US3229358A - Process of manufacturing heating means for de-icing static ports and the like - Google Patents
Process of manufacturing heating means for de-icing static ports and the like Download PDFInfo
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- US3229358A US3229358A US139209A US13920961A US3229358A US 3229358 A US3229358 A US 3229358A US 139209 A US139209 A US 139209A US 13920961 A US13920961 A US 13920961A US 3229358 A US3229358 A US 3229358A
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- Prior art keywords
- sheath
- heater
- passage
- support
- icing
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05B—ELECTRIC HEATING; ELECTRIC LIGHT SOURCES NOT OTHERWISE PROVIDED FOR; CIRCUIT ARRANGEMENTS FOR ELECTRIC LIGHT SOURCES, IN GENERAL
- H05B3/00—Ohmic-resistance heating
- H05B3/40—Heating elements having the shape of rods or tubes
- H05B3/42—Heating elements having the shape of rods or tubes non-flexible
- H05B3/48—Heating elements having the shape of rods or tubes non-flexible heating conductor embedded in insulating material
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49002—Electrical device making
- Y10T29/49082—Resistor making
- Y10T29/49087—Resistor making with envelope or housing
- Y10T29/49089—Filling with powdered insulation
- Y10T29/49091—Filling with powdered insulation with direct compression of powdered insulation
Definitions
- This invention relates to de-icing heating arrangements for incorporation with devices having a passage wherein the passage and the exterior of the device are subjected to temperature sufficiently low to induce freezing of moisture' entrained in the air or other gas flowing through the passage and past the device.
- it has reference to electrical heaters for-incorporation with air-entry ports as used on aircraft as well as the combination of the port and heater, for example, a port to sense the static pressure of the ambient air.
- the present invention relates to an arrangement of passage-forming means and heater which is characterized by minimum dimensions and therefore minimum air resistance and in which the rate of heat transfer from the heater to the remainder of the device is a maximum, thereby substantially reducing the wattage consumed.
- an elongated, electrical heating element of the metallic-sheathed type is provided with a peripheral portion juxtaposed to a congruent portion of the interior wall of the passage. Desirably the thus juxtaposed portions are further rendered into intimate contact by brazing.
- the remainder of the periphery of the heating element is conformed re-entrant- 1y to define, with the corresponding remainder of the passage wall, the air passage through the device.
- the invention in another aspect, comprehends a sheathed heater element per se having the configuration stated and capable of being fabricated to small dimensions, and the method of so fabricating the same.
- FIG. 1 is a longitudinal cross section of a static port as used, for example, on aircraft and incorporating the novel heating element of the invention
- FIG. 2 is a cross section taken on the line 22 of FIG. 1;
- FIG. 3 is a cross section similar to that of FIG. 2 but of an alternative embodiment
- FIG. 4 is a cross section similar to that of FIG. 2 but of still another alternative
- FIG. 5 is a combined side elevation and section to show certain steps in the fabrication of the heater element
- FIG. 6 is an elevational view similar to the showing of FIG. 5 to illustrate other steps in the fabrication
- FIGS. 7, 8 and 9 are cross sections taken on the lines 7-7, 88 and 9-9 respectively of FIG. 5;
- FIG. 10 is a later step in the processing sequence to be described in connection with FIGS. 5 and 6.
- the invention in one aspect, comprehends an electrical heater element for insertion in a fluid passage to heat both the wall defining the passage and the fluid passing therethrough.
- the heater element comprises an initially cylindrical sheath enclosing an electrical conductor of relatively high resistance which, when connected in a supply circuit of selected voltage, undergoes a substantial rise in temperature, e.g., Nichrome wire,
- the conductor preferably wound into helical form or a mandrel of insulating material, is housed in the sheath, from which it is electrically isolated by a refractory material such as densely compacted magnesium oxide powder.
- the sheath and its contents are deformed by an appropriate instrumentality to provide an exterior longitudinal channel.
- the diameter of the sheath is chosen to be a fairly snug fit in the passage and, therefore, when the completed heater is inserted therein the channel will, with the interior wall surface of the passage, define a smaller passage for flow of fluid.
- the relative transverse dimensions of the inserted heater and the original passage as well as the longitudinal channel in the heater are so chosen as to provide a usable fluid passage as required.
- the heater is rendered into intimatecontact with the interior wall surface of the initial passage by brazing or similar medium in order to improve heat transfer to the several parts of the device subject to deposition of moisture and consequent icing.
- a substantial area thereof constitutes a part of the wall of the ultimate fluid passage. Accordingly such passage is heated directly by radiation as well as by conduction through the metal constituting the device.
