| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 101 | AIRCRAFT TIRE PRESSURE LOOP LINK | PCT/US2009037983 | 2009-03-23 | WO2009117738A2 | 2009-09-24 | LAMPING JEFF; FINEFROCK MARK |
| The aircraft tire pressure loop link is formed of first and second single metal loops connected by parallel spaced apart metal shafts, and provides for coupling a magnetic field between a wheel hub coil and a tire pressure sensor coil to provide electromagnetic communication between a control unit connect to the wheel hub coil and a tire pressure sensor connected to the tire pressure sensor coil. The current induced in the first single metal loop travels the distance from the edge of the wheel axle coil to the periphery of the of the wheel rim to the second single metal loop, which generates the flux in the tire pressure sensor receiver coil necessary to power the tire pressure sensor. | ||||||
| 102 | 공기입 타이어 | KR1020137006900 | 2011-08-12 | KR1020130039774A | 2013-04-22 | 코바야시히로노리 |
| A pneumatic tire (1) comprises: a belt layer having a pair of intersecting belts, and a circumferential reinforcement layer provided with a steel wire disposed between the intersecting belts or further inside in the tire radial direction than the intersecting belts and wound around in helical fashion while sloping within a range of ±5 [deg] with respect to the tire circumferential direction; and a tread section disposed further outside in the tire radial direction than the belt layer and used for making contact with the road surface. The tread section is assembled onto a normal rim, filled with maximum air pressure for normal internal pressure, set to a camber angle of 0°. The shape of the contact surface when 100% of normal weight is applied is 0.9 = LZ/LC = 1.0, wherein LC is the ground contact length of the equatorial surface of the tire in the tire circumferential direction, and LZ is the ground contact length in the tire circumferential direction at the end part of the circumferential reinforcement layer in the tire circumferential direction. The width of the circumferential reinforcement layer in the tire width direction is 60%-85% of the maximum ground contact width of the contact surface of the tread section in the tire width direction. | ||||||
| 103 | 항공기용 타이어 고무조성물 | KR1020070107294 | 2007-10-24 | KR100885080B1 | 2009-02-25 | 박형우 |
| A tire rubber composition for aircrafts is provided to maintain high property and to ensure excellent conductivity in the condition of high weight load and fast speed. A tire rubber composition for aircrafts comprises 100 parts by weight of raw rubber; 40~65 parts by weight of conductive carbon black which has the DBP adsorption value of 200~250 ml/100 g and the surface area 65~80 m^2/g; 4~10 parts by weight of Al2O3 as a metal oxide; 2~35 parts by weight of a plasticizer which is mixed with a first plasticizer of dibenzoylphthalate and at least one second plasticizer selected from epoxidized bean oil, chlorinated paraffin and polyester in a weight ratio of 1:9~9:1; and 10~50 parts by weight of syndiotactic-1,2-polybutadiene which has the diameter of 0.01~0.1 micrometer and the specific surface area of 80~90 m^2/g, or syndiotactic-1,2-polybutadiene which has the diameter of 1~10 micrometer and the specific surface area of 100~120 m^2/g. | ||||||
