US2491630A - Engine constructed of sections bolted together along vertical plane to form an entire head, block, and crankcase thereof - Google Patents

Engine constructed of sections bolted together along vertical plane to form an entire head, block, and crankcase thereof Download PDF

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Publication number
US2491630A
US2491630A US688485A US68848546A US2491630A US 2491630 A US2491630 A US 2491630A US 688485 A US688485 A US 688485A US 68848546 A US68848546 A US 68848546A US 2491630 A US2491630 A US 2491630A
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engine
cylinder
sections
crankcase
block
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Expired - Lifetime
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US688485A
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Voorhies Carl
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COMPACT POWER PRODUCTS Inc
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COMPACT POWER PRODUCTS Inc
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01BMACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B1/00Reciprocating-piston machines or engines characterised by number or relative disposition of cylinders or by being built-up from separate cylinder-crankcase elements
    • F01B1/12Separate cylinder-crankcase elements coupled together to form a unit
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F7/00Casings, e.g. crankcases or frames
    • F02F7/0021Construction
    • F02F7/0031Construction kit principle (modular engines)
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S123/00Internal-combustion engines
    • Y10S123/06Detachable
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S123/00Internal-combustion engines
    • Y10S123/08Multiple engine units
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49229Prime mover or fluid pump making
    • Y10T29/49231I.C. [internal combustion] engine making
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49893Peripheral joining of opposed mirror image parts to form a hollow body

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Description

Dec. 20, 1949 Q VOQRHIES 2,491,630
ENGINE CONSTRUCTED 0F SECTIONS BOLTED TOGETHER ALONG VERTICAL PLANE TO FORM AN ENTIRE HEAD, BLOCK, AND CRANKCASE THEREOF Filed Aug. 5, 1946 I 3 Shets-Sheet 1 5O 30 40 48 20 22 3G 38 30 L INVENTOR.
CA /PL V0 (mu/5 Dec. 20, 1949 c, VQQRHIES 2,491,630
ENGINE CONSTRUCTED OF SECTIONS BOL'I'ED TOGETHER ALONG VERTICAL PLANE To FORM AN ENTIRE HEAD, BLOCK, AND CRANKCASE THEREOF Filed Aug. 5, 1946 3 Sheets-Sheet 2 Ell IT:- 4
IN VEN TOR.
CH/PL V O ORA A65 Dec. 20, 1949 Q voo s 2,491,630
ENGINE .coNsT ucTED OF SECTIONS BOLTED TOGETHER ALONG VERTICAL PLANE TO FORM AN ENTIRE HEAD, BLOCK, AND CRANKCASE THEREOF Filed Aug. 5, l946 5 Sheets-Sheet 3 I ulnvrmwllln...wllllnnun.
CHRL l/UOAH/ES Patented Dec. 1949 ENGINE CONSTRUCTED or ssorroNs BOLTED roce'rrr PLANE TO FORM AN FICE ER ALONG:v VERTICAL ENTIRE BLOCK, AND QRANKCASE THEREOF Carl Voorhies, Birmingham,
Mich; assignor, by
direct and mesne assignments, to Compactv Power Products, Inc., Detroit, Mich., a corporation of Michigan Application August 5,1946, Serial No. 688,485
Claims. 1
This invention relates to engines and more particularly to a novel form of construction thereof. A
Broadly the invention comprehends the provision of an engine of vertically split cylinder construction wherein the entire head, block, and crankcase thereof are formed of as few as two half sections bolted or otherwise suitably secured together.
Although numerous engines of partially split or sectionalized cylinder construction have been devised, none have previously provided a structure such as the instant invention wherein the engine cylinder is split entirely through the head, block. and crankcase.
An object of the invention is the provision of simple and economical sectionalized engine.
Another object of the'invention is the provision of an engine of sectionalized cylinder construction comprising a minimum number of of lightweight construction.
A further object of the invention is the proparts and I vision of an engine of vertically split cylinder construction permitting of the bolting together of a multiple of cylinders in accordance with requirements.
A still further object of the invention is the provision of an engine cylinder that can be formed of die cast sections bolted together along a vertical plane to form the entire head, block, and crankcase thereof.
