JPH10305799A - Buffer turbine wheel - Google Patents

Buffer turbine wheel

Info

Publication number
JPH10305799A
JPH10305799A JP9151497A JP15149797A JPH10305799A JP H10305799 A JPH10305799 A JP H10305799A JP 9151497 A JP9151497 A JP 9151497A JP 15149797 A JP15149797 A JP 15149797A JP H10305799 A JPH10305799 A JP H10305799A
Authority
JP
Japan
Prior art keywords
tire
turbine
buffer
blade
runway
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
Application number
JP9151497A
Other languages
Japanese (ja)
Inventor
Maaku Setsuson Yokota
マーク雪村 横田
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to JP9151497A priority Critical patent/JPH10305799A/en
Publication of JPH10305799A publication Critical patent/JPH10305799A/en
Pending legal-status Critical Current

Links

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  • Tires In General (AREA)

Abstract

PROBLEM TO BE SOLVED: To relax frictional resistance received between a tire and a runway when an aircraft is landed. SOLUTION: In this buffer turbine wheel, a turbine 2 is set up in a tire 1. Of blades 3, 4 in the turbine 2, the blade 3 provided in an upper part of the tire 1 receives no resistance of a wind 5, but of the blades 3, 4 of the turbine 2, the blade 4 mounted in a bottom part of the tire 1 receives resistance of the wind, so as to rotate the tire in a direction of arrow mark 6, frictional resistance generated between the tire and a runway instantaneously at landing can be suppressed.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【０００１】本発明は、航空機の着陸時に無回転状態の
タイヤが滑走路に触れて機体に大きな衝撃が加わるのを
防ぐものである。The present invention is intended to prevent a non-rotating tire from touching the runway when the aircraft lands and applying a large impact to the fuselage.

【０００２】従来の航空機のタイヤは、着陸時にタイヤ
が無回転状態になっている為に、着陸の瞬間にタイヤと
滑走路との間に大きな摩擦抵抗が発生し、機体に大きな
衝撃が加わる事があるので危険であった。In conventional aircraft tires, since the tires are in a non-rotating state at the time of landing, a large frictional resistance is generated between the tires and the runway at the moment of landing, and a large impact is applied to the fuselage. It was dangerous because there was.

【０００３】本発明は、航空機のタイヤに着陸時の飛行
速度に比例した回転速度を与え、着陸の瞬間にタイヤと
滑走路との間に発生する摩擦抵抗を低く抑えるものであ
る。The present invention provides an aircraft tire with a rotational speed proportional to the flight speed at the time of landing, and reduces the frictional resistance generated between the tire and the runway at the moment of landing.

【０００４】本発明は、航空機のタイヤにタービンを設
置するものである。The present invention is to install a turbine on an aircraft tire.

【０００５】本発明を用いると、航空機のタイヤに設置
したタービンが風の影響を受けてタイヤを回転させるの
で、着陸の瞬間にタイヤと滑走路との間に発生する摩擦
抵抗を低く抑える事ができる。According to the present invention, the turbine mounted on the tire of an aircraft rotates the tire under the influence of the wind, so that the frictional resistance generated between the tire and the runway at the moment of landing can be reduced. it can.

【０００６】本発明の実施例としては、図１のようにタ
イヤ（１）にタービン（２）を設置するものが上げられ
る。[0006] As an embodiment of the present invention, there is one in which a turbine (2) is installed on a tire (1) as shown in FIG.

【０００７】本発明を用いると、タービン（２）の羽根
（３）（４）の内、タイヤ（１）の上部に付く羽根
（３）は風（５）の抵抗を受けないが、タービン（２）
の羽根（３）（４）の内、タイヤ（１）の底部に付く羽
根（４）は風の抵抗を受けるので、タイヤは矢印（６）
の方向に回転させられ、着陸の瞬間にタイヤと滑走路と
の間に発生する摩擦抵抗を低く抑える事ができる。According to the present invention, among the blades (3) and (4) of the turbine (2), the blade (3) attached to the upper portion of the tire (1) does not receive the resistance of the wind (5). 2)
Of the blades (3) and (4), the blade (4) attached to the bottom of the tire (1) receives wind resistance.
And the frictional resistance generated between the tire and the runway at the moment of landing can be kept low.

【図面の簡単な説明】[Brief description of the drawings]

【図１】緩衝タービンホイールの構造図である。FIG. 1 is a structural view of a shock absorbing turbine wheel.

【符号の説明】[Explanation of symbols]

１ タイヤ ２ タービン ３ タービン（２）の羽根の内、タイヤ（１）の上部に
付く羽根 ４ タービン（２）の羽根の内、タイヤ（１）の底部に
付く羽根 ５ 風の流れ ６ タイヤ（１）が回転する方向を示す矢印DESCRIPTION OF SYMBOLS 1 Tire 2 Turbine 3 Blade of turbine (2), blade attached to upper part of tire (1) 4 Blade of turbine (2), blade attached to bottom of tire (1) 5 Wind flow 6 Tire (1) Arrow indicating the direction of rotation

Claims (1)

【特許請求の範囲】[Claims] 【請求項１】 図１のように、タイヤ（１）にタービン
（２）を設置する事により構成される航空機用のタイ
ヤ。1. An aircraft tire comprising a turbine (2) mounted on a tire (1) as shown in FIG.
JP9151497A 1997-05-06 1997-05-06 Buffer turbine wheel Pending JPH10305799A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9151497A JPH10305799A (en) 1997-05-06 1997-05-06 Buffer turbine wheel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9151497A JPH10305799A (en) 1997-05-06 1997-05-06 Buffer turbine wheel

Publications (1)

Publication Number Publication Date
JPH10305799A true JPH10305799A (en) 1998-11-17

Family

ID=15519803

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9151497A Pending JPH10305799A (en) 1997-05-06 1997-05-06 Buffer turbine wheel

Country Status (1)

Country Link
JP (1) JPH10305799A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101436561B1 (en) * 2013-02-13 2014-09-05 김범 Windmill Wheel Apparatus
US20170218924A1 (en) * 2014-05-12 2017-08-03 The Yokohama Rubber Co., Ltd. Power Generation System
CN107719649A (en) * 2016-08-10 2018-02-23 大东冲压工业株式会社 Airborne vehicle tire

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101436561B1 (en) * 2013-02-13 2014-09-05 김범 Windmill Wheel Apparatus
US20170218924A1 (en) * 2014-05-12 2017-08-03 The Yokohama Rubber Co., Ltd. Power Generation System
US10774812B2 (en) * 2014-05-12 2020-09-15 The Yokohama Rubber Co., Ltd. Power generation system
US11781525B2 (en) 2014-05-12 2023-10-10 The Yokohama Rubber Co., Ltd. Power generation system
CN107719649A (en) * 2016-08-10 2018-02-23 大东冲压工业株式会社 Airborne vehicle tire

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