| 104 | 항공기용 타이어 트레드 고무조성물 | KR1020070023200 | 2007-03-08 | KR100807340B1 | 2008-02-28 | 조대림 |
| A tread compound for aircraft tires is provided to be superior in wear-resistant performances and heat-resistant performances. A tread compound for aircraft tires includes 30-40 parts by weight of carbon black having an iodine adsorption number of 110-120 g/kg, a DBP adsorption number of 130-140 ml/100g, and a coloring rate of 115-125 % and 20-30 parts by weight of carbon black having an iodine adsorption number of 85-95 g/kg, a DBP adsorption number of 110-120 ml/100g, and a coloring rate of 110-120% based on 100 parts by weight of a base rubber. | ||||||
| 105 | 숄더부 세퍼레이션 방지 항공기용 타이어 | KR1020030079557 | 2003-11-11 | KR1020050045478A | 2005-05-17 | 이덕주 |
| 본발명은 고하중 고속주행 높은 공기압의 항공기용 타이어에 있어서 숄더부에서 응력과 스트레스를 완화시켜 세퍼레이션 발생을 완화 및 이를 획기적으로 개선하기 위한 것인데, 종래의 경우 OH 코드 및 트레드 코드의 엣지는 타이어가 지면에 접지되는 경계부위인 OACC부에 위치됨에 따라 반복 하중에 의한 응력과 스트레스가 OACC부에 집중하여 코드 엣지와 고무간의 세퍼레이션이 발생하게 되므로, 본 발명에서는 기존의 금형을 개조 개선하여 응력을 분산시키는 방법이 아닌 기존의 금형을 그대로 사용하되 OH 코드 및 트레드 코드 끝단의 위치를 OACC하단으로 연장시키어 숄더부의 세퍼레이션을 방지하는데 그 특징이 있다. | ||||||
| 106 | 압축공기 타이어 | KR1019880007055 | 1988-06-13 | KR1019960005990B1 | 1996-05-06 | 스티븐죤돔치크 |
| 내용 없음. | ||||||
| 107 | 경량 항공기 타이어 | KR1020110055679 | 2011-06-09 | KR101770831B1 | 2017-08-23 | 우에요코기요시 |
| 공압타이어는카커스와벨트보강구조체를포함하고, 상기벨트보강구조체는, 적어도하나의반경방향내측나선층과, 상기나선층의반경방향외측에위치하는적어도하나의지그재그벨트보강구조체를갖는복합벨트구조체이다. 지그재그벨트폭은나선층의폭보다좁은것이바람직하다. | ||||||
| 108 | 지오데식 벨트를 구비한 공기압 타이어 | KR1020130157542 | 2013-12-17 | KR1020140090555A | 2014-07-17 | 우에요코기요시; 카브레라루이스안토니오; 예라슈나스로이다메르세데스; 슬라이브카존조셉; 하트제임스마이클 |
| The present invention relates to a tire having a modified geodesic belt. The ideal geodesic belt path is modified to select the centerline belt angle and to avoid excessive build up of the belt at the belt edges. The method includes the step of calculating the minimum three dimensional distance from one belt edge to the other belt edge preferably using dynamic successive approximation. | ||||||
| 109 | 공기입 타이어 | KR1020137006900 | 2011-08-12 | KR101274462B1 | 2013-06-17 | 코바야시히로노리 |
| 이 공기입 타이어(1)는, 한 쌍의 교차 벨트와, 교차 벨트 사이 혹은 교차 벨트보다도 타이어 직경 방향 내측에 배치되고, 타이어 둘레 방향에 대하여 ±5[deg]의 범위 내에서 경사하면서 나선상(螺旋狀)으로 감아 돌려진 스틸 와이어를 구비하는 둘레 방향 보강층을 가지는 벨트층과, 벨트층보다도 타이어 직경 방향 외측에 배치되고, 노면(路面)과 접지(接地)하는 트레드부를 구비한다. 트레드부는, 정규 림에 림 끼움하여, 정규 내압의 최대 공기압을 충전하고, 캠버각을 0°로 하여, 정규 하중의 100%를 걸리게 하였을 때의 접지면의 형상이, 타이어 적도면에 있어서의 타이어 둘레 방향의 접지 길이를 LC로 하고, 상기 둘레 방향 보강층의 타이어 폭 방향의 단부(端部)에 있어서의 타이어 둘레 방향의 접지 길이를 LZ로 한 경우, 0.9≤LZ/LC≤1.0이고, 둘레 방향 보강층은, 타이어 폭 방향의 폭이 트레드부의 접지면의 타이어 폭 방향의 최대 접지 폭의 60% 이상 85% 이하이다.
