JP3095693U - Aircraft tires whose wheels automatically rotate in the landing direction before the aircraft lands. - Google Patents

Aircraft tires whose wheels automatically rotate in the landing direction before the aircraft lands.

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Publication number
JP3095693U
JP3095693U JP2003001219U JP2003001219U JP3095693U JP 3095693 U JP3095693 U JP 3095693U JP 2003001219 U JP2003001219 U JP 2003001219U JP 2003001219 U JP2003001219 U JP 2003001219U JP 3095693 U JP3095693 U JP 3095693U
Authority
JP
Japan
Prior art keywords
aircraft
tire
landing
air resistance
semicircular
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.)
Expired - Fee Related
Application number
JP2003001219U
Other languages
Japanese (ja)
Inventor
順太 香月
Original Assignee
順太 香月
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 順太 香月 filed Critical 順太 香月
Priority to JP2003001219U priority Critical patent/JP3095693U/en
Application granted granted Critical
Publication of JP3095693U publication Critical patent/JP3095693U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

(57)【要約】 (修正有) 【課題】 この考案は、航空機が着陸する際の、当該航
空機のタイヤと着陸接地面の摩擦抵抗を軽減する航空機
用のタイヤ構造に関するものである。 【解決手段】 航空機の着陸用タイヤ4に、空気対抗を
受ける半円形状の羽根型の突起5を複数型成したタイヤ
を着装することにより、当該航空機が着陸準備のために
着陸用車輪を機体から出した際に、当該航空機の着陸用
タイヤを着陸の進行方向に向かって、前もって回転させ
ることが可能になり、以て、当該航空機の着陸用タイヤ
と着陸接地面との摩擦抵抗を減少して、当該航空機の機
体、車軸、タイヤ等への衝撃負荷を軽減し、当該航空機
のより安全な運行や着陸をはかるものである。
(57) [Summary] (Modified) [PROBLEMS] The present invention relates to a tire structure for an aircraft for reducing frictional resistance between a tire of the aircraft and a landing contact surface when the aircraft lands. SOLUTION: By mounting a plurality of semicircular wing-shaped projections 5 receiving air resistance on a landing tire 4 of an aircraft, the aircraft can use landing gear to prepare for landing. When the vehicle comes out of the aircraft, the landing tire of the aircraft can be rotated in advance in the direction of landing, thereby reducing the frictional resistance between the landing tire of the aircraft and the landing contact surface. Thus, the impact load on the fuselage, axle, tires, etc. of the aircraft is reduced, so that the aircraft can operate and land more safely.