- the invention comprehends features of construction of the heater itself and the process of manufacturing the same.
- FIG. 1 there is shown a mounting 10 including a first boss 11., a flange 12 and a second boss 13.
- the mounting is secured at a selected location on the skin 15 of the aircraft by rivets 16 or equivalent means.
- boss 13 has one or more passages 18 for admission of air
- the pressure sensed by the device is static head as contrasted with the velocity head of an associated Pitot tube.
- the boss 11 is internally threaded at 21 to receive one correspondingly threaded end 22 of a fitting 23, in this case an elbow.
- a fitting 23 in this case an elbow.
- the desideratum being a metallic or other heatconducting body through which a fluid passage is provided.
- a locknut 26 is provided and the same also confines a gasket 27 to seal against possible leakage past the nut 26.
- the end 25 of the fitting is threaded for connection thereto of a conduit (not shown) leading to the indicating instrument, as will be understood.
- the leads 34 and 35 of the resistance winding 36 are carried to terminal posts 37 supported on an insulating disc 38 secured in a connector sleeve 41.
- a complementary sleeve (not shown) is engaged with the sleeve 41 to connect the heater in the supply and/ or control circuit.
- Suitable insulation 43 surrounds the leads 34 and 35.
- the heating element 31 serves to heat both the exterior and interior of the port the same is, in accordance with the principles of the invention, given a form now to be detailed.
- the same comprises a tubular metallic sheath 51 which, regarded in its transverse aspect, comprises a portion A extending over approximately 270 of arc and a portion B extending over approximately 90 of are.
- the cross section of the heating element may be described as substantially concave-convex.
- the initial diameter of the sheath (prior to deformation by swaging and indentation in a manner to be detailed) is so chosen that when operated upon it may yield a diameter such as to provide a snug fit in the passage into which it is introduced, e.g., the bore 32 of the fitting 23 of the example.
- the portion A After being located in its desired longitudinal position the portion A is desirably brazed or otherwise rendered into intimate contact with the adjoining surface. Such operation may be accomplished by allowing some clearance between the passage and the portion A and inserting a thin strip of silver solder therein. Heat is then applied to the exterior of the assembly.
- portion B will, together with the adjacent passage surface 32, will define a conduit 54 substantially of elliptical transverse aspect through which the air may pass from the opeiings 18 into the leg 25 of the fitting 23.
- the portion A of the heater By reason of the intimacy of contact between the portion A of the heater and the adjoining wall surface the body of. the device will be heated by conduction and that the Wall surfaces of the conduit 54 will be heated by conduction and radiation.
- FIGS. 3 and 4 are cross sections similar to that of FIG. 2 to illustrate alternative embodiments.
- the air passage or passages are indicated at 54a and 54b, and the heater or heaters at 3111 and 31b.
- heat is supplied to the air passage or passages and to the sheath. 1n the embodiment of FIG. 4 heat transfer may be implemented by soldering or brazing as indicated.
- a preferred construction of heater comprises a spool 61 of ceramic material (FIG. of beryllia, alumina or the like having flanges 62 flanking a cylindrical winding portion 63 of smaller diameter than the flanges.
- the flanges are relieved for a portion of their periphery by flats 64-64 to define, with the sheath blank 71 suitable spaces 60-.60 for a purpose to appear.
- the resistance wire 65 e.g., Nichrome
- the resistance wire 65 is helically Wound on the portion 63 either in juxtaposed coils or in a helical groove provided therein, and the ends are connected by welding or otherwise to terminal leads 66and, 67 passing through bores through the spool 61.
- the leads One v termined diameter and of a length more than spanning the overall length of the spool 61. is tack-brazed at its ends to the periphery of the blank 71. For example, for a blank 71 of diameter the rod will be As" diameter, and for a spool of length 2" the rod will be 3" long, thereby to extend beyond the spool approximately at each end.
- a pellet 86 of friable refractory material is deposited in the tube 71 from the right hand end.
- This pellet is a cylinder which is longitudinally truncated over its length to provide diametrically opposite flats 91-91, in turn defining with the tube 71 a pair of spaces 9292. Adjacent its ends the pellet is notched on both sides as indicated at 9494. While notching at one end only is sufllcient for the intended temporary use, both ends are desirably made the same to eliminate concern by the operator as to which end of the pellet is to be inserted first.
