the given invention , to be described in more detail below , provides for a radiant gas burner which improves the quality of gas mixture combustion , reduces nitric oxide and carbonic oxide content in the combustion products , and increases the burner &# 39 ; s efficiency owing to more uniform air - gas mixture flow . the mixture can be introduced tangentially into the casing and allowed to flow through a gas dissector , the gas dissector increases uniformity of the air - gas mixture flow . additionally , the gas dissector acts as a shield to catch backscattered emission and as a heat exchanger to heat the air - gas mixture at the same time . the design of the radiant gas burner described in detail below , assures reliable automatic ignition owing to the location of the apertures available in the burner &# 39 ; s casing and the gas dissector . location of emitter meshes is also an important improvement of the radiant gas burner . in one embodiment a lower and an upper mesh can be arranged so that a combustion zone is a biconvex lens . part of the ir radiation from the lower and upper meshes is focused onto an inter - mesh zone of combustion , intensifying the latter . the result is that gas combustion quality increases and carbonic oxide content in the combustion products decreases . in another embodiment , the meshes can be disposed in such a way that the combustion zone forms a convex - concave lens , whereas both meshes are placed with a convex side facing the air - gas mixture flux . referring to fig1 - 5 , where the components of a radiant gas burner to combust gas fuel are therein provided , including a casing with an aperture to ignite air - gas mixture , an air - gas mixer connected to the casing , and a gas dissector installed in the casing generally transverse to air - gas mixture flux . the gas dissector can be a grid including ribs having an inclination of about 50 - 60 ° relative to a plane transverse to a central axis a . the edges of adjacent ribs can be in the same plane perpendicular to that of a grid . the ribs can be in the form of flat or punched plates , or concentric cone rings . the radiant gas burner also includes a metallic - mesh emitter installed in the casing thereof generally perpendicular to the air - gas mixture flux . the emitter accommodates at least lower and upper meshes downstream from the air - gas mixture motion , and can include different sized mesh openings . the emitter meshes can be installed into the casing thereof so that they form an inner cavity in the form of a lens . the lens form can have a curvature radius of at least the burner &# 39 ; s diameter and can have a thickness of at least 8 - 10 times the size of the lower mesh openings . in addition , the upper and lower meshes of the emitter can form a biconvex or convex - concave lens . to facilitate automatic ignition of the air - gas mixture , a first aperture in the casing can be provided between the upper and lower meshes of the emitter . a second aperture can be provided in the dissector . the apertures can be of the same size and aligned such that there is a space therebetween . improvements are particularly secured by the design of the radiant gas burner that includes a casing in the form of a cylinder and an air - gas mixer connected with the casing thereof so as to ensure air - gas mixture input tangentially . the radiant gas burner can have one or several air - gas mixers of the same or different capacity , connected to the casing thereof as to ensure the air - gas mixture input into the casing in one direction ( i . e . clockwise or counter - clockwise ). the casing of the radiant gas burner can consist of two or more parts with a separate air - gas mixture supply to each of them . referring now to fig1 and 2 , fig1 displays a first embodiment of a radiant gas burner for gas fuel combustion , which comprises a cylindrical casing 1 , an injection - type air - gas mixer 2 , a gas dissector 3 a , and a metallic - mesh emitter 4 having a lower mesh 5 and an tipper mesh 6 forming a convex - concave lens . the casing includes an aperture 7 located in between the lower mesh 5 and the upper mesh 6 of emitter 4 . gas dissector 3 a can also include an aperture 8 adjoining casing 1 ( refer to fig2 ). apertures 7 and 8 can be the same size and can be located so that the distance between their centers is minimal . the radiant gas burner operates as described below . the gas entering mixer 2 injects some amount of air necessary for combustion and is mixed therewith . the injection - type gas mixer 2 can be fixed to cylindrical casing 1 so that air - gas mixture enters casing 1 tangentially at low velocity . the air - gas mixture flux can acquire rotary motion , thereby moving circularly inside casing 1 and being reverberated from a cylindrical surface and the bottom of casing 1 . the air - gas mixture is directed to the center of the casing and then to emitter 4 . thus , due to such attachment of mixer 2 to cylindrical casing 1 , more uniform flux distribution is obtained along the whole area of lower mesh 5 of emitter 4 . such solution produces uniform flux distribution by the whole emitter area even at its large dimensions without special flux bumpers , which are used in the existing radiant gas burners [ see for example , ir , unified , wind - proof gas burner giiv - 3 . 