491A JPH07149295A (en) | 1991-12-27 | 1991-12-27 | Aircraft landing time tire same speed rotating method and device therefor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH07149295A true JPH07149295A (en) | 1995-06-13 |
Family
ID=18473893
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP36151491A Pending JPH07149295A (en) | 1991-12-27 | 1991-12-27 | Aircraft landing time tire same speed rotating method and device therefor |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH07149295A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0939897A (en) * | 1995-07-31 | 1997-02-10 | Shuji Tanada | Device for lengthening life of tire for takeoff and landing of aircraft |
-
1991
- 1991-12-27 JP JP36151491A patent/JPH07149295A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0939897A (en) * | 1995-07-31 | 1997-02-10 | Shuji Tanada | Device for lengthening life of tire for takeoff and landing of aircraft |
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