- the heater core assembly comprising the spool, its winding and leads are assembled with another pellet 97 bored to receive the terminal leads 67 therethrough and these parts are inserted in the blank 71 to abut the pellet 91. Since the position of the leads 67 is desirably definitely angularly related to the portion B of the heater the same are orientated as shown with respect to the rod 84 which may then be removed. Although some endwise clearances between the components are shown on the drawing for clarity of comprehension no clearance need actually exist.
- the pellet 97 is provided with two diametrically opposite flats 98-98 (FIG. 9) similarly to the pellet 86 to provide a pair of spaces 99--99.
- the left end of the sheath blank 71 is taped closed and, with the tube held vertically a suitable pulverulentrefractory, e.g., powdered magnesium oxide is poured into the upper end. Meanwhile the tube is vibrated in any suitable jogging device to insure that all voids are filled.
- a suitable pulverulentrefractory e.g., powdered magnesium oxide
- the spaces 9999, -60 and 92-92 allow the powder to pass through to the left hand end and to fill all other voids. Vibration is continued until the powder is wellcompacted. Passage of the powder into the spaces '9292 is facilitated by the notches 9494 acting as funnels.
- the right hand end (presently the uppermost end) is then taped shut and the assembly (FIG. 5) is then turned end for end. The tape is removed from the left end (presently the uppermost end) and that end welded or otherwise closed.
- a metallic plug or disc may be used as part of this plugging operation.
- the assembly is turned end for end and vibrated once more as further assurance that the powder is a well-compacted mass. It will be understood that such mass remains until the heater assembly 31 is cut from the processing assembly, and that the powder surrounding the winding serves to insulate and to provide additional stability for such winding throughout the life of the heater.
- FIG. 5 The assembly of FIG. 5 is now swaged to its final diameter, in the example, 78", and then annealed.
- the rod 84 is re-affixed in its original position and assembly is passed through suitable swaging dies whereby the rod 84 is forced into the sheath blank 71 (FIG. 10) to form the indented peripheral re-entrant portion B.
- the desired finished diameter namely 0.343
- the sheath blank 71 is now severed adjacent both ends of the spool 61, care being taken not to disturb the leads 6767.
- the scrap, including the rod 84, is discarded, it being recalled that this rod was secured only at its ends.
- the outer end of the heater 31 (FIG. 1) is closed by a brazed-on closure plate 101 of proper outline and the heater is now ready for incorporation with the fitting 23, in the manner previously described.
- each of the heaters 31a is fabricated in a manner similar to that described in connection with FIG. 5 and, in the case of that form of the invention heater shown in FIG. 4 the rod 84 will be in multiple, spaced apart about the periphery of the sheath blank 71.
- an electrical heater of the type comprising a metallic sheath enclosing a conductive element of high electrical resistance and in which the element is spaced from, and supported relative to the sheath by a matrix of electrically-insulating material, which comprises: providing a sheath of tubular form, assemblying the element on a support of friable, electrically-insulating material, said support being a slip fit in the sheath, inserting the support with the thereon-supported element in the sheath, inserting a friable plug in at least one end of the sheath abutting one end of the support, temporarily attaching an incompressible rod-like indenting member to the sheath wall, said member being at least coextensive longitudinally with said support, forcing the member into the sheath wall to deform the sheath and crush the support and removing said member.
- an electrical heater of the type comprising a metallic sheath enclosing a conductive element of high electrical resistance and in which the element is spaced from, and supported relative to the sheath by a matrix of electrically-insulating material, which comprises: providing a sheath of tubular form, assembling the element on a support of friable, electrically-insulating material, inserting the support with the thereon-supported element in the sheath, inserting a friable plug in the sheath at each end of the support, temporarily attaching an incompressible rod-like indenting member to the sheath wall, said member being at least coextensive longitudinally with said support, forcing the member into the sheath wall to deform the sheath and crush the support and removing said member.
Description
Jan. 18, 1966 M. D. SCADRON ETAL PROCESS OF MANUFACTURING HEATING MEANS FOR DE-ICING STATIC PORTS AND THE LIKE Filed Sept. 19. 1961 mmvrox. Marv/17D. Sandra): 7
flifys United States Patent PROCESS OF MANUFACTURING HEATING MEANS FOR DE-ICING STATIC PORTS AND THE LIKE Marvin D. Scadron, Skokie, and Otto J. Cousins, Chicago, Ill., assignors, by mesne assignments, to American Radiator & Standard Sanitary Corporation, New York, N.Y., a corporation of Delaware Filed Sept. 19, 1961, Ser. No. 139,209 8 Claims. (Cl. 29--155.65)
This invention relates to de-icing heating arrangements for incorporation with devices having a passage wherein the passage and the exterior of the device are subjected to temperature sufficiently low to induce freezing of moisture' entrained in the air or other gas flowing through the passage and past the device. In particular it has reference to electrical heaters for-incorporation with air-entry ports as used on aircraft as well as the combination of the port and heater, for example, a port to sense the static pressure of the ambient air.
