Provided is a pneumatic tire. A transponder is embedded on an outer side in a tire width direction of a carcass layer, and the tan δout (−20° C.) at −20° C. of a rubber member having the largest storage modulus at 20° C. of rubber members located on the outer side in the tire width direction of the transponder is in the range of from 0.1 to 0.7. Further, the transponder is embedded on the outer side in the tire width direction of the carcass layer, and the tan δin (−20° C.) at −20° C. of a rubber member having the largest storage modulus at 20° C. of rubber members located on an inner side in the tire width direction of the transponder is in the range of from 0.1 to 0.7.

Provided are an RFID (radio frequency identification) module and a pneumatic tire in which the RFID module is embedded. An RFID module includes an IC (integrated circuit) substrate that stores data, an antenna that transmits and receives data, and a covering layer that covers the antenna. The covering layer contains calcium carbonate, and a relative dielectric constant of the covering layer is 7 or less.

A pneumatic tire is provided. A transponder is embedded in an outer side of a carcass layer in a tire width direction, a rubber member having a largest storage modulus at 20° C. of rubber members located on an outer side of the transponder in the tire width direction has a storage modulus at 0° C. E′out(0° C.) and a storage modulus at −20° C. E′out(−20° C.) that satisfy a relationship 0.50≤E′out(0° C.)/E′out(−20° C.)≤0.95, and a rubber member having a largest 20° C. storage modulus of rubber members located on an inner side of the transponder in the tire width direction has a storage modulus at 0° C. E′in(0° C.) and a storage modulus at −20° C. E′in(−20° C.) that satisfy a relationship 0.50≤E′in(0° C.)/E′in(−20° C.)≤0.95.

Provided is a pneumatic tire. A transponder is embedded in an outer side in a tire width direction of a carcass layer, the transponder is covered by a covering layer, and a storage modulus E′c at 20° C. of the covering layer and a storage modulus E′out at 20° C. of a rubber member having the largest storage modulus at 20° C. of rubber members located on an outer side in the tire width direction of the transponder satisfy the relationship 0.1≤E′c/E′out≤1.5. Further, the storage modulus E′c at 20° C. of the covering layer and a storage modulus E′in at 20° C. of a rubber member having the largest storage modulus at 20° C. of rubber members located on an inner side in the tire width direction of the transponder satisfy the relationship 0.03≤E′c/E′in≤1.50.

Provided is a pneumatic tire. A transponder is embedded in an outer side in a tire width direction of a carcass layer, the transponder is covered by a covering layer, and a storage modulus E′c at 20° C. of the covering layer and a storage modulus E′out at 20° C. of a rubber member having the largest storage modulus at 20° C. of rubber members located on an outer side in the tire width direction of the transponder satisfy the relationship 0.1≤E′c/E′out≤1.5. Further, the storage modulus E′c at 20° C. of the covering layer and a storage modulus E′in at 20° C. of a rubber member having the largest storage modulus at 20° C. of rubber members located on an inner side in the tire width direction of the transponder satisfy the relationship 0.03≤E′c/E′in≤1.50.

Provided is a pneumatic tire that can provide improved transponder durability while ensuring tire durability. The pneumatic tire includes: a tread portion (1) extending in a tire circumferential direction and having an annular shape; a pair of sidewall portions (2) disposed on both sides of the tread portion (1); and a pair of bead portions (3) disposed on an inner side in a tire radial direction of the sidewall portions (2). The tire is embedded with a transponder (20) covered with a covering layer (23). A glass transition temperature (Tg) of the covering layer (23) is in a range of from −70° C. to −45° C.

An aircraft tire has a pair of bead sections, sidewall sections extending from the bead sections, and a tread section extending between the sidewall sections; the aircraft tire includes an RFID tag having a tag main body (IC chip) configured to store information about the aircraft tire, and an antenna extended from the tag main body, wherein, in a tread surface view, the antenna is disposed such that an extending direction of the antenna is parallel to a tire width direction or intersects the tire width direction within a predetermined angle range, and the aircraft tire satisfies a configuration 0.1<L/W<0.2, where a width of the aircraft tire is denoted as “W” and a total length of the antenna in the extending direction of the antenna is denoted as “L”, and when a diameter of the aircraft tire is 21 inches or more.

An aircraft tire has a pair of bead sections, sidewall sections extending from the bead sections, and a tread section extending between the sidewall sections; the aircraft tire includes an RFID tag having a tag main body (IC chip) configured to store information about the aircraft tire, and an antenna extended from the tag main body, wherein, in a tread surface view, the antenna is disposed such that an extending direction of the antenna is parallel to a tire width direction or intersects the tire width direction within a predetermined angle range, and the aircraft tire satisfies a configuration 0.1<L/W<0.2, where a width of the aircraft tire is denoted as “W” and a total length of the antenna in the extending direction of the antenna is denoted as “L”, and when a diameter of the aircraft tire is 21 inches or more.

This disclosure provides a tire formed of a body having multiple plies and a tread that surrounds the body. The plies and/or the treads and/or other surfaces of the tire include one or more resonators that respond to being interrogated by an externally generated excitation signal. Multiple resonators formed of electrically-conducting materials are disposed (e.g., printed) on the plies and/or tread and/or other surfaces of the tire. Each of a group of multiple resonators can be individually configured to respond to different frequencies of the excitation signal such that the presence of a response (e.g., a measured attenuation of the excitation signal return) or lack of response (e.g., based on comparison of the excitation signal return to calibration curves) from individual ones of the multiple resonators can be combined to form a serial number that is unique to the tire or other elastomer-containing component (e.g., belts, hoses, etc.) being interrogated.

An aircraft tire has a pair of bead sections, sidewall sections extending from outer side in a radial direction of the bead sections, and a tread section extending between the sidewall sections; the aircraft tire includes an RFID tag having a tag main body (IC chip) configured to store an information about the aircraft tire and an antenna extended from the tag main body, wherein, when a diameter size of the aircraft tire is 15 inches or less, in a tread surface view, the antenna is disposed such that the antenna is parallel to a tire circumferential direction or intersects the tire circumferential direction within a predetermined angle range, and a belt part disposed in the tread section is made of non-metal material.