Othenobiects and advantages of the invention will appear from the following description taken in connection with the drawings, forming a part of the specification; and in which:
Fig. 1 is a top plan, partially sectionalized view of an engine of split cylinder construction comprising a pair of cylinders bolted together;
Fig. 2 .is aside plan view of Fig. 1 partially sectionalized;
Fig. 3 is an end plan view taken along line 8-8 of Fig. 1;
Fig. 4 is an end of Fig. 1; I Fig. 5 is a modified form of split engine cylinder having its vertical split running in a plane through the axis of the crankshaft of the engine;
Pig. 6 is a modified form of engine cylinder head from that shown in Fig. 2 with regards to the spark plug installation;
Fig. 7 is a face plan view of one-half cylinder section of a two cycle engine looking into the interior of the head, block, and crankcase thereof;
Fig. 8 is a face plan view of one-half cylinder section of a four cycle engine looking into the inplan view taken along line 4-4 2 terlor of the head, block, and crankcase thereof;
Fig. 9 is a cross sectional view taken along line 9-9 of Fig. 7;
Fig. 10 is a top plan view of arcompletely assembled engine of the four cycle type shown'by Fig. 8; and
Fig. 11 is a fragmentary face plan view of onehalf cylinder incorporating a modified form of head and crankcase structure.
The instant invention is the result of the fervent desire in engine construction to provide an engine of lightweight and economical construction capable of high horsepower output per cu. in. of displacement. The engine construction herein presented provides basically of theformation of an engine cylinder of two main die cast or otherwise suitably produced sections or halves bolted or otherwise suitably secured together along a vertical plane and including therewithin the entire head, block, and crankcase of a complete engine. It is suggested also that a cylinder liner of good material can be employed in the assembly of the half cylinder sections thus permitting of higher compression ratios than those ordinarily permissible in small engines. The cylinder liner will also assist in the proper alignment of the sections of the engine in the clamping of them together about the liner. By the manufacture of engines of split cylinder construction as herein taught, it is possible in addition to the lightweight andeconomical construction thereof to provide engines of air or liquid cooled and two or four cycle design with equal simplicity and feasibility. Furthermore, it is preferably desired to construct single cylinder units that can be so arranged and bolted together to provide two, three, or more cylinder engines as requirements may be. Several other innovations resulting from this type of engine cylinder construction will present themselves in the detailed description to follow.
Referring to the drawings for more specific details of the invention wherein like numerals refer to like parts, it represents an engine of two cylinder construction comprising separate cylinders l2 and I4 bolted or otherwise suitably secured together, as indicated, by bolts IS. The cylinders I2 and I4 might each in themselves be separate engines but are here shown in joined relation to illustrate the feasibility of joining any number of cylinders l2 and I! together as may be desired. Cylinders l2 and i4 differ from one another merely in the provision of horizontal cooling fins I1 on cylinder 12 as compared to the vertical cooling fins It on cylinder I4. Cylinders I2 and I4 are each formed or constructed of two main sections or halves 28 and 22 joined in a vertical plane "A? and bolted or otherwise suitably secured together as by bolts 24. The cost of construction of an engine of this type may, if desired, be minimized by securing the sections 28 and 22 together with any suitable metallic bonding agent, such as Cycleweld. The sections 28 and 22 as shown in assembled relation by Figs. 1 and 2 provide an entire engine cylinder in itself in the provision of a complete head 26, block 28, and crankcase 88, wherein the head 26 has arranged in clamped relationship therein between the sections 28 and 22 a spark plug socket 3| for the threaded reception of a spark plug 82. The block 28 secures therein between the sections a cylinder liner 34 of sheet steel or other good material effective to assist in the alignment of the sections as well as permit of the use of higher compression ratios in the engine through the strengthening effect the liner 84 affords the cylinder;
By so forming cylinders I2 and I4 of half sections 28 and 22, it is possible to economically die cast the sections of strong and lightweight materials, thereby providing for the production, manufacture and assembly of engines of lightweight, high-strength characteristics, durabiliy, and of low cost. Furthermore by employing die casting or other similar methods in the making of cylinder sections 28 and 22, the amount of machining required for finishing the interior of the head 26, block 28, and crankcase 38 can be held to a minimum thereby further emphasizing the cost saving as compared to the conventional form of engine construction.