Description

【考案の詳細な説明】 【0001】 【考案の属する技術分野】 この考案は、航空機の着陸用の車輪に、空気抵抗を受ける半円形状の羽根型の 突起を複数有し、同航空機の着陸進行する方向に向かって自動回転するタイヤを 着装することで、航空機が着陸する時のタイヤと接地面の摩擦抵抗を少なくする ものである。 【0002】 【従来の技術】 従来、航空機が着陸接地の際、航空機の着陸用の車輪ゴムタイヤがあらかじめ 回転しないため、接地面との著しい摩擦抵抗により、瞬間的に白煙をあげる程に 発熱し、さらに接地時の衝撃によりパンク事故のほか、タイヤや機体を支える車 軸等の劣化損傷に多大の悪影響があった。 【0003】 【考案が解決しようとする課題】 本案は、従来の欠点を除くため、航空機が着陸接地の際、同航空機の着陸用の タイヤを前もって着陸進行方向に向かって回転させておくことによって、タイヤ と地面との摩擦抵抗をより少なくし、より安全な航空機の着陸に寄与するもので ある。 【0004】 【課題を解決するための手段】 いまその手段を図面に追いながら説明すれば、 (ア) 航空機用のタイヤの両側面、又は片側の側面に、当該航空機のタイヤサ イズに合致した数や大きさの空気抵抗を受ける半円形状の羽根型の突起を複数有 するタイヤを、当該航空機用タイヤ製造時に型成して製造(図1、図2、図3、 図4)し、当該航空機に着装する。 (イ) 航空機用タイヤの両側面、あるいは片側面に、当該航空機のタイヤサイ ズと同一外周を有し、同タイヤサイズに合致した数や大きさの空気抵抗を受ける 半円形状の羽根型の突起を複数有する焼きつけ型成した物(図5)を、接着ある いは圧着したタイヤ(図6)を製造し、当該航空機に着装する。 (ウ) 当該航空機に着装する際の、空気抵抗を受ける半円形状の羽根型の突起 の向きついては、前記【請求項3】のとおり、当該航空機の機体車軸の中心から 左右のそれぞれのタイヤが空気抵抗によって当該航空機の着陸進行方向に向かっ て、回転する突起の向き方にする。 (エ) 当該航空機用に製造する場合の、突起の向き方については、前記(ウ) のとおり、同機体の着陸進行方向に向かって回転するように同機体の車軸の中心 から左右それぞれの両側面用(図7)(図8)片側側面用(図9)(図10)に する。 【0005】 【考案の実施の形態】 当該航空機用のタイヤホイルに着装際の、半円形状の羽根型の突起の向きつい ては、当該航空機によっては、車輪の大小のほか車軸とタイヤホイルの形状から 当該航空機の機体車軸の中心からそれぞれ右用左用とある場合があるので、左右 それぞれのタイヤが空気抵抗によって当該航空機の着陸進行方向に向かって、回 転する突起の向き方にする。 本案は、これらの構造物を、製造し、当該航空機に着装するものである。 【0006】 【考案の効果】 したがって、航空機が着陸の際、同航空機の着陸用のタイヤ車輪が着陸進行方 向に向かって接地前から自動回転することから、同航空機が着陸する時に接地抵 抗が少なく、タイヤのパンク事案のほか接地時の機体や車軸の衝撃が減少し機体 の損傷劣化防止に効果がある。[Detailed description of the invention]   [0001] [Technical field to which the invention belongs]   This invention is based on a semi-circular vane-shaped A tire that has multiple protrusions and automatically rotates in the direction of landing of the aircraft Wearing reduces the frictional resistance between the tire and the tread when the aircraft lands Things.   [0002] [Prior art]   Conventionally, when the aircraft is in landing touchdown, rubber tires for aircraft landing Because it does not rotate, it produces white smoke instantaneously due to remarkable frictional resistance with the ground surface Cars that generate heat and cause puncture accidents due to impact when touching down, and support tires and aircraft There was a great adverse effect on shaft and other deterioration damage.   [0003] [Problems to be solved by the invention]   In order to eliminate the conventional drawbacks, the present invention proposes that the aircraft By rotating the tire in advance in the landing direction, And reduce frictional resistance between the ground and the ground, contributing to safer aircraft landing. is there.   [0004] [Means for Solving the Problems] Now, let's explain the means while following the drawing, (A) On both sides or one side of the aircraft tire, Multiple semicircular blade-shaped projections that receive air resistance of the number and size that matches the size The tire to be manufactured is manufactured by molding at the time of manufacturing the aircraft tire (FIGS. 1, 2, 3, (Fig. 4) and wear the aircraft. (B) On both sides or one side of the aircraft tire, Has the same outer circumference as the tire and receives air resistance of the number and size that matches the tire size A baking type product having a plurality of semicircular blade-shaped projections (FIG. 5) is bonded. Alternatively, a crimped tire (FIG. 6) is manufactured and mounted on the aircraft. (C) A semi-circular wing-shaped projection that receives air resistance when worn on the aircraft As described in [Claim 3] above, the direction of The left and right tires move toward the landing direction of the aircraft due to air resistance. The direction of the rotating projection. (D) Regarding the orientation of the projections when manufacturing for the aircraft, see (c) above. The center of the axle of the aircraft so that it rotates in the landing direction of the aircraft From both sides (Fig. 7) (Fig. 8) and one side (Fig. 9) (Fig. 10) I do.   [0005] [Embodiment of the invention]   The orientation of the semicircular wing-shaped projections when mounting on the aircraft tire wheel Depending on the aircraft, depending on the size of the wheels, the shape of the axles and tire wheels, There are cases where there are right and left for each from the center of the aircraft axle. Each tire rotates in the direction of landing of the aircraft due to air resistance. Make the direction of the rolling projections.   In the present invention, these structures are manufactured and mounted on the aircraft.   [0006] [Effect of the invention]   Therefore, when the aircraft lands, the landing tire wheels of the aircraft The aircraft automatically rotates before landing, so when the aircraft lands, the ground contact There is little resistance, and in addition to tire puncture cases, the impact of the aircraft and axle at the time of touchdown is reduced and the aircraft It is effective in preventing damage deterioration.

