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公开(公告)号:US09821609B2
公开(公告)日:2017-11-21
申请号:US14783436
申请日:2014-04-02
Applicant: BRIDGESTONE CORPORATION
Inventor: Takeshi Yano
CPC classification number: B60C11/0327 , B60C11/042 , B60C11/1353 , B60C11/1369 , B60C2011/0341 , B60C2011/0355 , B60C2011/1361 , B60C2200/02
Abstract: An object is to, in an aircraft tire, promote heat dissipation from circumferential direction grooves of a tread and improve durability of the tire. Plural circumferential direction grooves (central side circumferential direction grooves (14), edge portion side circumferential direction grooves (16)) that extend in a tire circumferential direction are formed in a tread (12). In a tire circumferential direction cross-section, a groove bottom (18) of at least one of the circumferential direction grooves has a wave shape having amplitude in a tire radial direction.
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2.
公开(公告)号:US11519824B2
公开(公告)日:2022-12-06
申请号:US16771487
申请日:2018-12-13
Applicant: BRIDGESTONE CORPORATION
Inventor: Shoji Oida , Naoto Okazaki , Takeshi Yano , Tomotaka Sakiyama
Abstract: A wear amount estimation device estimates plural kinds of wear energy depending on each of an internal pressure of aircraft tires, a load acting on the aircraft tires, a velocity of an aircraft, a slip angle caused in the aircraft tires, and a braking force of the aircraft, in accordance with each of these elements and wear energy EFR of the aircraft tires in a state of a free rolling run The wear amount estimation device estimates the wear amount wear of the aircraft tires in accordance with each of the calculated wear energy and a wear resistance R indicating a relationship between predetermined wear energy and a predetermined wear amount.
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