The crankcases 38 of cylinders I2 and I4 have arranged therein a crankshaft 36 of split or builtup construction permitting of ease in assembly upon and within the crankcases 28 of the respective cylinders I2 and consists of one portion 88 disposed in crankcase 28 of cylinder I2 and another portion 48 disposed in crankcase of cylinder I4, and has a flywheel 42 splined or fitted to the free end of portion 38 thereof. The portions 38 and 48 of crankshaft 36 are varied in construction merely for the purpose of illustrating that a connecting rod 44 of the type having a cap might be assembled on a full throw section 46 of portion 88 of the crankshaft; or a conecting rod 41, without a split cap design, could be assembled upon a split or joined throw section 48 of portion 48 of crankshaft 36. The two cylinder engine I8 as shown by Figs. 1 and 2 is adapted to have a crankcase plate 58 secured to the base of the engine so as to permit of the proper machining of the interior of cylinders I2 and I4 prior to their final assembly with the plate in place as shown by Fig. 2. As an alternative to having a plate 68 mounted upon the crankcase of the cylinder, reference is had to Fig. 11 wherein a half cylinder section 52 of similar apearance as sections 28 and 22 of cylinders I2 and I4 is provided having a bottom or base member 54 as an integral part of the crankcase; whereas a separate head plate 56 is provided adapted to be fitted between a pair of cylinder sections, as shown by Fig. 11, or otherwise suitably secured to the sections of the cylinder, said head plate construction likewise as plate construction 58 of cylinders I2 and I4 serving the purpose of permitting of whatever machining is necessary to the head 26, block 28, and crankcase 88 of the engine prior to the securing of the head plate 56 in place in the final assembly of the engine.
I4. Crankshaft 36 Although Figs. 1 and 2 illustrate the formation and assembly of the cylinder sections 28 and 22 along a vertical plane perpendicular to the axis of the crankshaft of engine II. it may be preferalble and more convenient from a production assembly standpoint to split the engine in a vertical plane that passes through and along the axis of the crankshaft as shown by Fig. 5 wherein two half sections 68 and 68 are secured together in a vertical plane passing through the axis of an engine crankshaft 62 similar to crankshaft 86 thereby providing the bearing mounting 64 of the crankshaft 82. It is conceivable that this manner of splitting thecylinder has far reaching production assembly benefits and advantages over the structure shown by Figs. 1 and 2 in that the sections 68 and 68 after the completion of the necessary machining operations thereon and just prior to final assembly wherein all inclusive engine parts are to be assembled can be laid in a manner along parallel conveyor lines whereby it shall only be necessary to place one section upon the other section containing all the working mechanism of the engine and then secure said sections together without changing the position of the engine.
Fig. 6 illustrates an alternative to the threading of the spark plug 82 in a socket 8| secured between cylinder sections 28 and 22, shown by Fig. 2, in the threading of a plug 63 directly into a threaded hole 65 of the head 66 of an engine I8. This is shown merely as a possibly more economical plug installation without the necessity of employing an additional plug socket 8|.
Figs. 8 and 10 represent a half cylinder section 68 of similar structural nature as sections 28 and 22 of engine I8 wherein section 68 comprises one half of a cylinder of atom cycle type engine I8. Cylinder section 68 is formed to provide a camshaft chamber l2 in addition to head 14, block I6, and crankcase I8 as an integral part thereof and has associated therewith the conventional operating mechanism of a four cycle engine, namely, a camshaft 88 disposed in chamber I2, a push rod 82 mounted in section 68 directly actuated by a cam 84 of camshaft 88, a rocker arm 86 journalled upon a post 88 forming a part of cylinder section 68 having one end engaged by push rod 82 and its other end engaging a spring pressed valve 88 for the movement thereof as a result of the motion transmitted to the rocker arm 86 by the push rod. The engine I8 as a complete unit resembles the engine I8 and comprises two half sections such as section 68 bolted or otherwise suitably secured together and containing in association therewith all of the operating parts of a four cycle engine as represented by the detailed description directed to cylinder section 68. In viewing Fig. 8, it is to be noted that no cylinder liner such as shown by Fig. 2 of engine I8 is included as an illustration that it may not be necessary in the construction of an engine of this sort to employ a cylinder liner should the cylinder material be capable of withstanding high or moderate operating compression pressures. The omission of the cylinder liner 34 from engine I8 can also be made depending upon the operating conditions required of said engine.