The problem of icing of air-admitting adjuncts, e.g., static ports and Pitot tubes as used on aircraft, is constantly presented and much effort has been directed to its solution. In general, prior arrangements have attempted to combat icing, whether incipient or actual, by providing electrical heating means adjacent to a wall, either interior or exterior, of the port or tube. Inasmuch as the surface presented to the air stream by the device and the wattage consumed by the heater must both be a minimum compromise is unavoidable for, if an overrated heater is used, its'b'ulk not only increases the dimensions of the device and thus its air resistance but consumption of current rises beyond what the specification allows.
The present invention relates to an arrangement of passage-forming means and heater which is characterized by minimum dimensions and therefore minimum air resistance and in which the rate of heat transfer from the heater to the remainder of the device is a maximum, thereby substantially reducing the wattage consumed. In accordance with the principles of the invention an elongated, electrical heating element of the metallic-sheathed type is provided with a peripheral portion juxtaposed to a congruent portion of the interior wall of the passage. Desirably the thus juxtaposed portions are further rendered into intimate contact by brazing. The remainder of the periphery of the heating element is conformed re-entrant- 1y to define, with the corresponding remainder of the passage wall, the air passage through the device. Thus, not only is heat transmitted most efficiently to the body of the device to inhibit ice formation but the air passage is maintained at a temperature suflicient to prevent icing therewithin.
I Inasmuch as the physical dimensions of devices to which the invention heater is primarily adapted present restrictions on the size of the heating element incorporated therewith in the manner alluded to above. The invention, in another aspect, comprehends a sheathed heater element per se having the configuration stated and capable of being fabricated to small dimensions, and the method of so fabricating the same.
Other objects and advantages of the invention will become evident from the following description which, together with the accompanying drawing, discloses various forms which the invention heater may assume in practice, as well as certain steps in the method of manufacturing the same.
In this drawing:
FIG. 1 is a longitudinal cross section of a static port as used, for example, on aircraft and incorporating the novel heating element of the invention;
3,229,358 Patented Jan. 18, 1966 FIG. 2 is a cross section taken on the line 22 of FIG. 1;
FIG. 3 is a cross section similar to that of FIG. 2 but of an alternative embodiment;
FIG. 4 is a cross section similar to that of FIG. 2 but of still another alternative;
FIG. 5 is a combined side elevation and section to show certain steps in the fabrication of the heater element;
FIG. 6 is an elevational view similar to the showing of FIG. 5 to illustrate other steps in the fabrication;
FIGS. 7, 8 and 9 are cross sections taken on the lines 7-7, 88 and 9-9 respectively of FIG. 5; and
FIG. 10 is a later step in the processing sequence to be described in connection with FIGS. 5 and 6.
Regarded broadly the invention, in one aspect, comprehends an electrical heater element for insertion in a fluid passage to heat both the wall defining the passage and the fluid passing therethrough. Where herein We employ the term fluid we intended to encompass fluent substances generally. In accordance with the principles of this phase of the invention the heater element comprises an initially cylindrical sheath enclosing an electrical conductor of relatively high resistance which, when connected in a supply circuit of selected voltage, undergoes a substantial rise in temperature, e.g., Nichrome wire, The conductor, preferably wound into helical form or a mandrel of insulating material, is housed in the sheath, from which it is electrically isolated by a refractory material such as densely compacted magnesium oxide powder. Following such assembly the sheath and its contents are deformed by an appropriate instrumentality to provide an exterior longitudinal channel. The diameter of the sheath is chosen to be a fairly snug fit in the passage and, therefore, when the completed heater is inserted therein the channel will, with the interior wall surface of the passage, define a smaller passage for flow of fluid. The relative transverse dimensions of the inserted heater and the original passage as well as the longitudinal channel in the heater are so chosen as to provide a usable fluid passage as required. Desirably the heater is rendered into intimatecontact with the interior wall surface of the initial passage by brazing or similar medium in order to improve heat transfer to the several parts of the device subject to deposition of moisture and consequent icing. By reason of the deformation performed on the heater element a substantial area thereof constitutes a part of the wall of the ultimate fluid passage. Accordingly such passage is heated directly by radiation as well as by conduction through the metal constituting the device.
