US3923464A

US3923464A - Combustion apparatus for analytical instruments

Info

Publication number: US3923464A
Application number: US291763A
Authority: US
Inventors: George J Sitek; Robert N Revesz
Original assignee: Leco Corp
Current assignee: Leco Corp
Priority date: 1972-09-25
Filing date: 1972-09-25
Publication date: 1975-12-02
Anticipated expiration: 1992-12-02

Abstract

A combustion furnace for analytical apparatus in which the products of combustion of samples are to be transported in a gas stream for analysis wherein the admission of carrier gas is separate from the admission of combustion gas, resulting in a reduction of eddy currents of the gases within the furnace, so leading to a faster transfer of the component to be measured and to reduced purge and combustion time.

Description

United States Patent n 1 m1 3,923,464

Sitek et al. Dec. 2, 1975 COMBUSTION APPARATUS FOR 3,085,717 3/1963 Anscherlik 23/253 ux ANALYTICAL INSTRUMENTS 3,301,2[3 l/l967 GI'OChOWSki Ct a] 219/1043 X 3,459,938 8/l969 Stengler ct al 23/230 PC [75] Inventors: George J- l k, n fll Robert 3,567,386 3/1971 Stengler 23/230 PC N. Revesz, St. Joseph, both of Mich. [73] Assignee: Leco Corporation, St. Joseph, Mich. Primary Examiner Morri5 wolk Assistant ExaminerArnold Turk [22] Filed: Sept 1972 Attorney, Agent, or Firm-Price, Heneveld, Huizenga 211 Appl. No.: 291,763 & Cooper [52] US. Cl. 23/253 PC; 23/292; 138/40 [57] ABSTRACT [51] Int. cl. G01N 31/12; FD 1/00 A Combustion furnace for aflalytical apparatus in 5 Field f Search M 23/23() PC, 253 PC, which the products of combustion of samples are to be 219/1 43;55 3 3 210/198 transported in a gas stream for analysis wherein the 1 125 139 13 39 09 174 admission of carrier gas is separate from the admission of combustion gas, resulting in a reduction of eddy 5 References Cited currents of the gases within the furnace, so leading to UNITED STATES PATENTS a faster transfer of the component to be measured and to reduced purge and combustion time. 2,687,614 8/1954 Goddard 138/40 X 2,809,100 10/1957 Krasl 23/230 PC X 10 Claims, 1 Drawing Figure 62 6'6 44 [a 66 4 46 [Xi/4057' f0 98 h i 20 f5 i8 i0 4 -H' .90 CHER/E US. Patent D60. 2, 1975 cake/51a 6A5 COMBUSTION APPARATUS FOR ANALYTICAL INSTRUMENTS BACKGROUND OF THE INVENTION In U.S. Pat. No. 2,809,100 dated Oct. 8, 1957, to G. J. Krasl, entitled Combustion Analyzer, there is shown a glass capsule adapted to fit within an induction coil and to fit over a crucible supported on a post which positions the crucible within the'field of'the combustion coil. The bottom of the capsule is open for the vertical elevation of the crucible and post thereinto and is closed by a base plate carrying the post brought up into contact with the bottom of the capsule. The base plate has a passage therethrough for the downward flow of exhaust gases from the capsule. A tube extends centrally down through the top of the capsule into a position to direct a jet of oxygen into the crucible when it is in its elevated position. In use, a sample in a crucible is elevated into the capsule and heated by the induction coil. At the same time, oxygen is directed down onto the sample to support its combustion and the products of combustion together with a carrier stream of excess oxygen from the jet are carried out through the bottom of the capsule for electronic analysis.

This apparatus does not function as well as it might for several reasons. There is a dead space above the crucible between the jet tube and the wall of the capsule in which eddy currents will exist, delaying the total transfer of the material to be analyzed and leading to a trailing of the combustion gases which causes a tailing of the analysis curve. Optimum readout is derived from a total transfer of the product to be analyzed within as short a time period as possible, or in other words, an abrupt rise in the transfer curve to a high peak and an abrupt decline or decay thereafter. Eddying of the carrier gas extends the rise time, reduces the peak, and causes the decay curve to tail off gradually. The same eddy currents cause a depositing of metal on the walls of the capsule which, in time, couple to the field of the induction furnace and destroy the capsule.

