US1932610A - Radiation device - Google Patents

Radiation device Download PDF

Info

Publication number
US1932610A
US1932610A US639416A US63941632A US1932610A US 1932610 A US1932610 A US 1932610A US 639416 A US639416 A US 639416A US 63941632 A US63941632 A US 63941632A US 1932610 A US1932610 A US 1932610A
Authority
US
United States
Prior art keywords
fins
tube
strip
edge
base strip
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US639416A
Inventor
Tilley Edwin Frost
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US639416A priority Critical patent/US1932610A/en
Application granted granted Critical
Publication of US1932610A publication Critical patent/US1932610A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28FDETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F1/00Tubular elements; Assemblies of tubular elements
    • F28F1/10Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
    • F28F1/12Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element
    • F28F1/34Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending obliquely
    • F28F1/36Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only outside the tubular element and extending obliquely the means being helically wound fins or wire spirals

Definitions

  • the objects of the invention are to increase the thermal efficiency and to provide a simple, practical, inexpensive and readily manufactured form of construction, suitable for many uses in the fields of heating, cooling, air conditioning, etc.
  • Fig. 1 is a broken sectional view of one form of the invention.
  • Fig. 2 is an enlarged broken detail 0! the strip member which is spiralled about the tube to form the extended radiating surface.
  • Fig. 3 is a broken side view illustrating the application of the strip member to the conducting tube.
  • Fig. 3a is a fragmentary detail, illustrating the feature of twisting the fins.
  • Fig. 4 is a broken part sectional view of the strip spiralled in more compacted form on the tube and the latter connected with the header or support by an expansion joint.
  • Figs. 5, 6 and '7 are broken sectional details, illustrating various modifications in the angle of the radiating fingers.
  • the fins may be angled in various ways.
  • the ends of the fins are shown as twist- 0 ed out of parallelism with the edges of the strip and into substantial parallelism with each other in the final form, so as to form between them the substantially parallel.
  • the strip may be coiled upon the tubing in as closely or as widely separated convolutions as considered desirable.
  • the coils of the base strip are laid in spaced relation as Indicated at 15,. Fig. 4, to leave space for solder or tinning material, which may be employed to form a solid metal-to-metal seal between the edges of the base strip and the supporting tube.
  • the outstanding fins may be bent bodily at an acute angle as at 16, in Fig. 5, to overlie the base str'p; stand out at a right angle from the .base strip as at 17 in Fig. 6; or be bent at an obtuse angle as at 18 in Fig. 'l, away from the base strip.
  • the fins may be otherwise angled, curved or sloped to meet different requirements or provide different characteristics.
  • the fins may be made as long as needed for greatest efficiency in the transfer of heat and because of this possible high transfer rate, special expansion connections between the tubes and the header or supporting structure are desirable.
  • the tube is shown as having a plurality of expanded cross corrugations 19 therein, adjacent the end, where it is connected with the header or supporting structure 20, so that it may expand or contract as required, without breaking or injuriously affecting the jo nt with the header.
  • the depth or extent of the fin has been limited by the maximum stretch of the metal.
  • the fins can be made of any desired length, or the tube may be of any desired size or shape. The desirable combination of large tube and long fins is possible, the same forming an ideal assembly for concealed or open radiation for domestic purposes.
  • Theuseoithenewradiationdevice intansystems where power consideration is important, is particularly advantageous because of the minimum fiow resistance uttered by the fins.
  • Withtheinventiommorerowsottubes maybe used without consuming more power than heretoiore used with a lesser number oi tubes having continuous fins.
  • This splitting of the air into multitudinous generally parallel thin layers thus both reduces the impedance and increases the heat transfer.
  • the strips after being slotted at 11, 13, may be tormed through a die to the generally L-shaped position shown in Fig. 2 and in the helical winding of the base strip on the tube, the fins may be twisted transversely near their junction with the tube, as at 21, in Figs. 3 and 30 across from the inner edge of one serration to the outer edge 0! the next adjoining indentation.
  • the fins then form a series of substantially fiat parallel blades for cutting the air into thin parallel layers without turbulence or breaking the fiow.
  • the indentations in the edge of the base strip may be made as deep or as shallow as considered desirable. Deeper indentations permit wider fins and allow for more abrupt twist at the root of the fins with the base strip. This twisting of the fins gives them an added longitudinal stillness making it possible to use relatively thin sheet materialandkeep thefinssslongasdesirablei'or practical efilcieney.
  • Aheat radiationdevice comprisingincombination with a tube, a narrow base strip wound helically in close fiatwise engagement with said tube and having indentations in one edge of the same and angularly projecting radiating fins between said indentations said fins being each aligned at one edge with the inner portion of one of said indentations and aligned at the opposite edge with the outer portion of the next adjoining indentation and thereby positioned substantially parallel to cut an air stream fiowing past the tube in multitudinous parallel thin layers.
  • a tubular member and an extended surface unit comprising a narrow base strip wound in fiatwise engagement on said tubular member and having elongated fins projecting angularly from one edge or the same, said fins being separated from each other by notches extend'ng into the edge of the base strip between said fins and said fins being twisted transversely of their length across from the notch at one side to the notch at the opposite side of the same into substantial parallelism with each other to cut an ar stream fiowing past the tubular member into multitudinous parallel thin layers.
  • a heat radiation device comprising in combfnation with a tube, a narrow base strip wound helically in close fiatwise engagement with said tube and having one edge substantially continuous. and the other edge formed with notches therein and having radiating fins projecting angularly therefrom between said notches and a bonding material between the tube and said notched edge portion of the finned strip.

