US1492215A - Engine - Google Patents

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US1492215A
US1492215A US252386A US25238618A US1492215A US 1492215 A US1492215 A US 1492215A US 252386 A US252386 A US 252386A US 25238618 A US25238618 A US 25238618A US 1492215 A US1492215 A US 1492215A
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Prior art keywords
shaft
rotatable
cylinders
ring
engine
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Expired - Lifetime
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US252386A
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Charles L Nedoma
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NEDOMA NAJDER CORP
NEDOMA-NAJDER Corp
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NEDOMA NAJDER CORP
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Priority to US252386A priority Critical patent/US1492215A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/26Engines with cylinder axes coaxial with, or parallel or inclined to, main-shaft axis; Engines with cylinder axes arranged substantially tangentially to a circle centred on main-shaft axis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/16Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18Multi-cylinder engines
    • F02B2075/1804Number of cylinders
    • F02B2075/184Number of cylinders ten
    • 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
    • Y10T74/00Machine element or mechanism
    • Y10T74/18Mechanical movements
    • Y10T74/18056Rotary to or from reciprocating or oscillating
    • Y10T74/18296Cam and slide
    • Y10T74/18336Wabbler type

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Transmission Devices (AREA)

Description

April 29, 1924.
C. L. NEDOMA ENGINE INVENTOR (Thar/e5 Z Neda/7m,
ATTORN EY? April 29, 19240 1,492,215
C. L. NEDOMA ENGINE" Filed Sept. 5, 1918 6 Sheets-Sheet 5 INVENTOR p BY iTTORNEY) April 29 L924. 3,492,215
C. L. NEDOMA v ENGINE Fild 1918 6 Shees-Set 4 I lNVENTOR 6/)0F/65 fi/edomq,
j ATTORNEY April 29, 1924.
C. L. NEDOMA ENGINE INVENTOR [bar/e5 Z. Neda/7m 6 Sheets-Sheet 5 Filed Sept. 5, 1918 C. L. NEDOMA ENGINE Filed Se t. 3 l9 8 6 Sh eets-Sheet 6 CHARL L. NEDO 013 DETROIT, MICHIGAN, ASSIGNOB, BY HESNE ASSIG .2 a?
PATENT Q1 21;
TO NEDOMA-NAJDEB COOEATION, A CORPORATION OF NEW YORK.
ENGINE.
Application filed September 3, 1918. Serial No. 252,388.
To all whom it may concern:
Be it know that I, CHARLES,L. Nnoonm, a citizen of the United States, and residing at Detroit, in the county of Wayne and State of Michigan, have invented a new and Improved Engine, of which the following is a specification.
The invention relates to rotary motors which have cylinders substantially parallel to the axis of the motor, and more particularly to motors of this type wherein the reciprocating movement of the pistons is caused to turn a rotatable driving part through the medium of a rotatable member whose axis is at an acute angle to that of the driving part.
The invent-ion provides means whereby the ratio between the reciprocating movement of the pistons and the angular movement of the motor is such that a full fourcycle movement of the pistons is obtained for each complete revolution of the motor, that is, each piston travels the full length of stroke in one quarter revolution of the motor. A ain, the invention ve atly increases t e effective leverage o tl d pistons: this is accomplished by rotatin the abutment or support for the incline rotatable member oppositely to the movement of the member itself.
A further object of the invention is to provide a quiet and eflicient valve construction; also to provide an unusually simple valve gear construction.
The invention also relates to an improved casing whereby the connecting rods and as sociated parts are rendered easily accessible.
The invention further consists in other details of construction shown, described and claimed.
In the drawings, Fig. 1 is a side view of a preferred embodiment of the motor, the casing through which air for cooling is directed being shown in section. Fig 1 is a diagrammatic side elevation SllOWlIlg the preferred position of the connecting rods relatively to the center lines of the cylin ders. ig. 2 is a longitudinal section of the engine, this section being about on line 2-2 of Fig. 6. Fig. 3 is a firing diagram. Figs. 4 and 5 are sections on the line 6--6 and i'7 of Fig. 2. Fig. 6 is an enlarged section showing the timing mechanism more clearly. Fi 7 is a section on the line 99 of Fig. 2. l the barrel. Fi 9 is 9. fr enta on tudinal section showing fiodifi l val v e g'ear. Fig. 10 is a section on line 12-12 of Fig. 9.