By virtue of the single inlet port for the gas which serves both a combustion and carrier function which is directed straight into the crucible, the velocity of gas flow is desirably limited to avoid excessive reaction temperatures and excessive turbulence. Under conditions of a high content of combustible material, the combustion process can absorb the whole input of combustion gas and create a below-atmospheric pressure condition within the capsule. This necessarily extends the analysis time because the transportation of the unknown must await the completion of the combustion. Furthermore, in analytical procedures involving such sensors as conductivity cells in bridge configurations, it is necessary to have a constant flow of gas through the cell because these measurements are flow sensitive. The total absorption of the gas during combustion results in a flow change or even a backflow of the gas stream.

SUMMARY OF THE INVENTION The present invention is directed to a combustion apparatus lacking blind corners or ends wherein eddy currents might develop. The apparatus is characterized by two gas inlet ports, one intended essentially for combustion and the second intended essentially for transport whereby a continuous flow may be obtained through the apparatus. By operating the device above ambient pressure, the combustion process only decreases the pressure and a constant flow still exists to satisfy the measurement criteria. The device likewise includes provision for positioning the combustion gas inlet whereby optimum combustion circumstances can be provided. The device may operate continuously above or below ambient pressure if constant flow is not necessary. The device is easily cleaned and therefore less subject to damage from scsulling, and the destructible element of the combination, the jacket, is inexpensive and easily replaced. Other advantages of this invention will appear in the course of the description which follows.

BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a central vertical section through an induction furnace embodying the present invention.

DESCRIPTION OF A PREFERRED EMBODIMENT The furnace 10 consists of a stationary furnace proper 11 and a vertically reciprocable crucible elevator 12. The stationary furnace 11 includes a base 13 which consists of a flat, annular plate 14 having upper and

lower flanges

16 and 18 about the central aperture 20 thereof. The upper flange is externally grooved for the reception of an O-ring 22. The under side of the plate also has a downwardly extending outer flange 24 thereabout which likewise is grooved on its exterior surface for the reception of an O-ring 26. A carrier gas inlet tube 28 opens into and extends from the central aperture 20 through the lower flanges l8 and 24 and terminates in a free end 30 well beyond the plate 14 and the confines of the furnace itself.

A Vycor or similar high silica glass or fused silica combustion tube 32 is mounted on the base 13. The combustion tube is of relatively large diameter so as to contain comfortably the crucible 34 leaving ample gas flow space thereabout. The tube fits in spaced relation within the induction coil 36. The tube is belled out at its lower end 38 to fit over the upper flange 16 of the base 13 to rest on its bottom edge against the annular plate 14 and to engage the O-ring 22 in sealed relation. Adjacent its upper end 40, the tube has a circumferential restriction 42 therein for purposes to be described later.

The tube mounts at its upper end a top fitting 44. This top fitting is a generally cylindrical member with a side arm 46 and an integral flange 48 thereabout below the side arm 46. The fitting is externally grooved below the flange 48 for the reception of an O-ring 49. A large diameter central bore 50 extends from the bottom of the fitting upwardly to a point adjacent the top of the fitting, and the side arm 46 has a bore 52 therein intersecting the axial bore 50. The axial bore 50 terminates at an upper transverse wall 54 having a small diameter axial passage 56 therethrough. A threaded hole 58 extends from the top end of the top fitting down to the wall 54. A combustion gas adaptor 60 is threaded into the hole 58. The adapter 60 is a simple tubular member having exterior threads at its lower end for engagement with the threaded bore 58 and a centrallongitudinal passage 62 therethrough and internally threaded as at 64 at its upper end for the reception of an oxygen supply fitting (not shown).

The internal bore 62 loosely receives a length of quartz tubing 66 constituting an oxygen lance. The tubing has an annular rubber bushing 68 fitted on the exterior thereof. The bushing is slidable along the tubing for adjustment of the lance position. The bushing is adjusted on the lance to obtain a proper positioning of the lance for optimum performance with respect to the crucible 34, and the combustion gas adaptor is screwed down on the bushing 68 to compress it against the wall 54 and bulge it against the lance 66 to effect a seal and hold the lance securely.

The elevator 12 is mounted on the top end of a vertically reciprocable rod 70. The elevating mechanism may be identical with that described in the abovementioned patent to Krasl. The elevator consists of a shallow dish 72 having a rim 74 with a vertical inside wall 76 beveled at its top edge proportioned to telescope over the outer flange 24 of the furnace base 13 in sealing relation with the O-ring 26. The dish may have a central internally threaded downward sleeve 78 whereby the dish is mounted to the post 70 and an internally threaded central sleeve 80 extending upward from the floor of the dish 72. The sleeve 80 receives a stud 82 having a lower threaded end 84, a hexhead 86, and a cylindrical plug 88 upward of the head 86. A tubular ceramic crucible support is carried on the plug 88 and mounts the crucible 34 at its upper end. The adjustment capability of the stud 82 is, of course, to position the crucible optimally within the induction coil 36.