Although cylinders I2 and I4 and cylinder section 68 represent air-cooled type of construction, they could likewise be of the liquid cooled variety merely through the appropriate manufacture thereof with water cores in place of heat radiating or air cooling fins such as the fins I8 and I8 of engine I8.
l While this invention has been described in connection with certain specific embodiments, the principle involved is susceptible of numerous other applications that will readily occur to persons skilled in the art. The invention, therefore, is limited only as indicated by the scope of the appended claims.
What I claim is: 1. An engine comprising a pair of mating half sections joined along a common plane in opposed relation to one another forming the cylinder and crankcase of the engine, each having a semi-circular surface. throughout the cylinder section and annular internal grooves near one end opposite and axially disposed from the crankcase section mating with one another so as to form-a continuous annular groove, and a circular cylinder head received in the annular groove in clamped relation between the sections, said plane along which the sections are joined passing medially through the head, block, and crankcase oi the engine.
2. An engine comprising a pair of substantially alike semi-circular sections secured together in opposed relation to one another in a common plane passing through the center thereof and providing the cylinder and crankcase of the engine, each of said sections having internal semicircular openings throughout the cylinder por tion thereof with internal annular grooves cooperating therewith near one axial extremity thereof mating with one another to form a continuous annular groove, a cylinder liner retained in clamped relation in the cylinder formed by the sections, and a cylinder head received in the annular groove in clamped relation between the sections.
3. An internal combustion engine comprising a pair of similar semi-cylindrical sections secured together in a common plane lying P rpendicular to the axis of the engine crankshaft bearing supports formed in the sections, said sections providing therebetween th engine cylinder block and crankcase and each having a semi-circular internal annular groove near the one extremity of the cylinder block matching to form a continuous annular groove, a cylinder head received in the annular groove extending across the cylinder block opening and securely clamped between the sections, and a smooth surfaced relatively thin cylinder liner firmly embraced by the sections therebetween having one end in axial abutting relation to the cylinder head, said plane along which the sections are joined passing medially through the head, block, and crankcase of the engine.
4. An engine comprising a pair of substantially identical half sections joined along a common plane, each section having mating semi-circular openings therebetween constituting the engine cylinder, mating openings axially disposed from the semi-circular openings constituting the engine crankcase therebetween and mating internal annular grooves near the open end of the cylinder, a relatively thin cylinder liner clamped between the cylinder portions of the half sections having a radially extended annular collar on one end received in the groove formed between the sections, and a cylinder head clamped between the cylinder portions of the half sections having an annular collar received in axial wedged relaticn against the collar of the cylinder liner within the annular groove formed between the sections, said plane along which the sections are joined passing medially through the head, block, and crankcase of the engine.
5. An engine comprising a pair of substantially identical half sections joined along a common plane, each section havin mating semi-circular openings therebetween constituting the engine cylinder, mating openings axially disposed from the semi-circular openings constituting the engine crankcase therebetween and mating internal annular grooves near the opened end of the cylinder, a circular head clamped between the cylinder portions of the half sections having an annular collar received within the annular groove formed between the sections, a relatively thin cylinder liner clamped between the cylinder po'rtions of the half sections having one end in axially abutting relation upon the circular cylinder head, said plane along whichthe sections are joined passing medially through the head, block and crankcase of the engine.
CARL VOORHIES.
