US987361A - Engine heat-radiating structure. - Google Patents
Engine heat-radiating structure. Download PDFInfo
- Publication number
- US987361A US987361A US30452906A US1906304529A US987361A US 987361 A US987361 A US 987361A US 30452906 A US30452906 A US 30452906A US 1906304529 A US1906304529 A US 1906304529A US 987361 A US987361 A US 987361A
- Authority
- US
- United States
- Prior art keywords
- blade
- cylinder
- blades
- heat
- screw
- 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
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/12—Tubular 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
- F28F1/24—Tubular 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 transversely
- F28F1/30—Tubular 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 transversely the means being attachable to the element
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S29/00—Metal working
- Y10S29/012—Method or apparatus with electroplating
-
- 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
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/49231—I.C. [internal combustion] engine making
Definitions
- Figure 1 1s a part-sectional view of an en gine' cylinder having affixed thereto two blades of a built-up radiator structure.
- Fig. 2 is an elevation of a fragment of one of said blades, the cylinder being shown in section.
- Fig. 3 is a fragmentary section of a modified embodiment of my invention, and
- Fig. 4 a fragmentary elevation thereof.
- Figs. 5 and 6 are like views of another embodiment of my invention, and, Fig. 7 is an elevation with part in section, of a fragment of a locking ring shown in Figs. 5 and 6.
- 10 indicates an engine cylinder body, of any size or proportion, ex- I teriorly screw -threaded, as shown at 11,
- the radiator structure is built up preferably of a series of blade units, each comprising an annular member, screw-threaded for engagement with the threads 11, at its inner periphery, and preferably provided with apertures for air circulation and projections for heat distribution.
- each blade unit 13 has a thickened base portion 14, of
- each ,blade is provided with apertures 15 and'projections 16, the projections and apertures being formed by striking up from the blade semi-circular lips, which constitute the projections 16 and leave holes 15 in the blade.
- washers or thin rings 17 are provided between the"blade-bases, or enlargements, to receive the enlargements in contact therewith.
- Suchrings 17 are in screw-threaded engagemenflwit-h the cylinder and arepreferably wide enough to form small fins, to project between the tapering parts of the blade enlargements, and they afford means for compensating for slight irregularities of the side surfaces of the blade enlargements should such exist, and insure proper heat conductivity between the adjoining blade enlargements.
- Figs. 3 and 4 I have shown a somewhat similar arrangement, the blades 12% having base enlargements 1%, but having tions 16 and having said projections 16 provided on both sides of the blade to afl'ord a much larger area of heat disseminating surface than is provided by the arrangement shown in Figs. 1 and-2.
- Figs. 5 and 6 I show an arrangement embodying blades 13, with apertures and projections 15", 16 like those shown in Figs. 1 and 2, theentire blade structure being of uniform thickness and screw-threaded upon the cylinder.
- Spacing lock nuts or rings 18, each preferably channeled peripherally, as shown at 19 are provided between the blades to hold them properly spaced, lock them firmly together, strengthen the cylinder, and, by the large surface exposure ob tained by channeling, afford a good heat disseminating medium.
- Said nuts or rings 18, in the modified form are of sufficient width to encompass a. plurality of threads of the cylinder, corresponding to the similar formation of the blades 13 of Fig. 1.
- the screw-- thread feature of my invention not only affords a new method of attaching bladesand rings, but it also renders a comparative easy passage for heat from the cylinder body to the blades through the intimate union of the interlocking threads, and renders the structure substantially homogeneous in efl'ect while possessing '-all the advantage of the assemblage of parts.
- the blades themselves provide for circulation therethrough and, by the provision of projections, expose a large heat dissemi nating area in the path of travel of circulating air. a
- the advantages of the blade structures are, in a measure, retained if the blades be shrunk, brazed or otherwise secured on the cylinder body,
- a cylinder body providing on its outer surface uniformly-spaced, re atively fine pitch, screw-threads, said threads having an electroplated coat of metal thereover, and separable parts including a series of independent annular blades having portions struck therefrom to form air-circulation apertures and heat-dis tributing projections, each said blade having interior screw-threads corresponding with the threads of the cylinder and having an electroplated coat of metal thereover, and a series of soft metal washers each having an electroplated coat of metal thereover, the members of both of said series being screwed over the cylinder in alternating relation and having a uniting electroplated coat of metal applied thereto after they have been assembled.