The plate 14 of the base 13 and the flange 48 of top fitting 44 may be perforated as at 90 for the attachment of the furnace to brackets 92 whereby the furnace may be mounted to a cabinet or other element of the analytical apparatus.

From the foregoing, it will be appreciated that the assigned advantages of this invention have been well met. The provision for two gas inlets makes possible the continuous purge, avoidance of dead spaces, and avoidance of below-ambient pressure with combustion. The provision of the gas passages in the end fittings makes possible a low cost, simple tube and provides for a direct end-to-end passage of the gas. Gas flow through the apparatus may be continuous, and this immediate transfer, together with reduced purge time, appreciably shortens analysis time.

The upward flow of heated gases from the sample combustion, in the absence of the constriction 42 in the tube 32, exposes the O-ring 49 .to excessive temperatures and hot dust due to the direction of flow of the exhaust stream, subjecting it to damage and possible failure, which, of course, cannot be tolerated as leading to erroneous results. It has been found that the constriction 42 effectually shields the O-ring seal from damage by screening the seal from radiation from the burning sample and by deflecting the hot carrier gas stream with entrained products of combustion into the top fitting 44.

We claim:

1. A combustion furnace for analytical apparatus comprising an induction coil with a vertically extending axis, a combustion tube mounted within said coil, an upper closure member for sealably coupling to an upper end of said combustion tube, said upper closure member including an exhaust gas passage therethrough, and a separate aperture extending through said upper closure member along the vertical axis thereof, a lower closure member for sealably engaging the lower end of said combustion tube, said lower closure member including a passageway extending therethrough to define a carrier gas inlet communicating with the interior of said combustion tube and crucible supporting means associated with said lower closure member, said lower closure member movable between a first position sealing said lower end of said combustion tube and supporting a crucible within the field of. said coil and a second position displaced therefrom, a combustion gas lance, and means in said upper closure members for securing said lance in said separate aperture for optimal delivery of combustion gas into said crucible within said field.

2. The combination as claimed in claim 1 wherein said exhaust gas passage of said upper closure member extends vertically through a bottom surface of said upper closure member to communicate with the interior of said combustion tube and includes a radially-extending portion extending through a side of said upper closure member for providing an exhaust port for removal of combustion gases from said combustion tube.

3. The combination as claimed in claim 2 wherein said upper closure member includes a sealing member extending around the exterior of the lower periphery thereof to engage an inner surface of said combustion tube for sealing said upper closure member to said combustion tube.

4. The combination as claimed in claim 3 wherein said combustion tube is a cylindrical sleeve having a circumferential constriction formed at its upper end and immediately below said sealing member and extending inwardly sufficiently to shield said sealing member from combustion by-products.

5. A combustion furnace for analytical apparatus comprising an induction coil with a vertical axis, a vertical combustion tube within said coil, a base closure member mounted against the bottom end of said tube and having passage defining means for delivering gas into said tube, a vertically reciprocable elevator movable between a position of sealing against said base member and supporting a crucible within the field of said coil and a position downwardly displaced therefrom, a top fitting closing the top end of said combustion tube, means defining a second gas passage therethrough, and an oxygen lance mounted in said top fitting for delivering combustion gas into said crucible.

6. The combination as claimed in claim 5 wherein said oxygen lance is adjustably mounted in said top fitting for adjustment toward and away from said crucible. 7

7. The combination as claimed in claim 5 wherein said lance is a high silica tube and said top fitting telescopes within the top end of said combustion tube, said top fitting having a sealing ring thereabout in the telescoped portion thereof to seal against the interior surface of said combustion tube, said tube having a circumferential constriction extending inwardly immediately below said top fitting a distance sufficient for shielding said sealing ring from combustion byproducts. 1

8. For use in a furnace for heating specimens to their combustion temperature wherein the specimens are placed in a crucible positioned in a combustion tube with sealed end closures, and means extending through the end closures to provide a flow of gas through the combustion tube to carry combustion gases from the combustion tube, an improved combustion tube comprising:

a continuously extending cylindrical body having a first open end the interior wall surface of which defines an interior cylindrical sealing surface immediately adjacent said first open end and a circumferential restriction formed inwardly in said cylindrical body and spaced from said first end to shield said sealing surface from combustion by-products, said combustion tube including an enlarged open opposite end defining a cylindrical wall extending substantially parallel with said cylindrical body and defining a cylindrical interior sealing surface having a diameter greater than the diameter of said cylindrical body.