Description

Oct. 31, 1933. E. F. TILLEY 1,932,610
RADIATION DEVICE Filed Oct. 25, 1932 INVENTOR AT RNEY Patented Oct. 31, 1933 PATENT OFFICE UNITED STATES 4 Claim.
This invention relates to heat transmission broadly, whether the fiow of heat be from hot to cold or from cold to hot.
The objects of the invention are to increase the thermal efficiency and to provide a simple, practical, inexpensive and readily manufactured form of construction, suitable for many uses in the fields of heating, cooling, air conditioning, etc.
The foregoing and other desirable objects are attained by the novel features of construction, combinations and relations of parts particularly described and hereinafter broadly claimed.
The drawing accompanying and forming part of the specification illustrates certain practical embodiments of the invention, but with the understanding that the actual physical structure may be modified as regards this disclosure, all within the true intent and broad scope of the claims.
Fig. 1 is a broken sectional view of one form of the invention.
Fig. 2 is an enlarged broken detail 0! the strip member which is spiralled about the tube to form the extended radiating surface.
Fig. 3 is a broken side view illustrating the application of the strip member to the conducting tube. Fig. 3a is a fragmentary detail, illustrating the feature of twisting the fins.
Fig. 4 is a broken part sectional view of the strip spiralled in more compacted form on the tube and the latter connected with the header or support by an expansion joint.
Figs. 5, 6 and '7 are broken sectional details, illustrating various modifications in the angle of the radiating fingers.
The primary surface is provided by a tube 8, carrying the heating or cooling medium and the secondary or extended surface is provided by a strip 9, wound helically about the tube and having radiating fins 10 projecting therefrom.
Details of the secondary radiating member will be clear from Fig. 2, where the fin portions are shown as integral extensions from one edge of the base strip, bent up at right angles thereto and separated from each other by cuts 11, ex-
tending down past the line of bend 12, in the gagement with the tube or pipe as indicated" particularly in Fig. 3 and, since the separate fins are no limitation to the bending of the base strip, these fins may be made just as long as is efficient for heat transmission purposes.
The fins may be angled in various ways. Thus in Fig. 3, the ends of the fins are shown as twist- 0 ed out of parallelism with the edges of the strip and into substantial parallelism with each other in the final form, so as to form between them the substantially parallel. air passes indicated at 14. This has the effect of breaking up the 5 cross fiow of air into multitudinous parallel strata, practically without retarding the fiow and therefore without consuming useful energy.
The strip may be coiled upon the tubing in as closely or as widely separated convolutions as considered desirable. In a preferred construction however, the coils of the base strip are laid in spaced relation as Indicated at 15,. Fig. 4, to leave space for solder or tinning material, which may be employed to form a solid metal-to-metal seal between the edges of the base strip and the supporting tube.
The outstanding fins may be bent bodily at an acute angle as at 16, in Fig. 5, to overlie the base str'p; stand out at a right angle from the .base strip as at 17 in Fig. 6; or be bent at an obtuse angle as at 18 in Fig. 'l, away from the base strip. These are merely examples however and it will be understood that the fins may be otherwise angled, curved or sloped to meet different requirements or provide different characteristics.
The fins may be made as long as needed for greatest efficiency in the transfer of heat and because of this possible high transfer rate, special expansion connections between the tubes and the header or supporting structure are desirable. In Fig. 4, the tube is shown as having a plurality of expanded cross corrugations 19 therein, adjacent the end, where it is connected with the header or supporting structure 20, so that it may expand or contract as required, without breaking or injuriously affecting the jo nt with the header.