Power transmission featwrca.-The stationary shaft 10, preferably hollow, Fig. 2, is carried at one end in a suitable engine support 12 and rests at its opposite end in the rotatable engine hub 13 which is, in turn, carried in a support 14. As shown, a sleeve or bushing 15 is interposed between the shaft and the hub 13, and a double ball bearing 16 is disposed between the hub and the support 14, but other suitable bearings may be used. In the present construction,
' the hub is shouldered at 17 to form an abutment for the inner race of the bearin and a coupling member or the like 18, eyed to the rotatable hub at 19, serves the double function of holding the inner race properl 1' positioned when the threaded cap 20 is Justedand of transmittin torque from the hub to a suitable driven e ement, not shown. Annular elements or caps 21 and 22, threaded into the support 14, position the outer races and retain lubricant.
It will be observed that the hub 13 mar es into and forms a part of a barrel 25, ig. 10, and that the opposite end portion of the latter forms a ring or flange 26 that is bolted and shouldered on a flange 29 on the cylinder block 30. The latter is rotatably supported on the shaft 10 through the medium of the bushing 31, and is provided.
- with the threaded cap 32, follower ri 33,
packing 34., spacer 35, and pachng 36, whereby a tight joint is formed with the shaft. The barrel has a series of openings or hand holes 38, Fig. 10, through which the access may be had to the interior of the engine.
Near the junction of the main portion of the barrel with the hub 13, the metal is extended inwardly in the form of a gear hub on which the bevel gear 41 is fixed, as by means of the nut 42. This hub is also referably provided with the bushing 43,
ig. 4, which in efi'ect is a continuation of the bushing 15. Interiorly of the barrel t-h latter is provided with track 44 by which ig. 8 is a perspective view oftween the the thrust to the left (Fi 2) of the plate 45, which constitutes a cy indrical wedge, is taken .on the roller bearing 46. This wedge is rotatable on the shaft 10, being supported on the bushing 47; and carries a bevel gear 48 which is a duplicate ofthe gear 41. Bears 41 and 48, there is nonrotatable with the shaft 10 although free to slide longitudinally thereof, an annular pinion carrier or'spider 49, Figs. 2 and 9, on which a' plurality of pimons 50 are mounted as by means of the separate.stud shafts .51, the bushings 52 and the thrust bearings 53. These pinions mesh with the rs 41 and 48, consequently rotation of the cylinder block and barrel about the shaft causes the element .45 to turn in the opposite direction and at the same speed, thus doubli the relative angular movement between t e cylinder block and the wedge element.
The cylinder block carries a series of cylinders 1, 2, 3, 4, and 5, in the embodiment shown-see particularly Fig. 3(that may be either inte l with the block, as shown, or separate arranged with their axes parallel-to the axis of the shaft, and
. or the equlvalent. The ring rides on a roller bearing 63 that travels on a track surface 64 on the member 45, said surface being inclined to the axis of the shaft. In order to center the ring properly a ball bearing 65 is inter osed between it and the hub portion 66 of t e element 45, the inner race being conveniently held in place by the nut 68. By grooving the member 4 at 69 and by providi the ring with a flange 70, the constructlon is rendered com act. The ring is operatively connected tot e barrel or housing through the medium of the diametrically opposite pins 71 and blocks 72 pivoted thereon, Figs. 2 and 6, said blocks being arranged to reciprocate in the slots 73, Figs 2, 5 and 10, formed in the barrel 25, Preferably the walls of the slots are formed by separate hardened plates 74, Fig. 6. The thrust of theelement 45 to the right (Fig. 2) is taken by the thrust bearing 75 whlch seats against a gear 76 keyed or otherwise rigidly secured to the shaft.
It will be evident from the foregoing that the reciprocation of the pistons causes the ring 60 to turn about the axis of the beai'ings 63-65, and that the torque of the ring is applied to the rigid element 3025-13-18, to rotate the latter about the shaft and drive any suitable mechanism or part which may be attached to the coupling 18. The movement of the member 45 oppositely to the ring, asstated heretofore, results, in effect,
in a much sharper angle of reaction between the moving parts than could be. obtained were the member 45 stationary, and the travel of the piston is thus accomplished in a quarter turn of the engine instead of in a half turn as in earlier constructions.
