Instrumented plate for oven

1 . An instrumented plate intended for the monitoring of a refractory part of a furnace, the instrumented plate comprising:

a support plate through which a plurality of orifices pass and which is at least partially made of a material of fibers interconnected by a ceramic matrix, referred to as “ceramic-matrix composite”, or of a precursor of said ceramic-matrix composite;

a sensor borne by said support plate,

the ceramic-matrix composite precursor being a material which is capable of transforming into said ceramic-matrix composite under the effect of heating.

2 . The instrumented plate as claimed in claim 1 , wherein

each of said orifices has an equivalent diameter greater than 3 mm and/or less than 50 mm; and

the percentage of perforation, equal to the ratio of

the cumulative surface area of the orifices, or “perforated surface area”, to

the surface area of the support plate, said surface area including the perforated surface area,

is greater than 5% and less than 95%, and

the sensor is a sensor for measuring an optical, electrical or acoustic signal, and

the support plate has a thickness of between 1 and 20 mm.

3 . The instrumented plate as claimed in claim 2 , wherein said percentage of perforation is greater than 50%.

4 . The instrumented plate as claimed in claim 1 , wherein the orifices are evenly distributed in at least one perforated zone of the support plate.

5 . The instrumented plate as claimed in claim 4 , wherein the support plate has several of said perforated zones and at least one reinforcing zone separating two of said perforated zones, the reinforcing zone having a width greater than the largest dimension of said orifices.

6 . The instrumented plate as claimed in claim 1 , wherein the sensor is

embedded within the ceramic-matrix composite or the precursor of said ceramic-matrix composite, or

integrated in the arrangement of fibers of the ceramic-matrix composite or of the precursor of said ceramic-matrix composite, or

accommodated in a recess formed or inserted in the ceramic-matrix composite or the precursor of said ceramic-matrix composite, or

attached to a large face of the support plate.

7 . The instrumented plate as claimed in claim 1 , wherein the ceramic-matrix composite or the ceramic-matrix composite precursor comprises a plurality of superposed textiles, one or more identical or different sensors being inserted between two of said textiles.

8 . The instrumented plate as claimed in claim 1 , wherein

the fibers represent more than 25% and less than 70% of the volume of the ceramic-matrix composite, and

the ceramic-matrix composite comprises, in percentage by mass, more than 80% of one or more of the following oxides or non-oxides: Al 2 O 3 , ZrO 2 , HfO 2 , Cr 2 O 3 , MgO, CaO, SiO 2 , SiC, Si 3 N 4 , SiAlON, AlN, Si 2 ON 2 , BN, B 4 C, silicon oxycarbide, MoSi 2 , and carbon C.

9 . The instrumented plate as claimed in claim 1 , wherein the ceramic-matrix composite has a resistance to compressive crushing of greater than 5 MPa, and/or a thermal conductivity between 20° C. and 500° C. of greater than 2.0 W·m −1 ·K −1 .

10 . A measuring device comprising the instrumented plate as claimed in claim 1 and a measuring appliance communicating with the sensor so as to receive and interpret a signal emitted by the sensor.

11 . A furnace selected from a glass melting furnace, a metallurgical furnace, an incinerator, a gasifier, a combustion chamber for energy generation, and a gas reforming installation for the chemical industry, said furnace comprising:

the refractory part, and

the measuring device as claimed in claim 10 , the instrumented plate of the measuring device being disposed in contact with one face of the refractory part.

12 . The furnace as claimed in the claim 11 , wherein the refractory part has a face configured to be at a temperature greater than 800° C., referred to as hot face, and a face facing away from said hot face, referred to as cold face, said one face of the refractory part being said cold face, the instrumented plate being disposed in contact with said cold face.

13 . The furnace as claimed in claim 11 , wherein the coefficient of thermal expansion of the ceramic-matrix composite is equal to that of the material of the refractory part plus or minus 20%.

14 . The furnace as claimed in claim 11 , wherein the instrumented plate is attached to the refractory part so as to not exert thermomechanical stresses on the refractory part under the effect of a dimensional modification of the refractory part resulting from normal operation of the furnace.

15 . The furnace as claimed in claim 11 , wherein the surface area of the instrumented plate represents more than 20% of the surface area of the face of the refractory part to which it is applied.

16 . The furnace as claimed in claim 11 , wherein the refractory part is selected from the following:

a throat lintel or block,

a soldier block,

a refractory brick or sidewall block,

a corner block,

a tuckstone,

a paving tile or pavement,

a crown brick or beam,

a tuyere surround brick or block,

a brick for a tapping hole or spout,

an electrode block,

an injector block,

a refractory spout-lip for a glass furnace,

a block for an injector,

a glass furnace throat,

a component for a heat exchanger of the furnace,

a refractory tile or plate for a boiler lining,

a protective shell for a heater tube for an incinerator,

a tile of an incinerator,

a ceramic component for a solar absorber,

a protective component or tile for a turbine combustion chamber,

a block or surround for a tuyere or a burner.

17 . The furnace as claimed in claim 11 , wherein the measuring device uses the signal it receives from the sensor to provide information relating to

the thickness of the refractory part, or

the mean temperature in the furnace, or

the physical state of the refractory part.