In prior constructions employing .a continuous strip helically wound on the primary surface, the depth or extent of the fin has been limited by the maximum stretch of the metal. In the present inventon there is no such limitation and the fins can be made of any desired length, or the tube may be of any desired size or shape. The desirable combination of large tube and long fins is possible, the same forming an ideal assembly for concealed or open radiation for domestic purposes.
In cooling and refrigeration work the formation of the separate fins prevents frosting from blockingthepassageotairandwhenthefinsare angled on a downward slant, any moisture fiows toanddropsofitheendsotthefins,thusautomatically clearing the primary member.
Theuseoithenewradiationdevice intansystems, where power consideration is important, is particularly advantageous because of the minimum fiow resistance uttered by the fins. Thus withtheinventiommorerowsottubesmaybe used without consuming more power than heretoiore used with a lesser number oi tubes having continuous fins. This splitting of the air into multitudinous generally parallel thin layers thus both reduces the impedance and increases the heat transfer.
Theserrations l3intheedge otthebasestrip prevent tearing of the strip 'as it is tightly wound upon the tube and aid in the twisting of the fins from the inclined or helical lines o! the base strip to the generally parallel position in line with the air fiow.
In practical manufacturing operations the strips, after being slotted at 11, 13, may be tormed through a die to the generally L-shaped position shown in Fig. 2 and in the helical winding of the base strip on the tube, the fins may be twisted transversely near their junction with the tube, as at 21, in Figs. 3 and 30 across from the inner edge of one serration to the outer edge 0! the next adjoining indentation. The fins then form a series of substantially fiat parallel blades for cutting the air into thin parallel layers without turbulence or breaking the fiow.
The indentations in the edge of the base strip may be made as deep or as shallow as considered desirable. Deeper indentations permit wider fins and allow for more abrupt twist at the root of the fins with the base strip. This twisting of the fins gives them an added longitudinal stillness making it possible to use relatively thin sheet materialandkeep thefinssslongasdesirablei'or practical efilcieney.
What is claimed is:
1. An radiation unit consisting of a coiled strip with indentations in one edge 01 the same and angularly projecting radiating fins between said indentations and aligned at one edge with the inner portion oi said indentations and at the opposite edge with the outer edge of an adjoining indentation.
2. Aheat radiationdevice,comprisingincombination with a tube, a narrow base strip wound helically in close fiatwise engagement with said tube and having indentations in one edge of the same and angularly projecting radiating fins between said indentations said fins being each aligned at one edge with the inner portion of one of said indentations and aligned at the opposite edge with the outer portion of the next adjoining indentation and thereby positioned substantially parallel to cut an air stream fiowing past the tube in multitudinous parallel thin layers.
3. In a heat radiation device, the combination of a tubular member and an extended surface unit, comprising a narrow base strip wound in fiatwise engagement on said tubular member and having elongated fins projecting angularly from one edge or the same, said fins being separated from each other by notches extend'ng into the edge of the base strip between said fins and said fins being twisted transversely of their length across from the notch at one side to the notch at the opposite side of the same into substantial parallelism with each other to cut an ar stream fiowing past the tubular member into multitudinous parallel thin layers.
4. A heat radiation device, comprising in combfnation with a tube, a narrow base strip wound helically in close fiatwise engagement with said tube and having one edge substantially continuous. and the other edge formed with notches therein and having radiating fins projecting angularly therefrom between said notches and a bonding material between the tube and said notched edge portion of the finned strip.
EDWIN FROST 'I'lLLE'Y.
US639416A 1932-10-25 1932-10-25 Radiation device Expired - Lifetime US1932610A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US639416A US1932610A (en) 1932-10-25 1932-10-25 Radiation device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US639416A US1932610A (en) 1932-10-25 1932-10-25 Radiation device