It is evident that the necessary bearing adjustments between the bearings 46 and 7 5 for the wedge can be made by the tightening up on the nut 21. Likewise by inserting shims 77 between the track 44 and the annular rib or flange '7 8 against which it rests, or by removing one or more of said shims, as may be required, it is evident that the gears 41-48 may be brought into proper mesh with the pinions 50, 1t bei remembered that the spider 49 is slidab e on the shaft.
As is best indicated in Fig. 1, it is preferred to incline the connecting rods 59 forwardly (say three degrees) in respect todepends somewhat on the type selected;
However, it is preferred to utilize the hollow shaft for the admission of combustible mixture in which case the carburetor may be attached directly to a fitting 80 on the end of the shaft or to the mlxture pi e 81, Fig. 1, the mixture being distribut from the passage 82 through the ports 83, and 84in the shaft and in the spacer 35 and through the branch passages 85 to the several 0 linders. It is also preferred to provide s eeve valves 86 that are'interposed between the pistons andthecylinders and are received at the firing ends between the detachable heads 87 and the adjacent walls of the cylinders. Sealing-rings 88 set into grooves in the heads serve an obvious purpose.
These valves are provided with inlet ports 89 and exhaust orts 90 adapted to register respectively witii the inlet passages 85 and the exhaust passages 91, the latter preferably being connected by fittings 92 to a muffler 93. I
In the embodiment shown, the fixed gear 76 is of the helical type, and meshes with a series of helical gears 95, one for each cylinder, that are provided with thrust bearings 94, Fig. 6, and turn on shafts 96 carried in bosses 97 formed on the cylinder block 30; and the gears in turn mesh with ars 98 ,which are arranged radially about t e shaft and supported in bearings 99 carried by the block 30. The pitch of the teeth of the gears 7 695-98 is such that the gears 98 make one complete revolution for each revolution of the cylinder block. It will be observed that each of the gears 98 carries an eccentric pin 101 with respect to which' the corre neonate sponding gear freely turns (a bushing 102 being preferably interposed) and that the pins are pivotally connected to the corresponding sleeve valves 86 by pins 103 the axes of which are parallel to the shaft 10. Therefore, there is imparted to the valves 86 a compound sliding and oscillating motion, it being understood that the ports are so arranged as to bring a particular port 89 into registration with the corresponding passage for inlet purposes during one outward stroke of the piston (which is accomplished durin the time the cylinder block turns ninety degrees) and that the exhaust port 90 in like manner registers with the passage 91 while the piston is traveling in the opposite direction but not in the stroke immediately following. In other words, the engine shown operates on the four-cycle principle and each cylinder completes a full cycle for each revolution of the cylinder block.
1' gnitian.Cur1ent may be derived from any suitable source but in the embodiment shown the support 12 carries a ma etc the armature shaft 111 of which is riven by a pinion 112 which meshes with a gear 113 secured to the cylinder block 30 by the same bolts 114 that hold the cylinder heads in place. The spark plugs appear at 115 and each is connected to a corresponding contact 116, Fig. 8, by a conductor cable 117 and conductor 118. The contacts are carried in an insulator block 119 that is secured in the hub of the gear 113. A timer late 120 formed of insulating material and 1'. ed nonrotatably to the shaft 10 carries a suitable brush 121, connected to the magneto by a cable or conductor 123 and pressed against the face of the block 119 by a spring 125. The other branch of the circuit is formed by grounding the magneto to the support 12, as is obvious. A pad or rin 126 of soft material such as felt excludes dirt from the working parts.
By properly connecting the cables 117 to the spark plugs, the cylinders may be fired in the sequence shown in Fig. 3, that is, 1 d25-31, (the engine turning inthe direction of the arrow), which gives rise to a very desirable overlapping of impulses. Thus, in a five cylinder engine, assuming that the piston in cylinder 1 is at the beginning of its working stroke, cylinder 2 will have finished two fifths of its suction stroke, cylinder 3 will have completed four fifths of its working stroke, cylinder 4: will have com leted one fifth of its compression stroke and cylinder 5 will be through three fifths of its exhaust stroke. main pressures are, at the instant under consideration, transmitted to the ring from the cylinders 1 and 3 (working pressures) and from the cylinder a (compression), and cylinders 3 and i tend to balance the pressure That is, the
from 1 so far as stresses tending to tilt the ring 60 on the member l5 are concerned. The same general advantages occur at all times and regardless of the direction of rotation of the engine. This firing system may, of course, be modified and adapted to engines of this type wherein the number of cylinders is difi'erent from that shown.