65 . operation manual . kazan , 1989 ]. casing 1 can accommodate several air - gas mixers 2 , e . g ., to decrease overall dimensions . in one illustrative example , in order to prevent additional higher flow resistance during collision of separate air and gas fluxes , mixers 2 are fixed to casing 1 so as to ensure air - gas mixture input into the casing in one direction , clockwise or counter - clockwise ( fig2 ). gas dissector 3 a , which is located along the pathway of air - gas mixture flux ahead of emitter 4 , allows increasing uniformity of air - gas mixture flux distribution by emitter 4 . gas dissector 3 a is used to reflect part of the emission from emitter 4 which is directed towards burner bottom , as well as to heat air - gas mixture incoming for combustion . gas dissector 3 a can be in the form of a ribbed grid ( plate - type heat exchanger ) comprising ribs 10 which are inclined to an upper grid plane 12 and a lower grid plane 14 . to promote reflection of the emission , edges of adjacent ribs can be in the same plane perpendicular to that of the grid ( fig3 ). for example , an upper edge 16 of one rib can be connected by a plane 18 to a lower edge 20 of an adjacent rib , wherein plane 17 is perpendicular to grid planes 12 , 14 . emission hitting the grid heats the ribs 10 and then the air - gas mixture flux passing through gaps 22 between the ribs of the grid is heated by convective heat transfer . this enables increasing heat to be released during gas combustion thereby raising burner performance . to ensure reliable automatic ignition , aperture 8 can be provided in gas dissector 3 a and aperture 7 can be provided in casing 1 . a portion of the air - gas mixture entering into the space under gas dissector 3 a is directed to aperture 8 , since the gas dissector has low flow resistance . this same portion of the air - gas mixture passes through lower mesh 5 of emitter 4 and to aperture 7 , as upper mesh 6 of emitter 4 also possesses low flow resistance . an automatic igniter ( not illustrated ) can be fixed opposite aperture 7 outside the burner casing . air - gas mixture combustion can occur in the space between meshes 5 and 6 of emitter 4 and the igniter can be positioned outside high temperature zone and thus will not interfere with a heat receiver located above emitter 4 . to facilitate ignition , apertures 7 and 8 can have similar dimensions . aperture 8 can be along a side of casing 1 and geometrical centers of the apertures 7 , 8 can be aligned including a distance therebetween . the cross - section of the gas dissector grid is one of its defining parameters . on the one hand , it must be as small as possible to ensure high effectiveness of backscattered emission “ trapping ” and / or reflection , and on the other hand , it must be sufficiently large to assure low flow resistance to the incoming air - gas mixture . thus , the maximum allowable flow resistance of the gas dissector grid provides a limitation to the increasing effectiveness of backscattered emission trapping . the area of the grid surface contacting the air - gas mixture flux is another parameter . a larger contact surface enables more heat to be transferred from the heated grid to the air - gas flux . the grid ribs as shown and described provide for an increase to the contact surface area and an increase in heat transfer . to increase heat transfer and its effectiveness in the gas dissector , one can use corrugated plates or rings to form a ribbed grid ( fig4 ). an alternative gas dissector 3 b can be made in the form of coupled concentric cone rings 11 . to align upper and lower edges 17 , 21 of adjacent ribs in the same vertical plane 19 ( between an upper grid plane 13 and a lower grid plane 15 ), a larger diameter of one ring can be equal to a smaller diameter of another adjoining ring . thus , the gas dissector grid 3 b provides : low flow resistance to the incoming air - gas mixture 23 ; maximum heat transfer during heat exchange between the emitter , the gas dissector , and the air - gas mixture flux ; and , small dimensions . tables 1 , 2 and 3 document operational parameters of a gas dissector grid 3 a , calculated for a radiant gas burner with specific heat capacity of 200 kw / m 2 , and an emitter &# 39 ; s area of 0 . 01 m 2 . the grid material used was steel 12x18h9t . the variable parameters included : grid thickness — h , rib inclination to grid plane — β , and rib thickness — δ . the calculated values included : real cross - section of the grid — m , hydrodynamic resistance — δp ( pa ), and heat transferred by convection — q ( w ). as seen from table 1 , increasing the grid thickness h leads to a larger real grid cross - section m on the one hand , and on the other hand , to a prominent reduction of heat q transferred by the grid to the air - gas flux . table 2 shows that increasing grid rib thickness δ results in smaller real cross - section m of the grid while having little affect on the heat q transferred by the grid to air - gas flux . as seen from table 3 , decreasing rib inclination β to the grid plane leads to lower heat q transferred by the grid to air - gas flux and significantly reduces the real cross - section m of the grid . on the basis of the given data and with regard to the parameters of the gas dissector grid , one preferred embodiment for a grid configuration is as follows : a grid thickness less than or equal to 5 . 0 mm ; a grid rib thickness less than or equal to 1 . 