In other aspects the invention comprehends features of construction of the heater itself and the process of manufacturing the same.
By way of example the invention heater will be described in connection with a static port as used on an airplane, viz. to sense static air pressure in flight. Thus, adverting to FIG. 1 there is shown a mounting 10 including a first boss 11., a flange 12 and a second boss 13. The mounting is secured at a selected location on the skin 15 of the aircraft by rivets 16 or equivalent means. The
boss 13 has one or more passages 18 for admission of air,
and, since, such passages 18 are normal to the principal direction of the air stream, the pressure sensed by the device is static head as contrasted with the velocity head of an associated Pitot tube.
The boss 11 is internally threaded at 21 to receive one correspondingly threaded end 22 of a fitting 23, in this case an elbow. At this point it is to be noted that the form of the body with which the heater is incorporated is variable, the desideratum being a metallic or other heatconducting body through which a fluid passage is provided. To obtain the desired orientation of the other end 3 25 of the fitting a locknut 26 is provided and the same also confines a gasket 27 to seal against possible leakage past the nut 26. The end 25 of the fitting is threaded for connection thereto of a conduit (not shown) leading to the indicating instrument, as will be understood.
A heating element 31, to be considered in more detail subsequently, is received in a bore or initial passage 32 of the fitting 23 and extends over substantially the full length thereof. The leads 34 and 35 of the resistance winding 36 are carried to terminal posts 37 supported on an insulating disc 38 secured in a connector sleeve 41. A complementary sleeve (not shown) is engaged with the sleeve 41 to connect the heater in the supply and/ or control circuit. Suitable insulation 43 surrounds the leads 34 and 35.
Inasmuch as the heating element 31 serves to heat both the exterior and interior of the port the same is, in accordance with the principles of the invention, given a form now to be detailed. As shown best in the example of FIG. 2 the same comprises a tubular metallic sheath 51 which, regarded in its transverse aspect, comprises a portion A extending over approximately 270 of arc and a portion B extending over approximately 90 of are. For convenience of description and claiming the cross section of the heating element may be described as substantially concave-convex. The initial diameter of the sheath (prior to deformation by swaging and indentation in a manner to be detailed) is so chosen that when operated upon it may yield a diameter such as to provide a snug fit in the passage into which it is introduced, e.g., the bore 32 of the fitting 23 of the example. After being located in its desired longitudinal position the portion A is desirably brazed or otherwise rendered into intimate contact with the adjoining surface. Such operation may be accomplished by allowing some clearance between the passage and the portion A and inserting a thin strip of silver solder therein. Heat is then applied to the exterior of the assembly.
It will be noted that the portion B will, together with the adjacent passage surface 32, will define a conduit 54 substantially of elliptical transverse aspect through which the air may pass from the opeiings 18 into the leg 25 of the fitting 23. By reason of the intimacy of contact between the portion A of the heater and the adjoining wall surface the body of. the device will be heated by conduction and that the Wall surfaces of the conduit 54 will be heated by conduction and radiation.
FIGS. 3 and 4 are cross sections similar to that of FIG. 2 to illustrate alternative embodiments. In these cases the air passage or passages are indicated at 54a and 54b, and the heater or heaters at 3111 and 31b. In either case heat is supplied to the air passage or passages and to the sheath. 1n the embodiment of FIG. 4 heat transfer may be implemented by soldering or brazing as indicated.
A preferred construction of heater comprises a spool 61 of ceramic material (FIG. of beryllia, alumina or the like having flanges 62 flanking a cylindrical winding portion 63 of smaller diameter than the flanges. The flanges are relieved for a portion of their periphery by flats 64-64 to define, with the sheath blank 71 suitable spaces 60-.60 for a purpose to appear.
The resistance wire 65, e.g., Nichrome, is helically Wound on the portion 63 either in juxtaposed coils or in a helical groove provided therein, and the ends are connected by welding or otherwise to terminal leads 66and, 67 passing through bores through the spool 61. The leads One v termined diameter and of a length more than spanning the overall length of the spool 61. is tack-brazed at its ends to the periphery of the blank 71. For example, for a blank 71 of diameter the rod will be As" diameter, and for a spool of length 2" the rod will be 3" long, thereby to extend beyond the spool approximately at each end.
A pellet 86 of friable refractory material is deposited in the tube 71 from the right hand end. This pellet is a cylinder which is longitudinally truncated over its length to provide diametrically opposite flats 91-91, in turn defining with the tube 71 a pair of spaces 9292. Adjacent its ends the pellet is notched on both sides as indicated at 9494. While notching at one end only is sufllcient for the intended temporary use, both ends are desirably made the same to eliminate concern by the operator as to which end of the pellet is to be inserted first.