It is evident that the same number of impulses are secured per revolution with a five cylinder four-cycle engine of this type as have been attained heretofore in a ten cylinder engine; in other words the present englue is, in this respect, the equivalent of prior engines of double its number of cylinders.
Modified power transmission, Fe 9.-ln some cases the driving torce may e transmitted from the ring 60 to the cylinder block 210, which corresponds to the block 30, by means of an inner barrel 211 which may be either separate from said block, as shown, and rigidly connected thereto in any suitable manner, or integral therewith. In the embodiment shown, the barrel has an end wall 212 which bears on the hub 213 of the member 45, thus securing a rigid support. By slotting the barrel at 214- and providing the pins 215 and shoes 216 corresponding to the pins 71 and shoes 72 heretofore described, it is evident that torque is transmitted to drive the cylinder block substantially as before.
Modified valve gears, Figs. 9 and 10.-A somewhat more direct drive for the valves may be secured by substituting for the ear 7% a similar gear 220 keyed to the she t at 221 the helical. teeth of which mesh with those of the gears 222 which are supported in bearings 223 and carry the pins 224. corresponding to. the pins 101. The connection between the pin and the associated sleeve valve 86 is as before, and the diameter and pitch of the gears is such as to cause one complete turn of the gears 222 for each revo lution of the engine. v
The engine thus constructed is especially adapted to aeroplane motors as 't permits the use of aluminum to a great on nt. The cylinders and pistons maybe made of light metal and the sleeve valves of cast iron or steel. The element 13-25 may also be made of aluminum. This, with the lent-er number of cylinders, pistons, connectin rods, etc., involved, results in a motor 0? very light weight as compared with existing types. The engine is equally well ada ted for general purposes, such as on vehicles or motor boats; and certain features thereof, for example, the power trans mitting elements and valve gear, may be applied to steam engines as well as to those 0 the internal combustion type or other mechanism such as pumps or compressors.
Various changes may be made in the details of construction oi the several features lid? lltl
involved without departing from the spirit of the invention. 1 do not, therefore, wish to be limited except as indicated by the subjoined claims.
I claim 1. An engine comprising a non-rotatable shaft, a rotatable structure embodying cylinders and pistons, a wabbling element hav-' ing an axis inclined to that of the shaft, said element being rotatable about the shaft, means whereby the reciprocation of the pistons tends to rotate the rotatable structure in one direction, and means for simultaneously rotating the wabbling element in the opposite direction.
2. A rotary internal combustion engine including a fixed shaft and a lurality of cylinders parallel thereto an rotatable about the shaft, pistons reciprocable therein, and means connecting the pistons and shaft whereby an intake stroke, a compression stroke, an explosion stroke and a scavenging stroke are set up in the cylinders in the order stated during each complete revolution of said cylinders, said means including an element rotatable about an axis at an acute angle to, and intersecting the ax s of the shaft and a support for said last named element rotatable about the shaft in the opposite direction.
3. A rotary engine including a fixed shaft and comprising a plurality of cylinders disposed around the shaft and parallel thereto and rotatable about the s aft, a wedge rotatable on; the shaft, a ring traveling on the wedge and rotatable about an axis at an acute angle to the axis of the shaft, pistons for the cylinders, means for applying force. from the pistons to the ring to cause the latter to turn about its axis, means forcausing the ring to rotate the cylinders, and means associated with the cylinders and the wedge for turning latter about the shaft in a direction opposite to the movement of the cylinders and at the same 5 sad.
4. A rotary engine inc udmg two elements, the first a shaft, the second element having a plurality of cylinders spaced about the shaft and substantially para lel thereto, means for transmitting force from one of said elements to the other to cause relative rotation, said means including istons for the cylinders, a ring on who pressure from the pistons is exerted, said ring bemg inclined to the axis of the shaft, a wedge concentric with the shaft and receiving the thrust of said ring, means connecting the ring to one of the elements to transmit torque, means for turning the wedge about the axis of the shaft and relatively to both of said elements, said second element having a track on which pressure from the ring is exerted, said track being farther from the axis of the shaft than is the means for turning the wedge.
5. A rotary engine includin a shaft and a structure rotatable about t e shaft and having a plurality of cylinders spaced about the shaft and substantially parallel thereto, pistons reciproeable in the cylinders, means connecting the pistons with the rotatable structure to cause the latter to turn as the pistons reciprocate, said means including a ring having its axis inclined to that of the shaft, a wedge concentric with the shaft and on which the ring is rotatable, means for rotating the wedge oppositely tothe direction of movement of the rotatable structure, said structure having a track, co-axial with the shaft, on which the wedge travels, the track being positioned farther from the axis of the shaft than are the inner edges of the bores of the cylinders.
