摘要:
A pneumatic tire having a carcass (22) and a belt reinforcing structure (40) is disclosed. The belt reinforcing structure (40) comprises a reinforcement strip (43) comprising at least two reinforcement cords (44, 46) aligned in parallel relationship, wherein a second cord (44) is located next to a first cord (46) and wherein the second cord is made of a different material than the first cord. In one aspect, the belt reinforcing structure (40) comprises a zigzag belt reinforcing structure (70) formed of said reinforcement strip (43), the reinforcement strip being inclined at 5 to 30 degrees relative to the centerplane of the tire (10) extending in alternation to turnaround points at each lateral edge.
摘要:
Landing gear tire pressure sensing systems, methods and apparatuses are provided. In various embodiments, a tire pressure sensing system may be mounting to a landing gear. The system may comprise a rotating portion 240 and a stationary portion 250. The rotating portion and stationary portion may be in electronic communication. The stationary portion may be configured to communicate an indication of tire pressure to a control unit.
摘要:
The invention relates to an aircraft tire (1) including: two beads (2), each intended to come into contact with a rim (3) via at least one radially inner bead surface (4); and a carcass reinforcement (5) including at least one carcass layer (6) that connects the two beads (2), each carcass layer (6) being wound inside each bead (2) around a bead wire (7) having a central meridian section (O). In each bead (2), a portion (8) for clamping under the bead wire extends radially inside a portion (5) of the carcass reinforcement, located radially inside the bead wire (7), as far as the radially inner bead surface (4). The portion (8) for clamping under the bead wire includes a surface layer (9) intended to come into contact with the rim (3) via the radially inner bead surface (4), said layer having a shear stiffness K 1 . The inventors aim to reduce the speed at which critical defects or "pits" form on the rim seat, so as to extend the life of the rim and thus increase the number of use cycles prior to its removal from service. According to the invention, the portion (8) for clamping under the bead wire includes: a rigid layer (10) located radially outside and adjacent to the surface layer (9) and having a shear stiffness K 2 at least equal to five times the shear stiffness K 1 of the surface layer (9); and a deformable layer (11) that is located radially outside and adjacent to the rigid layer (10) and radially inside and adjacent to the carcass reinforcement portion (5) which is radially inside the bead wire (7), said deformable layer having a shear stiffness K 3 at most equal to 0.3 times the shear stiffness K 1 of the surface layer (9).
摘要:
Tire treads, especially tire treads for aircraft or for heavy vehicles, formed from a material that is based upon a cross-linkable rubber composition, the cross-linkable rubber composition comprising, per 100 parts by weight of rubber, between 40 phr and J 00 phr of a polyisoprene rubber, between 0 and 60 phr of a highly unsaturated diene rubber and between 1 phr and 25 phr of a polylerpene resin having a glass transition temperature of between 50° C. and 120° C. The rubber composition further includes between 0.1 phr and 10 phr of a poly-thiosulfate anti-reversion agent having the formula: MO3S—S—X—S—SO3M wherein X is an alkylene radical or a radical comprising two or more alkylene units, pairs of which units being linked through an oxygen or a sulfur atom, through a group SO2—, —NH—, —NH2+—, —NlC1-16alkyl)- or —COO—, or through an arylene or cycloalkylene radical and M is a metal.
摘要:
A tire (100) having a circumferential tread (102), at least one belt (132a-f), an inner liner, a pair of sidewalls (104), and at least three carcass plies (114, 116, 118). The tire (100) includes a pair of bead portions (106), each including a bead core (108), a bead filler (110), a flipper, a chafer, and a gum strip. The at least three carcass plies (114, 116, 118) extend radially downward, inward of the bead filler (110), extend around the bead core (108), and continue upward, outward of the bead filler (110) and terminate in at least three turn-up ends (126, 128, 130). At least one of the turn-up ends does not contact at least one of the radially downward extending carcass plies, the flipper, or the bead filler (110) in one of the sidewalls (104), and at least two of the turn-up ends contact at least one of the radially downward extending carcass plies, the flipper (204), or the bead filler (110, 308, 408, 508, 608) in one of the sidewalls (104, 304, 404, 504, 604).
摘要:
A pneumatic tire (10) having a carcass (22) comprising at least two inner plies (1, 2, 3, 4) is disclosed. At least two if the inner plies (1, 2, 3, 4) is wound about an annular bead member (14) from axially inside of the annular bead member (14) toward axially outside thereof and extends radially outward towards a tread portion (20) of the tire (10) forming a respective turnup portion (2', 3', 4'). At least one of the inner plies (1) has a terminal end (1') which has a radial location in a zone (B) between a first plane (28) and a second plane (29), wherein the first plane (28) is tangent to the outer radial surface of the annular bead member (14) and parallel to the axis of rotation of the tire (10), and wherein the second plane (29) is parallel to the first plane (28) and tangent to the radial inner surface of the annular bead member (14). Preferably, the tire (10) is an aircraft tire such as a radial aircraft tire.
摘要:
A passive RFID transponder sensor system includes a sensor assembly having a focused field transponder antenna with a highly magnetically permeable transponder antenna stem, and a reader antenna with an electrical reader coil generating a magnetic field having magnetic flux extending between the reader antenna and a sensor assembly. The electrical transponder coil and the electrical reader coil are coupled by the magnetic field, so that information can be transferred to and from the sensor assembly through the magnetic field by which the electrical transponder coil and the electrical reader coil are coupled.
摘要:
A pneumatic tire having a carcass (22) comprising at least two inner plies (1, 2, 3, 4) is disclosed. At least one inner ply (1, 2, 3, 4) is wound about an annular bead member (14) from axially inside of the annular bead member (14) toward axially outside thereof and extends radially outward towards a tread portion (20) of the tire (10) forming a respective turnup portion (1', 3', 4'). Furthermore, at least one of the inner plies (2) has a terminal end (2') which has a radial location in a first zone (C) defined by a first plane (28) and a second plane (29), wherein the first plane (28) is tangent to the outer radial surface of the annular bead member (14) and parallel to the axis of rotation of the tire (10), wherein the second plane (29) is perpendicular to the first plane (28) and extends through the center of the annular bead member (14), and wherein the first zone (C) is located radially inward of the first plane (28) and axially outward of the second plane (29). Preferably, the tire (10) is an aircraft tire.
摘要:
The invention relates to a pneumatic tire having a carcass (22) and a belt reinforcing structure (40), the belt reinforcing structure (40) comprising a first and a second belt layer (50,60). One or both of the first and a second belt layers (50,60) have cords arranged at an angle of 5 degrees or less with respect to the midcircumferential plane of the tire (10). The belt reinforcing structure (40) further comprises a zigzag belt reinforcing structure (70) comprising cords inclined at an angle in a range of from 5 to 30 degrees relative to the midcircumferential of the tire extending in alternation to turnaround points at lateral edges (44,45) of the zigzag belt reinforcing structure (70), wherein the axial width of the zigzag belt reinforcing structure (70) is wider than the axial width of the first and second belt layer (50,60).