0 mm ; and , a rib inclination to grid plane from about 45 ° to about 60 °. as described above , the gas mixture combustion occurs in metallic - mesh emitter 4 between meshes 5 and 6 . a greater portion of the heat during combustion is transferred to lower mesh 5 , which , when heated , becomes a source of ir . the upper mesh 6 intensifies the combustion process by returning part of the emission back into inter - mesh space 30 , and by being heated through the combustion process and emission from lower mesh 5 , thereby also becoming a source of ir radiation . mesh openings in the meshes , 5 , 6 attempt to meet contradictory objectives . on the one hand , they should be sufficiently large to provide low hydrodynamic resistance necessary for normal operation of the injector and , on the other hand , the size of lower mesh 5 openings should avoid flashback . for the upper mesh 6 , the total space of open flow area should be sufficiently large to provide low hydrodynamic resistance and at the same time it should return sufficient part of the emission from the lower mesh 5 to maintain combustion in between the meshes . in one embodiment , the lower mesh openings ( not illustrated ) can have a maximum opening size of 0 . 8 mm and the upper mesh openings can have a minimum opening size of 1 . 5 mm . the distance between the meshes can be about 8 - 10 times the size of the lower mesh openings and depends on the ratio of combustion rate and air - gas mixture flow velocity . fig5 shows a second embodiment of a radiant gas burner b 2 including casing 31 , consisting of two parts or segments . the casing has central 42 and peripheral 44 parts with one air - gas mixer 32 a , 32 b attached to each of them respectively . the burner b 2 also includes a gas dissector 33 and a metallic - mesh emitter 34 including a lower mesh 35 and an upper mesh 36 that form a biconvex lens having an inter mesh area 40 therebetween . a pair of apertures 37 , 38 can be positioned in the inter - mesh area and the dissector 33 , respectively . in such burner design , the air - gas mixture can go to different parts of the casing both simultaneously and in turn . in other respects gas fuel combustion occurs as described for the burner design shown in fig1 . in one preferred version of the burner , a metallic - mesh emitter was used with square openings of 0 . 5 × 0 . 5 mm for the lower mesh and 3 × 3 mm for the upper one . referring to table 4 , comparative experiments were made using a conventional gas - plasma burner ( no . 1 ), and burners with different geometry of a metallic - mesh emitter , namely , with parallel meshes ( no . 2 ), meshes forming a biconvex lens ( no . 3 ) and meshes forming a convex - concave lens ( no . 4 ). all of the burners were of the same power − 1 . 8 kw . the time to heat 2 kg of water to 90 ° c . was measured and the combustion products composition was determined . instantaneous and total gas flow rate was monitored during the experiment . the same pan was used to heat water in each experiment . combustion products composition was determined by gas analyzer testo - 350 . table 4 gives the results of the comparative experiments . as seen from the data given in table 4 , the burner having a combustion zone formed in a biconvex lens ( no . 3 ) resulted in a carbonic oxide content 1 - 2 ppm or 10 times less than that for a flat burner ( no . 2 ). when heating the same amount of water with a burner in which the combustion space was a convex - concave lens ( no . 4 ), gas flow rate was 12 % less ( 32 . 1 compared to 36 . 5 ) than the burner with flat meshes ( no . 2 ). as described above , the stated problems can be solved by a radiant gas burner b 1 , b 2 having metallic mesh emitter 4 , 34 comprising lower 5 , 35 and upper 6 , 36 meshes forming an inner cavity 30 , 40 in the form of a lens ( i . e . convex - concave , biconvex ) with a radius of curvature of at least the burner &# 39 ; s diameter and a thickness or width of at least 8 - 10 times the characteristic sizes of the lower mesh openings . the lower mesh having mesh size openings less than the upper mesh size . it is to be appreciated that the lower mesh 5 , 35 is in a convex orientation relative to the flow of air - gas mixture . when the meshes are arranged such that the combustion area is an inner cavity in the form of a biconvex lens ( fig5 ), part of the ir emission from the lower and upper meshes 35 , 36 is focused at the inter - mesh combustion area 40 , thereby intensifying the combustion process . this results in an increase to the gas combustion quality and a decrease in the carbonic oxide content in the combustion products . while this invention has been described in conjunction with the exemplary embodiments outlined above , various alternatives , modifications , variations , improvements , and / or substantial equivalents , whether known or that are or may be presently unforeseen , may become apparent to those having at least ordinary skill in the art . accordingly the exemplary embodiments of the invention , as set forth above , are intended to be illustrative , not limiting . various changes may be made without departing from the spirit and scope of the invention . therefore , the claims as filed and as they may be amended are intended to embrace all known or later developed alternatives , modifications , variations , improvements , and / or substantial equivalents .