6. An engine comprising a first member forming a shaft, a second member disposed about the shaft and having cylinders par-' allel thereto, pistons for the cylinders, means for causing the pistons to rotate one of the members, said means including a ring through which the shaft passes, said ring being inclined to the axis of the shaft,
means for transmitting torque from the ring to the rotatable member, a wedge con centric with the shaft and co-operating with the ring, means for rotating the wedge oppositely to the direction of movement of the rotatable member and at the same speed, a bearing, concentric with the shaft and positioned substantially at-the extreme outer dge'of the wedge on the side thereof nearest the wedge rotating means, whereon the thrust of the wedge is received.
7. An engine comprising a fixed shaft, 0. member rotatable about the shaft and having cylinders parallel thereto, pistons for the cylinders, a ring through which the shaft passes, said ring being inclined to the shaft and being connected to the rotatable member to turn the latter by a sli-ding connection, a rotatable wedge through which the shaft passes and on which the ring is mounted, and means for rotatin the wedge oppositely to the movement 0 the first named rotatable member, said means including a pair ofgears, one fixed to the first named rotatable member and the other to the wedge, and a pinion rotatable about a fixed pivot carried by the shaft and mesh-, ing with the gears.
8. An internal combustion engine comprising a shaft, a cylinder block rotatable thereon and having a plurality of cylinders disposed parallel thereto, an annular track having an axis at an angle to and intersect ing the axis of the shaft, a ring rotatable thereon and connected to the block to drive the latter, pistons for the cylinders, said;
pistons exerting pressure on the ring to rotate the letter about the axis of the track, means for imparting to the track an angular movement relative to the ring, and a hearing supporting the track along the outer edge thereof,-said bearing being located on the side of the track opposite to that at which the ring is located.
9. An engine comprising a first element forming a shaft and a second element forming a plurality of cylinders parallel thereto, pistons for the cylinders, one of the elements being rotatable in respect to the other, a rotatable wedge co-axial with the shaft and having an annular track the axis of which is inclined to that of the shaft, a ringlike member co-axial with the track and rotatable thereon, means connecting the ringlike member to the rotatable element to drive the latter, a bearing interposed between the ring-like member and the track, a second bearing interposed between the wedge and the ring-like element and being. positioned considerably nearer the shaft than the first mentioned bearing, and a third bearing 00- axial with the shaft and interposed between the wedge and the rotatable element, and means for rotating the wedge oppositely to the movement of the rotatable element.
10. An internal combustion engine comprising two elements, one a shaft and the other a plurality of parallel cylinders spaced around the shaft and parallel thereto, one of the elements being rotatable about the axis of the shaft, pistons for the cylinders, means connecting the pistons to the shaft for causing the pistonsto turn the rotatable element, a casing for the connecting means, said casing including a air of sheet metal members one of which is telescopic on the other longitudinally of the shaft.
11. In an internal combustion engine having a plurality of parallel cylinders disposed about a shaft and pistons for the cylinders, together with means for turning the cylinders about the shaft as the istons reciprocate, casing means for said ast named means, said casing means including a tubular sheet metal member having an end ortion with an inturned end and a second daring sheet metal member having an end portion with an outturned edge enclosed by the first named end portion, and packing between said edges.
12. An engine comprising a first element forming a shaftand a second element having a plurality of cylinders parallel thereto, one of the elements being rotatable about the axis of the shaft, pistons for the cylinders, a ring revoluble about an axis inclined to that of the shaft, connecting rods joining the pistons and ring, said rods being Inclined slightly forwardly in respectto the axes of the cylinders, whereby dead centers are avoided.
. 13. 'An internal combustion engine havin an odd number of cylinders rotatable aroun a fixed shaft, a wabbler ring rotatable on sure, said ring being inclined to the axis of the rotatable element, said rotatable element being slotted lengthwise of the shaft, and a block pivotally connected to the ring and slidable in the slot for transmitting torque from the ring to the rotatable element.