Following insertion of the pellet 86, the heater core assembly comprising the spool, its winding and leads are assembled with another pellet 97 bored to receive the terminal leads 67 therethrough and these parts are inserted in the blank 71 to abut the pellet 91. Since the position of the leads 67 is desirably definitely angularly related to the portion B of the heater the same are orientated as shown with respect to the rod 84 which may then be removed. Although some endwise clearances between the components are shown on the drawing for clarity of comprehension no clearance need actually exist. The pellet 97 is provided with two diametrically opposite flats 98-98 (FIG. 9) similarly to the pellet 86 to provide a pair of spaces 99--99.
Now the left end of the sheath blank 71 is taped closed and, with the tube held vertically a suitable pulverulentrefractory, e.g., powdered magnesium oxide is poured into the upper end. Meanwhile the tube is vibrated in any suitable jogging device to insure that all voids are filled.
The spaces 9999, -60 and 92-92 allow the powder to pass through to the left hand end and to fill all other voids. Vibration is continued until the powder is wellcompacted. Passage of the powder into the spaces '9292 is facilitated by the notches 9494 acting as funnels. The right hand end (presently the uppermost end) is then taped shut and the assembly (FIG. 5) is then turned end for end. The tape is removed from the left end (presently the uppermost end) and that end welded or otherwise closed. A metallic plug or disc may be used as part of this plugging operation. The assembly is turned end for end and vibrated once more as further assurance that the powder is a well-compacted mass. It will be understood that such mass remains until the heater assembly 31 is cut from the processing assembly, and that the powder surrounding the winding serves to insulate and to provide additional stability for such winding throughout the life of the heater.
The assembly of FIG. 5 is now swaged to its final diameter, in the example, 78", and then annealed.
The rod 84 is re-affixed in its original position and assembly is passed through suitable swaging dies whereby the rod 84 is forced into the sheath blank 71 (FIG. 10) to form the indented peripheral re-entrant portion B. During this step the desired finished diameter, namely 0.343", is also imparted to the sheath.
As a result of the swaging steps it will be comprehended that the spool 61 will be crushed and the winding there-v on deformed congruently to the indentation, that thematrix of refractory powder will be compressed thereby to improve the integration thereof with the heater assembly 31, and that the pellets 91 and 97 will be crushed. However, since these latter constitute no part of the final assembly their fate is immaterial.
The sheath blank 71 is now severed adjacent both ends of the spool 61, care being taken not to disturb the leads 6767. The scrap, including the rod 84,, is discarded, it being recalled that this rod was secured only at its ends. The outer end of the heater 31 (FIG. 1) is closed by a brazed-on closure plate 101 of proper outline and the heater is now ready for incorporation with the fitting 23, in the manner previously described.
By reason of the process steps described in connection With FIGS. 5 and 6 it will have become evident that, by employing a rod 84 somewhat longer than the eventual sheath 51 and extending the same beyond the ends thereof the entire useful length of the sheath is provided with the channel 54; and that the ample support given to the spool 61 by the tightly juxtaposed pellets 91 and 97 allows the flanges 6262 of the spool to be crushed during swaging without the hazard of pieces being bodily broken off the same. Stated otherwise these flanges, even though fractured, remain virtually intact, the pieces thereof being tightly bound by the sheath constricted therearound.
In the case of the alternative embodiment of FIG. 3 it will now become apparent that each of the heaters 31a is fabricated in a manner similar to that described in connection with FIG. 5 and, in the case of that form of the invention heater shown in FIG. 4 the rod 84 will be in multiple, spaced apart about the periphery of the sheath blank 71.
While We have shown particular embodiments of our invention, it will be understood, of course, that we do not wish to be limited thereto since many modifications may be made and we, therefore, contemplate by the appended claims to cover any such modifications as fall within the true spirit and scope of our invention.
We claim:
1. The method of fabricating an electrical heater of the type comprising a metallic sheath enclosing a conductive element of high electrical resistance and in which the element is spaced from, and supported relative to the sheath by a matrix of electrically-insulating material, which comprises: providing a sheath of tubular form, assemblying the element on a support of friable, electrically-insulating material, said support being a slip fit in the sheath, inserting the support with the thereon-supported element in the sheath, inserting a friable plug in at least one end of the sheath abutting one end of the support, temporarily attaching an incompressible rod-like indenting member to the sheath wall, said member being at least coextensive longitudinally with said support, forcing the member into the sheath wall to deform the sheath and crush the support and removing said member.