9. The combustion tube as defined in claim 8 wherein said combustion tube is made of high silica glass.

10. An induction furnace comprising:

a vertically extending induction coil;

a cylindrical combustion tube positioned within said induction coil and including an open upper end, an enlarged cylindrical lower open end and a circumferential restriction spaced from said open upper end;

an upper closure member for sealably fitting into said upper end of said combustion tube and including an axial opening through an end thereof for receiving an oxygen lance tube therethrough and further including a relatively large opening formed axially upwardly through a bottom surface of said upper closure member and communicating with a radially extending port for exhausting combustion and carrier gases from said combustion tube, said upper closure member including a peripheral sealing member positioned adjacent said restriction of said combustion tube; and

a lower closure member including means for supporting a crucible within the induction field of said induction coil when said lower closure member is sealably fitted in the enlarged lower end of said combustion tube, said lower closure member including an axially extending aperture opening at the top surface of said lower closure member and means for introducing a carrier gas to said last named aperture to provide a flow of gas upwardly through said combustion tube.

Claims

1. A COMBUSTION FURNACE FOR ANALYTICAL APPARATUS COMPRISING AN INDUCTION COIL WITH A VERTICALLY EXTENDING AXIS, A COMBUSTION TUBE MOUNTED WITHIN SAID COIL, AN UPPER CLOSURE MEMBER FOR SEALABLY COUPLING TO AN UPPER END OF SAID COMBUSTION TUBE, SAID UPPER CLOSURE MEMBER INCLUDING AN EXHAUST GAS PASSAGE THERETHROUGH, AND A SEPARATE APERTURE EXTENDING THROUGH SAID UPPER CLOSURE MEMBER ALONG THE VERTICAL AXIS THEREOF, A LOWER CLOSURE MEMBER FOR SEALABLY ENGAGING THE LOWER END OF SAID COMBUSTION TUBE, SAID LOWER CLOSURE MEMBER INCLUDING A PASSAGEWAY EXTENDING THERETHROUGHT TO DEFINE A CARRIER GAS INLET COMMUNICATING WITH THE INTERIOR OF SAID COM-

2. The combination as claimed in claim 1 wherein said exhaust gas passage of said upper closure member extends verticallY through a bottom surface of said upper closure member to communicate with the interior of said combustion tube and includes a radially extending portion extending through a side of said upper closure member for providing an exhaust port for removal of combustion gases from said combustion tube.

6. The combination as claimed in claim 5 wherein said oxygen lance is adjustably mounted in said top fitting for adjustment toward and away from said crucible.

7. The combination as claimed in claim 5 wherein said lance is a high silica tube and said top fitting telescopes within the top end of said combustion tube, said top fitting having a sealing ring thereabout in the telescoped portion thereof to seal against the interior surface of said combustion tube, said tube having a circumferential constriction extending inwardly immediately below said top fitting a distance sufficient for shielding said sealing ring from combustion by-products.

8. For use in a furnace for heating specimens to their combustion temperature wherein the specimens are placed in a crucible positioned in a combustion tube with sealed end closures, and means extending through the end closures to provide a flow of gas through the combustion tube to carry combustion gases from the combustion tube, an improved combustion tube comprising: a continuously extending cylindrical body having a first open end the interior wall surface of which defines an interior cylindrical sealing surface immediately adjacent said first open end and a circumferential restriction formed inwardly in said cylindrical body and spaced from said first end to shield said sealing surface from combustion by-products, said combustion tube including an enlarged open opposite end defining a cylindrical wall extending substantially parallel with said cylindrical body and defining a cylindrical interior sealing surface having a diameter greater than the diameter of said cylindrical body.

10. An induction furnace comprising: a vertically extending induction coil; a cylindrical combustion tube positioned within said induction coil and including an open upper end, an enlarged cylindrical lower open end and a circumferential restriction spaced from said open upper end; an upper closure member for sealably fitting into said upper end of said combustion tube and including an axial opening through an end thereof for receiving an oxygen lance tube therethrough and further including a relatively large opening formed axially upwardly through a bottom surface of said upper closure member and communicating with a radially extending port for exhausting combustion And carrier gases from said combustion tube, said upper closure member including a peripheral sealing member positioned adjacent said restriction of said combustion tube; and a lower closure member including means for supporting a crucible within the induction field of said induction coil when said lower closure member is sealably fitted in the enlarged lower end of said combustion tube, said lower closure member including an axially extending aperture opening at the top surface of said lower closure member and means for introducing a carrier gas to said last named aperture to provide a flow of gas upwardly through said combustion tube.