15. A rotary engine comprising a hollow shaft and a cylinder block having a cylinder parallel to said shaft, means for suppl ing) fuel mixture to the opening in the she. a ranch passa e in the block leading to the cylinder, 2. earing interposed between the block and the shaft, a tubular spacer surrounding the shaft and having a port connecting the space within the shaft to the branch passage, and means, separate from the spacer, for sealing the joint between the shaft and the block, on both sides of the spacer.
16. A rotary engine comprising a hollow shaft and a cylinder block having a cylinder parallel to said shaft, means for suppl ing fuel mixture to the opening in the sha a branch passage in the block leading to the cylinder, a bearing interposed between the block and the shaft, a tubular spacer surrounding the shaft and having a ort connecting the space within the sha to the branch passage, packing interposed between the spacer and the bearing, and a gland for sealing the joint between the shaft and the block on the opposite side of the spacer.
17. An engine comprising a fixed shaft, a member rotatableabout, the shaft and having cylinders parallel thereto, pistons for the cylinders, a ring through which the shaft passes, said ring being inclined to the shaft and being connected to the rotatable member to turnthe latter, a rotatable wedge through which the shaft passes and on which the ring is mounted, a bevel gear carried by the wedge, another bevel :gear carried by the rotatable member, bevel pinions radially disposed about the shaft and meshing with the gears, said inions being movable longitudinally of the shaft, and means for establishing proper relative adjustment between the gears, whereby they may be made to mesh properly with the pinions.
18. An enginecomprising a first member forming a shaft, a second member disposed about the shaft and having cylinders parallel thereto, pistons for the cylinders, means for causing the pistons to rotate one of the members, said means including a ring through which the shaft passes, said ring being inclined to the axis of the shaft, means for transmitting torque from the ring to the rotatable memher, a wedge concentric with the shaft, and co-operating with the ring, means for rotating the wedge oppositely to the direction of movement of the rotatable member and at the same speed, a thrust bearing between the wedge and shaft, and means for adjust ing the second member longitudinally of the shaft to secure proper adjustment of the bearin 19. rotary internal combustion engine com rising a non-rotatable shaft and an odd num er of cylinders parallel thereto and rotatable about the shaft, pistons reciprocable therein, means connecting the pistons and shaft whereby an explosion stroke and an exhaust stroke are set up in each 0 linder during each revolution of said cy inders, said means including an element rotatable about an axis at an acute angle to and intersecting the axis of the shaft, and means for successivel firing non-adjacent cylinders whereby orce tending to twist the ring across its axis is reduced.
20. In a rotary internal combustion engine, a shaft, a plurality of cylinders parallel to said shaft and revoluble therearound, a support for said shaft, a cylindercarrymg element on which said cylinders are mounted, a
sleeve extension rotatable with said cylinder carrying element passin through said support and anti-frictiona bearingsv between said extension and support.
' CHARLES L. NEDOMA.
US252386A 1918-09-03 1918-09-03 Engine Expired - Lifetime US1492215A (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2596410A (en) * 1947-12-26 1952-05-13 Le Grand L Jordan Internal-combustion engine
US4569314A (en) * 1980-11-01 1986-02-11 Institutul National De Motoare Termice Two-stroke axial pistons engines
US6250262B1 (en) * 1995-03-17 2001-06-26 Noel Stephen Duke Axial piston machines
US6662775B2 (en) 1999-03-23 2003-12-16 Thomas Engine Company, Llc Integral air compressor for boost air in barrel engine
US6698394B2 (en) 1999-03-23 2004-03-02 Thomas Engine Company Homogenous charge compression ignition and barrel engines
US8046299B2 (en) 2003-10-15 2011-10-25 American Express Travel Related Services Company, Inc. Systems, methods, and devices for selling transaction accounts

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2596410A (en) * 1947-12-26 1952-05-13 Le Grand L Jordan Internal-combustion engine
US4569314A (en) * 1980-11-01 1986-02-11 Institutul National De Motoare Termice Two-stroke axial pistons engines
US6250262B1 (en) * 1995-03-17 2001-06-26 Noel Stephen Duke Axial piston machines
US6662775B2 (en) 1999-03-23 2003-12-16 Thomas Engine Company, Llc Integral air compressor for boost air in barrel engine
US6698394B2 (en) 1999-03-23 2004-03-02 Thomas Engine Company Homogenous charge compression ignition and barrel engines
US8046299B2 (en) 2003-10-15 2011-10-25 American Express Travel Related Services Company, Inc. Systems, methods, and devices for selling transaction accounts

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