2. The method in accordance with claim 1 characterized by the additional step of trimming the deformed sheath adjacent the said one end of the support.
3. The method in accordance with claim 1 wherein the member is forced into the sheath by swaging.
4. The method in accordance with claim 1 further characterized in that said indenting member is of uniform cross section.
5. The method of fabricating an electrical heater of the type comprising a metallic sheath enclosing a conductive element of high electrical resistance and in which the element is spaced from, and supported relative to the sheath by a matrix of electrically-insulating material, which comprises: providing a sheath of tubular form, assembling the element on a support of friable, electrically-insulating material, inserting the support with the thereon-supported element in the sheath, inserting a friable plug in the sheath at each end of the support, temporarily attaching an incompressible rod-like indenting member to the sheath wall, said member being at least coextensive longitudinally with said support, forcing the member into the sheath wall to deform the sheath and crush the support and removing said member.
6. The method in accordance with claim 5 characterized by the additional step of trimming the deformed sheath adjacent the ends of the crushed support.
7. The method in accordance with claim 5 wherein the member is forced into the sheath by swaging.
8. The method in accordance with claim 5 further characterized in that said indenting member is of uniform cross section.
References Cited by the Examiner UNITED STATES PATENTS Re. 19,567 5/1935 Wiegand 29155.65 Re. 23,449 1/1952 Freeman 21919 1,477,602 12/1923 Simon 21938.3 X 1,613,426 1/1927 Wiegand 29155.65 2,130,715 9/1938 Coupier 29155.68 2,381,327 8/1945 Woodman et al. 219--19 X 2,404,978 7/1946 Morton 219-19 X 2,428,900 10/1947 Wiegand 29-15564 2,866,062 12/1958 Fisher 219-19 X 2,899,664 8/1959 Andrews 29-155.67 2,933,805 4/1960 McOrlly 29-155.65 2,947,842 8/1960 Rook 21919 WHITMORE A. WILTZ, Primary Examiner.
MAX L. LEVY, JOHN F. CAMPBELL, Examiners.
Claims (1)
1. THE METHOD OF FABRICATING AN ELECTRICAL HEATER OF THE TYPE COMPRISING A METALLIC SHEATH ENCLOSING A CONDUCTIVE ELEMENT OF HIGH ELECTRICAL RESISTANCE AND IN WHICH THE ELEMENT IS SPACED FROM, AND SUPPORTED RELATIVE TO THE SHEATH BY A MATRIX OF ELECTRICALLY-INSULATING MATERIAL, WHICH COMPRISES: PROVIDING A SHEATH OF TUBULAR FORM, ASSEMBLYING THE ELEMENT ON A SUPPORT OF FRIABLE, ELECTRICALLY-INSULATING MATERIAL, SAID SUPPORT BEING A SLIP FIT IN THE SHEATH, INSERTING THE SUPPORT WITH THE THEREON-SUPPORTED ELEMENT IN THE SHEATH, INSERTING A FRIABLE PLUG IN AT LEAST ONE END OF THE SHEATH ABUTTING ONE END OF THE SUPPORT, TEMPORARILY ATTACHING AN INCOMPRESSIBLE ROD-LIKE
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US139209A US3229358A (en) | 1961-09-19 | 1961-09-19 | Process of manufacturing heating means for de-icing static ports and the like |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US139209A US3229358A (en) | 1961-09-19 | 1961-09-19 | Process of manufacturing heating means for de-icing static ports and the like |
Publications (1)
Publication Number | Publication Date |
---|---|
US3229358A true US3229358A (en) | 1966-01-18 |
Family
ID=22485576
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US139209A Expired - Lifetime US3229358A (en) | 1961-09-19 | 1961-09-19 | Process of manufacturing heating means for de-icing static ports and the like |
Country Status (1)
Country | Link |
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US (1) | US3229358A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3898431A (en) * | 1974-01-29 | 1975-08-05 | Atomic Energy Commission | Tubular electric heater with a thermocouple assembly |
US4039778A (en) * | 1976-07-01 | 1977-08-02 | Rama Corporation | Electric cartridge heater with a multiple thermocouple assembly |