|
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| 110 | 경량 항공기 타이어 | KR1020110055679 | 2011-06-09 | KR1020110135817A | 2011-12-19 | 우에요코기요시 |
| PURPOSE: A light aircraft tire is provided to ensure light weight and be used under high speed and load conditions. CONSTITUTION: A light aircraft tire comprises carcass(22) and a belt reinforcing structure. The belt reinforcing structure comprises first and second belt layers, and a zigzag belt reinforcing structure. The first and second belt layers comprise cords, which are arranged on the middle circumferential surface at an angle or 5° or less. The belt reinforcing structure is located on the outside of the radial direction of the first belt layer. The belt reinforcing structure forms two layers of cords, and the cord slopes to the central surface of a tire extended alternately from each transversal edge to a return point by 5°. | ||||||
| 111 | 항공기 착륙바퀴 회전장치. | KR1020030063856 | 2003-09-15 | KR1020030076556A | 2003-09-26 | 이두원 |
| PURPOSE:A rotating device of landing wheels in an airplane is provided to extend the life of tires by rotating the landing wheels in an advancing direction, to reduce the air pollution by preventing the smoke and to prevent the separation of the landing wheels and to reduce the maintenance cost by minimizing the sticking of a tire material on the surface of a runway. CONSTITUTION:A rotating device of a landing wheel is formed in a streamline and vertically installed to be protruded in the side of the wheel. The wheel is driven in the back of the rotating device to receive smaller air resistance during landing an airplane. | ||||||
| 112 | 공기 타이어 | KR1019890001564 | 1989-02-11 | KR1019960015014B1 | 1996-10-24 | 토마스니콜라스허버트웰터 |
| 내용없음. | ||||||
| 113 | 공기 타이어 | KR1019850006024 | 1985-08-21 | KR1019920005419B1 | 1992-07-03 | |
| 내용 없음. | ||||||
| 114 | 飞机轮胎 | CN01236180.1 | 2001-03-29 | CN2468898Y | 2002-01-02 | 韩保禄 |
| 本实用新型为一种飞机轮胎。它在现有飞机轮胎胎体两侧分别设计至少两个突起的风耳,而风耳的一个侧面带有内凹结构,胎体两侧风耳上内凹结构的方向一致。利用本实用新型上的风耳能够在飞机着陆前使轮子转动起来,使轮子的转速等于或大于飞机与跑道相对运动的速度,即轮速与接地速度一致,消除轮子与跑道之间的速度差,由滑动摩擦变成滚动摩擦,从而大大减轻对轮胎的磨损,延长轮胎的使用寿命。 | ||||||
| 115 | THERMAL MITIGATION FOR TIRE PRESSURE MEASUREMENT ELECTRONICS | PCT/US2013048865 | 2013-07-01 | WO2014011426A3 | 2015-07-16 | SMITH GARY THOMAS |
| A thermal pressure measurement assembly coupled to a rim of an aircraft wheel. A housing is configured to be fastened to a wheel face. An electronics enclosure is positioned in the housing. Electronics are positioned in the electronics enclosure and configured to process a signal received from a remote sensor that measures tire pressure and temperature. Internal insulation is positioned in an interior of the housing. The internal insulation is configured to reduce the temperature of the electronics sufficiently to permit use of low temperature electronics rated to 125 degrees C. | ||||||
| 116 | SYSTEM AND METHOD TO ASSESS AND REPORT THE HEALTH OF LANDING GEAR RELATED COMPONENTS | PCT/US2011030150 | 2011-03-28 | WO2012021179A3 | 2012-04-12 | FOLLOWELL DAVID A; MAGGIORE JEANNE C; MAJKOWSKI WAYNE R |
| The different advantageous embodiments provide an apparatus comprising a number of landing gear components (310) for a vehicle, a number of systems (314), and a number of processor units (308). The number of systems is configured to generate data about the number of landing gear components and the vehicle. The number of processor units is configured to monitor the data and manage health of the number of landing gear components. | ||||||
| 117 | PNEUMATIC RADIAL TIRE, AND METHOD OF PRODUCING THE SAME | PCT/JP0300661 | 2003-01-24 | WO03061991B1 | 2003-10-23 | YANO TAKESHI; MORI HIROYUKI; NAKAMURA MASAAKI; ITAI SEIJI |