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- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Geometry (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Description
J. W. HASBURG. ENGINE HEAT RADIATING STRUCTURE.
APPLICATION FILEIDMAR. 6. 1906. 987,361, j Patented Mar.21, 1911.
' 2 SHEETS-SHEET 1.
4;; M I \J. 1 .Z no? Q J. W. HASBURG.
ENGINE HEAT RADIATING STRUCTURE.
APPLICATION FILED MAR.6,190E.
987,361. 7 Patented Mar.21, 1911.
2 SHEETS SHEBT 2 72-65 66 I7zz/e7zZ0/ Ja/zfa' /9 /640 5 Lug JOHN W. HASBURG, OF CHICAGO, ILLINOIS.
ENGINE HEAT-RADIATING STRUCTURE.
Specification of Letters iatent. Patented Mar, 1911,
Application filed March 6, 1906. Serial No. 304,529.
To all whom it may concern:
Be it known that I, Journ -W. Hasnunc,
a citizen of'the United States, residing at .novel construction and arrangement of the radiating blades or fins and intermediate washers, and to provide a built-up radiator structure easy of application to a cylinder body, lending strength to the said body and afiording maximum heat-conductivity between the blade structures and the body.
Other and further objects of my invention will become apparent to those skilled in the art from the following description, taken in conjunction with the accompanying drawings, wherein;
Figure 1 1s a part-sectional view of an en gine' cylinder having affixed thereto two blades of a built-up radiator structure. Fig. 2 is an elevation of a fragment of one of said blades, the cylinder being shown in section. Fig. 3 is a fragmentary section of a modified embodiment of my invention, and
.Fig. 4 a fragmentary elevation thereof.
Figs. 5 and 6 are like views of another embodiment of my invention, and, Fig. 7 is an elevation with part in section, of a fragment of a locking ring shown in Figs. 5 and 6.
Throughout the drawings like numerals of reference refer always to like parts.
In the drawings, 10 indicates an engine cylinder body, of any size or proportion, ex- I teriorly screw -threaded, as shown at 11,
throughout its length and preferably termina'ting atone end in a flange 10' to which may be securedthe cylinder head 12.
The radiator structure is built up preferably of a series of blade units, each comprising an annular member, screw-threaded for engagement with the threads 11, at its inner periphery, and preferably provided with apertures for air circulation and projections for heat distribution.
Referring now to Figs. 1 and 2, each blade unit 13 has a thickened base portion 14, of
size sufficient to include a plurality of the screw-threads on the cylinder, forming a relatively strong central zone, gradually taporing outward, and each ,blade is provided with apertures 15 and'projections 16, the projections and apertures being formed by striking up from the blade semi-circular lips, which constitute the projections 16 and leave holes 15 in the blade. I
In the assembling of the structure, washers or thin rings 17 preferably of copper, are provided between the"blade-bases, or enlargements, to receive the enlargements in contact therewith. Suchrings 17 are in screw-threaded engagemenflwit-h the cylinder and arepreferably wide enough to form small fins, to project between the tapering parts of the blade enlargements, and they afford means for compensating for slight irregularities of the side surfaces of the blade enlargements should such exist, and insure proper heat conductivity between the adjoining blade enlargements.
In Figs. 3 and 4:, I have shown a somewhat similar arrangement, the blades 12% having base enlargements 1%, but having tions 16 and having said projections 16 provided on both sides of the blade to afl'ord a much larger area of heat disseminating surface than is provided by the arrangement shown in Figs. 1 and-2.