【図面の簡単な説明】 【図1】本考案の空気抵抗を受ける半円形状の羽根型の
突起の側面図 【図2】本考案の空気抵抗を受ける半円形状の羽根型の
突起の平面図 【図3】本考案の空気抵抗を受ける半円形状の羽根型の
突起の斜視図 【図4】空気抵抗を受ける半円形状の羽根型の突起を複
数有するタイヤの状況 【図5】当該航空機のタイヤサイズと同一円周を有し、
同タイヤサイズに合致した数や大きさの半円形状の羽根
型の突起を複数有する物で、用法上、航空機用タイヤに
接着あるいは圧着するために 【請求項2】を型成製造した物 【図6】「図5」を、接着あるいは圧着したタイヤの断
面斜視図 【図7】機体車軸の中心から右側、側面用の半円形状の
羽根型の突起の向きの状況 【図8】機体車軸の中心から左側、側面用の半円形状の
羽根型の突起の向きの状況 【図9】機体車軸の中心から右側の片側、側面用の半円
形状の羽根型の突起の向きの状況 【図10】機体車紬の中心から左側の片側、側面用の半
円形状の羽根型の突起の向きの状況 【符号の説明】 1は航空機が着陸時の進行方向 2は機体着陸車輪の車軸 3はタイヤホイル 4は空気抵抗を受ける半円形状の羽根型の複数の突起を
有するタイヤ 5は空気抵抗を受ける半円形状の羽根型の突起の向きの
状況 6はタイヤの回転方向を矢印で示した状況
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a side view of a semicircular blade-shaped projection receiving air resistance according to the present invention. FIG. 2 is a plane view of a semicircular blade-shaped projection receiving air resistance according to the present invention. FIG. 3 is a perspective view of a semicircular wing-shaped projection receiving air resistance according to the present invention. FIG. 4 is a situation of a tire having a plurality of semicircular wing-shaped projections receiving air resistance. Have the same circumference as the aircraft tire size,
A product that has a plurality of semicircular blade-shaped protrusions of the number and size corresponding to the tire size, and is formed by molding [Claim 2] for bonding or crimping to an aircraft tire in usage. FIG. 6 is a cross-sectional perspective view of a tire in which “FIG. 5” is adhered or crimped. FIG. 7 is the situation of the orientation of a semicircular blade-shaped projection for the right and side from the center of the body axle. Left and right side semicircular vane-shaped projections from the center of the aircraft [Fig. 9] Direction of semicircular vane-shaped projections for one side and right side from the center of the vehicle axle [Fig. 10. The direction of the semicircular wing-shaped projections for one side and the left side from the center of the airframe car pongee [Explanation of reference numerals] 1 is the traveling direction when the aircraft lands 2 is the axle 3 of the aircraft landing wheels The tire wheel 4 is a tire 5 having a plurality of semicircular blade-shaped projections that receive air resistance. Is the situation of the direction of the semicircular wing-shaped projection receiving the air resistance 6 is the situation where the rotation direction of the tire is indicated by an arrow

Claims (1)

【実用新案登録請求の範囲】 【請求項1】 航空機用タイヤの両側面あるいは片側面
に空気抵抗を受ける半円形状の羽根型の突起を複数型成
したタイヤ。 【請求項2】 航空機用タイヤの両側面あるいは片側面
に、同タイヤと同一外周を有し、空気抵抗を受ける半円
形状の羽根型の突起を複数有する焼きつけ型成した物
を、接着あるいは圧着したタイヤ。 【請求項3】 上記 【請求項1】 【請求項2】の空気抵抗を受ける半円形状の羽根型の突
起の向きついては、当該航空機の機体車軸の中心から左
右のそれぞれのタイヤが空気抵抗によって当該航空機の
着陸進行方向に向かって、回転する突起構造を有するタ
イヤ。
[Claim 1] A tire in which a plurality of semicircular blade-shaped projections receiving air resistance are formed on both sides or one side of an aircraft tire. 2. Bonding or crimping a baked product having a plurality of semicircular wing-shaped projections having the same outer circumference as the tire and receiving air resistance on both side surfaces or one side surface of the aircraft tire. Tires. 3. With respect to the orientation of the semicircular wing-shaped projection receiving the air resistance according to the above [1], the respective tires on the left and right from the center of the body axle of the aircraft are caused by air resistance. A tire having a projection structure that rotates in the landing traveling direction of the aircraft.
JP2003001219U 2003-02-03 2003-02-03 Aircraft tires whose wheels automatically rotate in the landing direction before the aircraft lands. Expired - Fee Related JP3095693U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2003001219U JP3095693U (en) 2003-02-03 2003-02-03 Aircraft tires whose wheels automatically rotate in the landing direction before the aircraft lands.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2003001219U JP3095693U (en) 2003-02-03 2003-02-03 Aircraft tires whose wheels automatically rotate in the landing direction before the aircraft lands.

Publications (1)

Publication Number Publication Date
JP3095693U true JP3095693U (en) 2003-08-15

Family

ID=43249603

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2003001219U Expired - Fee Related JP3095693U (en) 2003-02-03 2003-02-03 Aircraft tires whose wheels automatically rotate in the landing direction before the aircraft lands.

Country Status (1)

Country Link
JP (1) JP3095693U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009029385A (en) * 2007-07-30 2009-02-12 Bridgestone Corp Pneumatic tire

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009029385A (en) * 2007-07-30 2009-02-12 Bridgestone Corp Pneumatic tire

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