Combustion module having substantially uniform temperature

Patent metadata

Field	Value
Publication number	US-10340434-B2
Application number	US-201615000473-A
Country	US
Kind code	B2
Filing date	Jan 19, 2016
Priority date	Jan 20, 2015
Publication date	Jul 2, 2019
Grant date	Jul 2, 2019

Abstract

A combustion module including a body in which are formed several combustion chambers extending parallel to each other along a longitudinal direction between a first end face and a second end face of the body in which they emerge, the distance between the combustion chambers and/or the dimensions of the combustion chambers are chosen so as to reduce a temperature gradient transversal to the combustion chambers.

First claim

The invention claimed is:

1. A hybrid solar system comprising:
a concentrator for concentrating solar radiation;
at least one combustion module that includes
a body having a first end face and a second end face, the combustion module being arranged such that concentrated radiation illuminates one face of the body, and
several combustion chambers formed in said body, and extending parallel to each other along a longitudinal direction between the first end face and the second end face of the body, a distance between the combustion chambers and/or dimensions of the combustion chambers being chosen so as to reduce a temperature gradient transversal to the combustion chambers, wherein

the body comprises two lateral faces and first combustion chambers situated near to the lateral faces and second combustion chambers arranged between the first combustion chambers, the first combustion chambers having a transversal cross-section greater than the second combustion chambers;
a convertor for converting thermal energy into electricity on a face opposite to that illuminated by the concentrated solar radiation; and
a controller for controlling combustion in the combustion module as a function of the concentrated solar radiation.

2. The hybrid solar system according to claim 1 , wherein a distance separating two second combustion chambers is greater than a distance separating a first combustion chamber and a second combustion chamber.

3. The hybrid solar system according to claim 1 , wherein the combustion chambers are catalytic combustion chambers.

4. The hybrid solar system according to claim 1 , further comprising at least one first connector in contact with the first end face of the body and configured to assure the connection between the combustion chambers and at least one source of at least one gas and/or a zone for evacuating combustion gases, said connector having a thermal conductivity substantially lower than that of the body.

5. The hybrid solar system according to claim 4 , further comprising a second connector in contact with the second end face of the body and configured to assure the connection between the combustion chambers and at least one source of at least one gas and/or a zone for evacuating combustion gases, said connector having a thermal conductivity substantially lower than that of the body.

6. The hybrid solar system according to claim 4 , wherein the first connector is configured to connect the combustion chambers and at least one source of at least one gas, said first connector comprising a supply orifice to be connected to a gas source by a conduit, as many channels as connection chambers, said channels connecting the supply orifice and the combustion chambers.

7. The hybrid solar system according to claim 6 , wherein each channel has a section similar to or identical to that of the combustion chamber to which it is connected.

8. The hybrid solar system according to claim 6 , wherein the first connector comprises a distribution chamber downstream of the supply orifice and upstream of the channels.

9. The hybrid solar system according to claim 4 , wherein the first connector comprises at least two inlet orifices and as many outlet orifices as combustion chambers, a distribution network for distributing gas between inlet orifices and outlet orifices, and a mixing zone situated downstream of the two inlet orifices and upstream of the distribution network.

10. The hybrid solar system according to claim 8 , wherein the first connector comprises a structure configured to favor mixing of gases.

11. The hybrid solar system according to claim 1 , wherein the body is made of SiC and a supply connector and an evacuation connector are made of zirconium oxide.

12. A The hybrid solar system according to claim 1 , further comprising a combustion device including at least one source and one conduit connected to an inlet orifice of a supply connector and to a gas source.

13. A hybrid solar system comprising:
a concentrator for concentrating solar radiation:
at least one combustion module that includes
a body having a first end face and a second end face, the combustion module being arranged such that concentrated radiation illuminates one face of the body, and
several combustion chambers formed in the body, and extending parallel to each other along a longitudinal direction between the first end face and the second end face of the body, a distance between the combustion chambers and/or dimensions of the combustion chambers being chosen so as to reduce a temperature gradient transversal to the combustion chambers, wherein

the body comprises two lateral faces and first combustion chambers situated near to the lateral faces and second combustion chambers arranged between the first combustion chambers;
a convertor for converting thermal energy into electricity on a face opposite to that illuminated by the concentrated solar radiation; and
a controller for controlling combustion in the combustion module as a function of the concentrated solar radiation, wherein
a distance between a pair of second combustion chambers is greater than a distance separating a first combustion chamber and a second combustion chamber.

14. The hybrid solar system according to claim 13 , wherein the concentrator comprises at least one mirror or Fresnel lens.

15. The combustion module according to claim 3 , wherein the catalytic combustion chamber comprises inner surfaces which are at least in part covered with at least one catalyst material configured to cause a combustion of one or more gases.

16. The hybrid solar system according to claim 1 , wherein the first combustion chambers have a diameter greater than the second combustion chambers.

Assignees

• Commissariat Energie Atomique

Inventors

• Ollier Emmanuel

Classifications

• F23B10/02

  including separate secondary combustion chambers · CPC title

• F23C9/00

  Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber (fluidised bed combustion apparatus with means for recirculation of particles entrained from the bed F23C10/02; fluidised bed combustion apparatus with devices for removal and partial reintroduction of material from the bed F23C10/26) · CPC title

• F23C3/00

  Combustion apparatus characterised by the shape of the combustion chamber · CPC title

• F23B30/00

  Combustion apparatus with driven means for agitating the burning fuel; Combustion apparatus with driven means for advancing the burning fuel through the combustion chamber · CPC title

• F23C6/00

  Combustion apparatus characterised by the combination of two or more combustion chambers {or combustion zones, e.g. for staged combustion} · CPC title