Publications (1)

Publication Number Publication Date
US1932610A true US1932610A (en) 1933-10-31

Family

ID=24563999

Family Applications (1)

Application Number Title Priority Date Filing Date
US639416A Expired - Lifetime US1932610A (en) 1932-10-25 1932-10-25 Radiation device

Country Status (1)

Country Link
US (1) US1932610A (en)

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2471582A (en) * 1944-09-15 1949-05-31 Poole Ralph Heat exchange apparatus for fluids
US2553142A (en) * 1947-05-29 1951-05-15 Johns Manville Method for making heat exchangers
US2643863A (en) * 1948-09-09 1953-06-30 Hydrocarbon Research Inc Recuperative heat exchanger and process of producing same
US2662749A (en) * 1949-01-21 1953-12-15 Hydrocarbon Research Inc Annular flow heat exchanger
US2827551A (en) * 1956-01-27 1958-03-18 Combustion Eng Method of fabricating tubes for heat exchangers
US2870999A (en) * 1955-02-24 1959-01-27 Soderstrom Sten Hilding Heat exchange element
US3185210A (en) * 1962-05-23 1965-05-25 American Schack Company Inc High temperature recuperator
US3240177A (en) * 1962-06-11 1966-03-15 Calumet & Hecla Method for making finned tubing
US3462990A (en) * 1963-12-23 1969-08-26 Reynolds Metals Co Meshing gear apparatus for making heat exchangers
FR2019968A1 (en) * 1968-10-04 1970-07-10 Escoa Corp
US3578952A (en) * 1969-06-05 1971-05-18 Escoa Fintube Corp Tubular electrical heating element with a segmented helical fin
US3907340A (en) * 1974-04-08 1975-09-23 Forney International Flange-boiler insulation cover attachment
US3955552A (en) * 1974-04-18 1976-05-11 Heat Research Corporation Heater for large flows at low pressure losses
US3965885A (en) * 1974-04-18 1976-06-29 Heat Research Corporation Heater for large flows at low pressure losses
DE2840744A1 (en) * 1978-09-15 1980-03-27 Mannesmann Ag Tubular metal heat exchanger with barrel fins mfr. - by rolling strip into split flange Z=section for spiral winding and welding
US4236578A (en) * 1978-05-04 1980-12-02 Condar, Co. Heat exchange enhancement structure
US4258782A (en) * 1979-06-28 1981-03-31 Modine Manufacturing Company Heat exchanger having liquid turbulator
US4742869A (en) * 1985-10-21 1988-05-10 Mitsubishi Denki Kabushiki Kaisha Heat and mass transfer device
AT386073B (en) * 1985-10-03 1988-06-27 Austria Metall Finned (fin-tube) heat exchanger or heater
EP0660062A1 (en) * 1993-07-21 1995-06-28 Babcock-Hitachi Kabushiki Kaisha Heat exchanger using finned tubes
US7166850B2 (en) * 2000-06-06 2007-01-23 Trojan Technologies Inc. Fluid mixing device
US20070224565A1 (en) * 2006-03-10 2007-09-27 Briselden Thomas D Heat exchanging insert and method for fabricating same
US20150345708A1 (en) * 2013-01-08 2015-12-03 Agility Fuel Systems, Inc. Vortex fill