REFERENCES CITED I The following references are of record in the tile of this patent:
UNITED STATES PATENTS Number Name Date r 1,402,695 Wall Jan. 3, 1922 1,423,365 Smith July 18, 1922 1,540,172 Green June 2, 1925 2,337,661 Ireland Dec. 28, 1943 2,383,065 Lehman Aug. 21, 1945 2,397,434 Ricart Mar. 26, 1946 FOREIGN PATENTS Number Country Date 246,209 Germany Apr. 26, 1912
US688485A 1946-08-05 1946-08-05 Engine constructed of sections bolted together along vertical plane to form an entire head, block, and crankcase thereof Expired - Lifetime US2491630A (en)

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Cited By (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2650578A (en) * 1949-02-12 1953-09-01 Daub Rudolph Air cooling for internal-combustion engines
US2740393A (en) * 1952-10-27 1956-04-03 Roscoe C Hoffman Cylinder block and method of construction
DE1003989B (en) * 1953-12-24 1957-03-07 Reitter & Schefenacker Light metal cylinder for air-cooled small internal combustion engines
DE1023270B (en) * 1956-01-30 1958-01-23 Maybach Motorenbau Gmbh Welded cylinder crankcase
US2946322A (en) * 1958-04-11 1960-07-26 Engineering Res & Applic Ltd Internal combustion engines
US3279279A (en) * 1964-03-30 1966-10-18 Toyo Kogyo Company Ltd Crankshaft for multi-stage rotary piston engine
US3302537A (en) * 1964-05-29 1967-02-07 Borsig Ag Machine frame, especially for piston compressors and piston steam engines
US3521434A (en) * 1967-07-13 1970-07-21 Solo Kleinmotoren Gmbh Lawnmower
US3561416A (en) * 1969-04-25 1971-02-09 Kiekhaefer Elmer Carl Internal combustion engine cylinder block
US3768252A (en) * 1971-01-09 1973-10-30 Mtu Friedrichshafen Gmbh Cylinder crankcase assembly for dual crankshaft multi-cylinder engine
US3852963A (en) * 1973-09-27 1974-12-10 Gen Motors Corp Connecting and accessory drive means for separate internal combustion engines
US4084554A (en) * 1974-04-11 1978-04-18 Horst Bohnlein Multi-cylinder internal combustion engine
US4554893A (en) * 1984-10-01 1985-11-26 General Motors Corporation Lightweight engine
US4595345A (en) * 1979-01-15 1986-06-17 Varga John M J Gas compressor or blower
US4714060A (en) * 1986-02-04 1987-12-22 R K W Industries, Inc. Composite engine
US4802447A (en) * 1985-12-17 1989-02-07 Brunswick Corporation Foam pattern for engine cylinder block
US4957072A (en) * 1988-11-28 1990-09-18 Goldowsky Michael P Balanced radial engine
US5003935A (en) * 1988-11-28 1991-04-02 Goldowsky Michael P Balanced radial engine
US5271363A (en) * 1992-12-02 1993-12-21 Briggs & Stratton Corp. Reinforced cylinder for an internal combustion engine
US5429080A (en) * 1993-12-13 1995-07-04 Evestar Technologies, Inc. Compact internal combustion engine
US6076494A (en) * 1996-12-13 2000-06-20 Motorenfabrik Hatz Gmbh & Co. Kg Internal combustion engine and method for manufacturing same
US6196181B1 (en) * 1997-07-25 2001-03-06 Evestar Technologies, Incorporated Compact internal combustion engine
US20040025823A1 (en) * 2002-04-15 2004-02-12 Snyder Dale D. Internal combustion engine
US20040031458A1 (en) * 2002-04-15 2004-02-19 Snyder Dale D. Modular internal combustion engines
US6769384B2 (en) 2001-07-07 2004-08-03 Thomas J. Dougherty Radial internal combustion engine with floating balanced piston
WO2006053047A3 (en) * 2004-11-10 2006-11-09 Buck Supply Co Inc Individual cylinder assemblies and modular cylinder carrier
US7287493B2 (en) 2004-11-10 2007-10-30 Buck Supply Co., Inc. Internal combustion engine with hybrid cooling system
US7543558B2 (en) 2004-11-10 2009-06-09 Buck Diesel Engines, Inc. Multicylinder internal combustion engine with individual cylinder assemblies
US20120093665A1 (en) * 2009-05-28 2012-04-19 Flanigan Paul J Light Weight Crankcase Casting for Compressor
US8316814B2 (en) 2009-06-29 2012-11-27 Buck Kenneth M Toploading internal combustion engine
RU2479736C1 (en) * 2011-08-24 2013-04-20 Юрий Васильевич Костюкович Internal combustion engine