| With the pneumatic tire of the invention, the overall strength (KO) of a belt layer (20) peripherally of the tire per unit width at the tire equatorial plane position (PO) is set at a value greater than that of the overall strength of the belt layer (20) peripherally of the tire per unit width at a width position (P2) that is 2/3 of the maximum width of the belt layer with the tire equatorial plane (CL) as the center, thereby making it possible to suppress the amount of peripheral elongation of the tread rubber in the middle region of the tread and to suppress the radial growth of the tire during the filling of standard inner pressure and during high speed rotation while suppressing the amount of use of material for the belt layer (20). Suppression of the amount of peripheral elongation of the tread rubber results in decreasing the degree of stretching of the rubber, thus making it possible to increase the resistance of the tread to the sticking or the like of foreign objects in the tread and to suppress the growth of cracks even in the event that a foreign object sticks in the tread. | ||||||
| 118 | HEAVY-DUTY PNEUMATIC TIRE | PCT/JP2010058359 | 2010-05-18 | WO2010134523A9 | 2011-12-22 | KATSUBE YOSHIHIRO |
| A heavy-duty pneumatic tire is provided in which it is possible to prevent cracks (including cracks generating from the joint) from generating in the rubber portions that come into contact with the rim flanges during the period from no load to a high load when the tire has been inflated to a proper air pressure, and which can hence have greatly improved durability. The heavy-duty pneumatic tire has a rubber chafer (8) disposed in at least the area of each bead portion (1) which comes into contact with the rim, and is configured so that the rubber chafer (8) is formed from a rubber composition comprising: 100 parts by mass of a rubber component comprising 45-55 parts by mass of butadiene rubber having 10-30 parts by mass of polybutadiene rubber containing a syndiotactic 1,2-structure and 45-55 parts by mass of natural rubber; and 50-60 parts by mass, excluding 50 and 60 parts by mass, of carbon black having a DBP of 85-115 mL/100 g and an N2SA of 50-100 m2/g. | ||||||
| 119 | A WIRELESS TIRE PRESSURE AND/OR WHEEL SPEED SENSING SYSTEM FOR AIRCRAFT | PCT/US2004027443 | 2004-08-24 | WO2005043264A3 | 2006-03-02 | BUENZ MARK J; NORLIEN JOHN A; KUNIK WILLIAM G; WILLIAMS WADE W; MYHRE DOUGLAS C |
| A wireless tire pressure sensing system for an aircraft comprises: dual resonant circuits mounted to a wheel of the aircraft, each resonant circuit comprising: a variable capacitance sensor (16) and a wire loop (12) of a predetermined inductance coupled thereto, one capacitance sensor for monitoring the pressure of a tire mounted to the wheel, and the other capacitance sensor operative as a reference to the one capacitance sensor; an interrogating circuit (18) magnetically coupleable to the dual resonant circuits and operative to induce magnetically a variable frequency current in the dual resonant circuits, the one resonant circuit responding to the induced current with an E-field signal at a first resonant frequency commensurate with the capacitance of the one sensor, and the other resonant circuit responding to the induced current with an E-field signal at a second resonant frequency commensurate with the capacitance of the other sensor; a receiving circuit (20) E-field coupleable to the dual resonant circuits and operative to receive the E-field signals at the first and second resonant frequencies and to generate first and second signals representative thereof; and a processing circuit coupled to the receiving circuit for processing the first and second signals to generate a compensated pressure reading of the tire. The pressure sensing system may be modified to provide and/or include wheel speed sensing. | ||||||
| 120 | AIRCRAFT TYRE WITH IMPROVED TYRE BEAD | PCT/EP0107223 | 2001-06-25 | WO0200456A3 | 2002-05-10 | HERBELLEAU YVES; GUERINON BERNARD; ROUX PIERRE |
| The invention concerns an aircraft tyre whereof the inflating pressure is higher than 12 bars, comprising a crown, two sidewalls and two beads, a carcass reinforcement anchored in the two beads and a crown reinforcement, wherein the carcass reinforcement comprises at least two circumferential alignments of first reinforcing elements with high modulus of elasticity and wherein the anchoring means of the first reinforcing elements in each bead comprise second circumferentially oriented reinforcing elements axially bordering the circumferential alignments of the first reinforcing elements, the first and second reinforcing elements being separated by a layer of a mixture with very high modulus of elasticity. | ||||||
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