Cited By (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2471582A (en) * 1944-09-15 1949-05-31 Poole Ralph Heat exchange apparatus for fluids
US2553142A (en) * 1947-05-29 1951-05-15 Johns Manville Method for making heat exchangers
US2643863A (en) * 1948-09-09 1953-06-30 Hydrocarbon Research Inc Recuperative heat exchanger and process of producing same
US2662749A (en) * 1949-01-21 1953-12-15 Hydrocarbon Research Inc Annular flow heat exchanger
US2870999A (en) * 1955-02-24 1959-01-27 Soderstrom Sten Hilding Heat exchange element
US2827551A (en) * 1956-01-27 1958-03-18 Combustion Eng Method of fabricating tubes for heat exchangers
US3185210A (en) * 1962-05-23 1965-05-25 American Schack Company Inc High temperature recuperator
US3240177A (en) * 1962-06-11 1966-03-15 Calumet & Hecla Method for making finned tubing
US3462990A (en) * 1963-12-23 1969-08-26 Reynolds Metals Co Meshing gear apparatus for making heat exchangers
FR2019968A1 (en) * 1968-10-04 1970-07-10 Escoa Corp
US3578952A (en) * 1969-06-05 1971-05-18 Escoa Fintube Corp Tubular electrical heating element with a segmented helical fin
US3907340A (en) * 1974-04-08 1975-09-23 Forney International Flange-boiler insulation cover attachment
US3955552A (en) * 1974-04-18 1976-05-11 Heat Research Corporation Heater for large flows at low pressure losses
US3965885A (en) * 1974-04-18 1976-06-29 Heat Research Corporation Heater for large flows at low pressure losses
US4236578A (en) * 1978-05-04 1980-12-02 Condar, Co. Heat exchange enhancement structure
DE2840744A1 (en) * 1978-09-15 1980-03-27 Mannesmann Ag Tubular metal heat exchanger with barrel fins mfr. - by rolling strip into split flange Z=section for spiral winding and welding
US4258782A (en) * 1979-06-28 1981-03-31 Modine Manufacturing Company Heat exchanger having liquid turbulator
AT386073B (en) * 1985-10-03 1988-06-27 Austria Metall Finned (fin-tube) heat exchanger or heater
US4742869A (en) * 1985-10-21 1988-05-10 Mitsubishi Denki Kabushiki Kaisha Heat and mass transfer device
EP0660062A1 (en) * 1993-07-21 1995-06-28 Babcock-Hitachi Kabushiki Kaisha Heat exchanger using finned tubes
EP0660062A4 (en) * 1993-07-21 1996-06-12 Babcock Hitachi Kk Heat exchanger using finned tubes.
US5617916A (en) * 1993-07-21 1997-04-08 Babcock-Hitachi Kabushiki Kaisha Fin tube heat exchanger
EP0915313A2 (en) * 1993-07-21 1999-05-12 Babcock-Hitachi Kabushiki Kaisha Fin tube heat exchanger
EP0915313A3 (en) * 1993-07-21 1999-11-03 Babcock-Hitachi Kabushiki Kaisha Fin tube heat exchanger
US7166850B2 (en) * 2000-06-06 2007-01-23 Trojan Technologies Inc. Fluid mixing device
US20070224565A1 (en) * 2006-03-10 2007-09-27 Briselden Thomas D Heat exchanging insert and method for fabricating same
US8162040B2 (en) 2006-03-10 2012-04-24 Spinworks, LLC Heat exchanging insert and method for fabricating same
US20150345708A1 (en) * 2013-01-08 2015-12-03 Agility Fuel Systems, Inc. Vortex fill

Similar Documents

Publication Publication Date Title
US1932610A (en) Radiation device
US2471317A (en) Heat exchanger
US2347957A (en) Heat exchange unit
US3750709A (en) Heat-exchange tubing and method of making it
US3202212A (en) Heat transfer element
US3197975A (en) Refrigeration system and heat exchangers
US2553142A (en) Method for making heat exchangers
US2703702A (en) Condenser coil assembly
US4305457A (en) High density fin material
US4143710A (en) Heat transfer fin structure
US2310970A (en) Heat exchanger
US2281207A (en) Method of manufacturing heat exchange devices
US2386159A (en) Heat exchanger fin tube
US3643735A (en) Fin and tube heat exchanger
US2070539A (en) Fin tube
US3519070A (en) Heat exchange unit
US4960170A (en) Finned tube and method of making the same
US2963779A (en) Method of making heat exchange structures
CN204227766U (en) A kind of C type hair fin condenser
JP2005127595A (en) Heat exchanger
US2532301A (en) Condenser
US2247243A (en) Heat exchange element and method of making the same
JPS6152592A (en) Heat exchanger core and manufacture thereof
CN102128523A (en) Heat exchanger
US3455379A (en) Finned tube produced from continuous strip