Heat-resistant product
A process is provided for a heat-resistant product that has a support chosen from a glass fiber and an assembly of glass fibers, and a coating extending over the outer surface of said support, in a zone called the “protected zone.” The coating has particles having a mean size of less than 100 nm and has more than 95% by mass of Al 2 O 3 and/or ZrO 2 , referred to as “protective particles.” The protective particles cover more than 50% and less than 90%of the protected zone, as percentage by surface area. The process includes the step of subjecting the heat-resistant product to a temperature of greater than 600° C. for a duration of greater than 0.5 hours.
1 . A process in which a heat-resistant product having:
a support chosen from a glass fiber and an assembly of glass fibers, and
a coating extending over the outer surface of said support, in a zone called the “protected zone”, said coating comprising particles having a mean size of less than 100 nm and comprising more than 95% by mass of Al 2 O 3 and/or ZrO 2, referred to as “protective particles”, the protective particles covering more than 50% and less than 90% of the protected zone, as percentage by surface area, wherein said process comprises the step of
subjecting said heat-resistant product to a temperature of greater than 600° C. for a duration of greater than 0.5 hours.
2 . The process as claimed in claim 1 , wherein the support is in the form of an optical fiber, a single yarn, an assembled yarn, a felt, a web, a knit, a ribbon, a braid or a woven fabric.
3 . The process as claimed in claim 2 , wherein the support is in the form of a woven fabric including a network of parallel warp yarns and weft yarns transversely crossing said network, at least some of the warp and/or weft yarns being heat-resistant products as claimed in either of the preceding claims .
4 . The process as claimed in claim 1 , wherein the glass fibers constituting the support is a material having an SiO 2 content of greater than or equal to 55%, as percentage by mass based on the oxides.
5 . The process as claimed in claim 4 , wherein the glass fibers constituting the support is a material having, as percentages by mass based on the oxides:
an SiO 2 content of greater than 90% and an Al 2 O 3 content of greater than 0.1% and less than 5%, oxides other than SiO 2 and Al 2 O 3 constituting the remainder to 100%, or
an SiO 2 content of less than 79.9%, an Al 2 O 3 content of greater than 12.5% and less than 32%, and an MgO content of greater than 4% and less than 20%, oxides other than SiO 2, Al 2 O 3 and MgO constituting the remainder to 100%, or
an SiO 2 content of greater than 99.9%.
6 . The process as claimed in claim 1 , wherein the total surface area of the interstices present in the protected zone between the protective particles and having a size of greater than 250 nm represents less than 50% of the total surface area of the interstices of said protected zone, as percentage by surface area.
7 . The process as claimed in claim 1 , wherein the protected zone represents more than 50% of the outer surface area of the support.
8 . The process as claimed in claim 1 , wherein the protective particles cover more than 75% and/or less than 85% of the protected zone, as percentage by surface area.
9 . The process as claimed in claim 1 , wherein the coating comprises, as percentage by mass based on the total mass of the coating, more than 60% protective particles.
10 . The process as claimed in claim 1 , wherein the mean size of the protective particles is greater than 10 nm and less than 70 nm.
11 . The process as claimed in claim 1 , wherein the coating comprises a dry binder comprising
an organic film former in an amount, as percentage by mass based on the mass of the coating, of greater than 0.3% and less than 57%, and/or
an organic coupling agent in an amount, as percentage by mass based on the mass of the coating, of greater than 0.1% and less than 35%, and/or
an organic constituent other than the film former and the coupling agent and chosen from a lubricant, a surfactant, an emulsifier, a wetting agent and mixtures thereof, in an amount, as percentage by mass based on the mass of the coating, of greater than 0.05% and less than 34%.
12 . The process as claimed in claim 1 , the heat-resistant product comprising a layer at least partially covering the coating, said layer comprising one or more materials chosen from:
a polyvinyl alcohol,
a paraffin,
a polytetrafluoroethylene,
a polymethyl methacrylate,
a polyurethane,
a latex,
a resin,
an organic material capable of constituting a dry binder of said coating,
when the coating comprises a dry binder.
13 . The process as claimed in claim 1 , wherein the heat-resistant product is manufactured according to a process comprising the following steps 1) to 3):
1) preparing the support and a suspension comprising a liquid binder and the protective particles;
2) applying said suspension to the support;
3) drying so as to transform the suspension into a coating having a solid form.
14 . The process as claimed in claim 1 , wherein the heat-resistant product is disposed so as to serve
as a heat shield, in particular
of a drive shaft,
of an engine attachment harness,
of an insulation element of an engine
of an actuating cylinder,
of a pipe,
of a system for attachment of said pipe,
of a cable,
of a conveying roller,
of a system for attaching and driving said rollers,
of a nacelle of an engine,
of an engine,
of a suspension structure of an engine
of a thrust reverser
of a fluid supply element of an engine
of a tube in which a fluid circulates
of a seal,
of a valve;
as a sensor, the support being an optical fiber.
15 . The process as claimed in claim 14 , wherein
the drive shaft is a drive shaft of a land vehicle, aircraft or helicopter engine,
the insulation element is an insulation casing of an engine,
the cable is an electric cable or a thermocouple cable,
the conveying roller is for conveying glass sheets,
the nacelle is a nacelle of an aircraft engine,
the heat-resistant product is disposed so as to serve as a heat shield of an engine in a land vehicle, aircraft, helicopter or space rocket engine,
the suspension structure is struts of an aircraft or helicopter engine,
the thrust reverser is a thrust reverser in an aircraft engine,
the fluid supply element of a space rocket engine,
the tube is a tube in which a heat transfer fluid circulates in a reactor,
the optical fiber incorporates at least one Bragg grating.