In Figs. 5 and 6 I show an arrangement embodying blades 13, with apertures and projections 15", 16 like those shown in Figs. 1 and 2, theentire blade structure being of uniform thickness and screw-threaded upon the cylinder. Spacing lock nuts or rings 18, each preferably channeled peripherally, as shown at 19 are provided between the blades to hold them properly spaced, lock them firmly together, strengthen the cylinder, and, by the large surface exposure ob tained by channeling, afford a good heat disseminating medium. Said nuts or rings 18, in the modified form, are of sufficient width to encompass a. plurality of threads of the cylinder, corresponding to the similar formation of the blades 13 of Fig. 1.
In connection with any of these constructions I preferably coat each of the parts before assembling, and the whole structure after it is assembled,with cop er, by electro-' plating, for the ,purposes 0 bonding the parts together for heat communication, rendering the structure more heat conductive, and giving a pleasing finish. It will be seen that. in each of these constructions intimate strengthened by the addition of t e encompassing, (peripherally uninterrupted bladeunits," an the blade locking members, and that ease of construction and facility in assembling are insured. Thus, the screw-- thread feature of my invention not only affords a new method of attaching bladesand rings, but it also renders a comparative easy passage for heat from the cylinder body to the blades through the intimate union of the interlocking threads, and renders the structure substantially homogeneous in efl'ect while possessing '-all the advantage of the assemblage of parts.
The blades themselves provide for circulation therethrough and, by the provision of projections, expose a large heat dissemi nating area in the path of travel of circulating air. a The advantages of the blade structures are, in a measure, retained if the blades be shrunk, brazed or otherwise secured on the cylinder body,
While I have herein described in some detail specific embodiments of my invention, which I believe to be newand advantageous,
it will be apparent to those skilled in the art that other changes might be made in the s ecific construction without departure .from t e spirit and scope'of' my invention.
" Having thus described myinvention, what I claim and desire to secure by Letters Patent of the United States, is:
1. The combination with an exteriorly screw-threaded cylinder body, of a series of annular blades and a series of soft metal washers, the members of one of said series being enlargled adjacent the cylinder body and screw-t readed to embrace a plurality of the threads of the cylinder body, and the members of both of said series bein screwed over the cylinder in alternating re ation.
2. In a structure of the character described, the combination of a cylinder body providing on its outer surface uniformly-spaced, re atively fine pitch, screw-threads, said threads having an electroplated coat of metal thereover, and separable parts including a series of independent annular blades having portions struck therefrom to form air-circulation apertures and heat-dis tributing projections, each said blade having interior screw-threads corresponding with the threads of the cylinder and having an electroplated coat of metal thereover, and a series of soft metal washers each having an electroplated coat of metal thereover, the members of both of said series being screwed over the cylinder in alternating relation and having a uniting electroplated coat of metal applied thereto after they have been assembled.
In testimony whereof I hereunto set my hand in the presence of twowitnesses.
, JOHN W. HASBURG. In the presence of Gno. T. MAY, J12, MARY F. ALLEN.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US30452906A US987361A (en) | 1906-03-06 | 1906-03-06 | Engine heat-radiating structure. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US30452906A US987361A (en) | 1906-03-06 | 1906-03-06 | Engine heat-radiating structure. |
Publications (1)
Publication Number | Publication Date |
---|---|
US987361A true US987361A (en) | 1911-03-21 |
Family
ID=3055701
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US30452906A Expired - Lifetime US987361A (en) | 1906-03-06 | 1906-03-06 | Engine heat-radiating structure. |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3104136A (en) * | 1960-05-19 | 1963-09-17 | Henry H Merriman | Bushing |
US3687194A (en) * | 1969-06-13 | 1972-08-29 | Scholl Dr Ing Gunter | Ribbed pipe unit |
US4638854A (en) * | 1983-06-15 | 1987-01-27 | Noren Don W | Heat pipe assembly |
-
1906
- 1906-03-06 US US30452906A patent/US987361A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3104136A (en) * | 1960-05-19 | 1963-09-17 | Henry H Merriman | Bushing |
US3687194A (en) * | 1969-06-13 | 1972-08-29 | Scholl Dr Ing Gunter | Ribbed pipe unit |
US4638854A (en) * | 1983-06-15 | 1987-01-27 | Noren Don W | Heat pipe assembly |
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