US4349727A (en) * | 1973-07-25 | 1982-09-14 | Southport Enterprises, Inc. | Heater unit |
US4468556A (en) * | 1982-08-09 | 1984-08-28 | Emerson Electric Co. | Electric heating elements |
FR2556167A1 (en) * | 1983-12-03 | 1985-06-07 | Hotset Heizpatronen Zubehoer | ELECTRIC HEATER BODY WITH SOCKET |
US4965436A (en) * | 1973-07-25 | 1990-10-23 | Southport Enterprises | Heater unit |
US20130264326A1 (en) * | 2012-04-04 | 2013-10-10 | Gaumer Company, Inc. | High Velocity Fluid Flow Electric Heater |
Citations (12)
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US1477602A (en) * | 1921-04-25 | 1923-12-18 | Simon Maurice | Electrical heating unit |
US1613426A (en) * | 1923-08-31 | 1927-01-04 | Edwin L Wiegand | Process of producing electrical heating element |
USRE19567E (en) * | 1935-05-07 | Method of forming electrical | ||
US2130715A (en) * | 1934-07-19 | 1938-09-20 | Coupier Marcel Marie Jo Eugene | Electric heating element |
US2381327A (en) * | 1944-02-19 | 1945-08-07 | Westinghouse Electric Corp | Pitot static air-speed indicator |
US2404978A (en) * | 1944-02-10 | 1946-07-30 | Westinghouse Electric Corp | Fluid speed indicator |
US2428900A (en) * | 1940-10-21 | 1947-10-14 | Wiegand Co Edwin L | Electrical heating element |
USRE23449E (en) * | 1952-01-15 | Electric internal-combustion engine | ||
US2866062A (en) * | 1956-03-05 | 1958-12-23 | Trent Inc | Electrical heating elements |
US2899664A (en) * | 1956-02-27 | 1959-08-11 | Electric heating units and methods of making the same | |
US2933805A (en) * | 1954-02-19 | 1960-04-26 | Wiegand Co Edwin L | Electric heaters |
US2947842A (en) * | 1958-06-09 | 1960-08-02 | Gen Electric | Internally fused electric heater |
-
1961
- 1961-09-19 US US139209A patent/US3229358A/en not_active Expired - Lifetime
Patent Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
USRE19567E (en) * | 1935-05-07 | Method of forming electrical | ||
USRE23449E (en) * | 1952-01-15 | Electric internal-combustion engine | ||
US1477602A (en) * | 1921-04-25 | 1923-12-18 | Simon Maurice | Electrical heating unit |
US1613426A (en) * | 1923-08-31 | 1927-01-04 | Edwin L Wiegand | Process of producing electrical heating element |
US2130715A (en) * | 1934-07-19 | 1938-09-20 | Coupier Marcel Marie Jo Eugene | Electric heating element |
US2428900A (en) * | 1940-10-21 | 1947-10-14 | Wiegand Co Edwin L | Electrical heating element |
US2404978A (en) * | 1944-02-10 | 1946-07-30 | Westinghouse Electric Corp | Fluid speed indicator |
US2381327A (en) * | 1944-02-19 | 1945-08-07 | Westinghouse Electric Corp | Pitot static air-speed indicator |
US2933805A (en) * | 1954-02-19 | 1960-04-26 | Wiegand Co Edwin L | Electric heaters |
US2899664A (en) * | 1956-02-27 | 1959-08-11 | Electric heating units and methods of making the same | |
US2866062A (en) * | 1956-03-05 | 1958-12-23 | Trent Inc | Electrical heating elements |
US2947842A (en) * | 1958-06-09 | 1960-08-02 | Gen Electric | Internally fused electric heater |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4349727A (en) * | 1973-07-25 | 1982-09-14 | Southport Enterprises, Inc. | Heater unit |
US4965436A (en) * | 1973-07-25 | 1990-10-23 | Southport Enterprises | Heater unit |
US3898431A (en) * | 1974-01-29 | 1975-08-05 | Atomic Energy Commission | Tubular electric heater with a thermocouple assembly |
US4039778A (en) * | 1976-07-01 | 1977-08-02 | Rama Corporation | Electric cartridge heater with a multiple thermocouple assembly |
US4468556A (en) * | 1982-08-09 | 1984-08-28 | Emerson Electric Co. | Electric heating elements |
FR2556167A1 (en) * | 1983-12-03 | 1985-06-07 | Hotset Heizpatronen Zubehoer | ELECTRIC HEATER BODY WITH SOCKET |
US20130264326A1 (en) * | 2012-04-04 | 2013-10-10 | Gaumer Company, Inc. | High Velocity Fluid Flow Electric Heater |
US9074819B2 (en) * | 2012-04-04 | 2015-07-07 | Gaumer Company, Inc. | High velocity fluid flow electric heater |
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