http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2010212802-A1

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classificationCPCAdditional http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B60C2200-02
classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B60C9-2009
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B60C9-04
filingDate 2008-04-17-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_5e612566c31ad46778a8371c94f3c770
publicationDate 2010-08-26-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber US-2010212802-A1
titleOfInvention Radial tire for aircraft
abstract This invention provides a radial tire for aircraft comprising a belt composed of a plurality of belt layers, wherein a total strength of the belt T belt [N] in a circumferential direction over its full width satisfies T belt /WD≧1.5×10 6 in which D [m] is an outer diameter of the tire and W [m] is a width of the tire, the belt is composed of at least two belt layers each containing organic fiber cords with an elongation in an extension direction under a load of 3.2 cN/dtex of 2.2-9.3%, a protection belt layer having a circumferential stiffness lower than that of the belt is disposed at an outside of the belt in a radial direction, a ratio of the circumferential stiffness of the protection belt layer to the circumferential stiffness of the belt is less than 0.5, and the protection belt layer is composed of organic fiber cords having a tensile strength at break of not less than 6.3 cN/dtex and a heat shrinkage factor of 0.5-5.0%, whereby a durability of a tread portion can be improved without damaging an excellent durability against foreign matters.
isCitedBy http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9290056-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2014373992-A1
priorityDate 2007-05-16-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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