US20160348664A1 (en) * 2014-02-12 2016-12-01 Nuovo Pignone Srl Base unit for assembling a crankcase of a reciprocal compressor
US9562494B2 (en) 2013-01-31 2017-02-07 Brp-Powertrain Gmbh & Co. Kg Internal combustion engine having a split crankcase
US9709001B2 (en) 2012-09-28 2017-07-18 Global Ip Development Foundation Internal combustion engine with hinged access to lower block

Citations (7)

* Cited by examiner, † Cited by third party
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DE246209C (en) *
US1402695A (en) * 1918-12-27 1922-01-03 Wall Arthur William Casing of internal-combustion engines
US1423365A (en) * 1922-07-18 Organized under a
US1540172A (en) * 1923-12-14 1925-06-02 Frederick Ernest Rebbeck Internal-combustion single-acting engine cylinder
US2337661A (en) * 1941-12-08 1943-12-28 Jr Ward Stone Ireland Meter boxes
US2383065A (en) * 1942-07-30 1945-08-21 Bendix Aviat Corp Fluid filter
US2397434A (en) * 1942-10-17 1946-03-26 Ricart Wilfredo Crankcase and cylinder cooling

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE246209C (en) *
US1423365A (en) * 1922-07-18 Organized under a
US1402695A (en) * 1918-12-27 1922-01-03 Wall Arthur William Casing of internal-combustion engines
US1540172A (en) * 1923-12-14 1925-06-02 Frederick Ernest Rebbeck Internal-combustion single-acting engine cylinder
US2337661A (en) * 1941-12-08 1943-12-28 Jr Ward Stone Ireland Meter boxes
US2383065A (en) * 1942-07-30 1945-08-21 Bendix Aviat Corp Fluid filter
US2397434A (en) * 1942-10-17 1946-03-26 Ricart Wilfredo Crankcase and cylinder cooling

Cited By (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2650578A (en) * 1949-02-12 1953-09-01 Daub Rudolph Air cooling for internal-combustion engines
US2740393A (en) * 1952-10-27 1956-04-03 Roscoe C Hoffman Cylinder block and method of construction
DE1003989B (en) * 1953-12-24 1957-03-07 Reitter & Schefenacker Light metal cylinder for air-cooled small internal combustion engines
DE1023270B (en) * 1956-01-30 1958-01-23 Maybach Motorenbau Gmbh Welded cylinder crankcase
US2946322A (en) * 1958-04-11 1960-07-26 Engineering Res & Applic Ltd Internal combustion engines
US3279279A (en) * 1964-03-30 1966-10-18 Toyo Kogyo Company Ltd Crankshaft for multi-stage rotary piston engine
US3302537A (en) * 1964-05-29 1967-02-07 Borsig Ag Machine frame, especially for piston compressors and piston steam engines
US3521434A (en) * 1967-07-13 1970-07-21 Solo Kleinmotoren Gmbh Lawnmower
US3561416A (en) * 1969-04-25 1971-02-09 Kiekhaefer Elmer Carl Internal combustion engine cylinder block
US3768252A (en) * 1971-01-09 1973-10-30 Mtu Friedrichshafen Gmbh Cylinder crankcase assembly for dual crankshaft multi-cylinder engine
US3852963A (en) * 1973-09-27 1974-12-10 Gen Motors Corp Connecting and accessory drive means for separate internal combustion engines
US4084554A (en) * 1974-04-11 1978-04-18 Horst Bohnlein Multi-cylinder internal combustion engine
US4595345A (en) * 1979-01-15 1986-06-17 Varga John M J Gas compressor or blower
US4554893A (en) * 1984-10-01 1985-11-26 General Motors Corporation Lightweight engine
US4802447A (en) * 1985-12-17 1989-02-07 Brunswick Corporation Foam pattern for engine cylinder block
US4714060A (en) * 1986-02-04 1987-12-22 R K W Industries, Inc. Composite engine
US4957072A (en) * 1988-11-28 1990-09-18 Goldowsky Michael P Balanced radial engine
US5003935A (en) * 1988-11-28 1991-04-02 Goldowsky Michael P Balanced radial engine
US5271363A (en) * 1992-12-02 1993-12-21 Briggs & Stratton Corp. Reinforced cylinder for an internal combustion engine
US5429080A (en) * 1993-12-13 1995-07-04 Evestar Technologies, Inc. Compact internal combustion engine
US6076494A (en) * 1996-12-13 2000-06-20 Motorenfabrik Hatz Gmbh & Co. Kg Internal combustion engine and method for manufacturing same
US6196181B1 (en) * 1997-07-25 2001-03-06 Evestar Technologies, Incorporated Compact internal combustion engine
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