US1374164A - Internal-combustion engine - Google Patents
Internal-combustion engine Download PDFInfo
- Publication number
- US1374164A US1374164A US339279A US33927919A US1374164A US 1374164 A US1374164 A US 1374164A US 339279 A US339279 A US 339279A US 33927919 A US33927919 A US 33927919A US 1374164 A US1374164 A US 1374164A
- Authority
- US
- United States
- Prior art keywords
- shaft
- cylinders
- engine
- casing
- disks
- 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
Links
- 238000002485 combustion reaction Methods 0.000 title description 4
- 238000010276 construction Methods 0.000 description 4
- 241000235319 Havinthus Species 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 210000000887 face Anatomy 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 210000003128 head Anatomy 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05G—X-RAY TECHNIQUE
- H05G1/00—X-ray apparatus involving X-ray tubes; Circuits therefor
- H05G1/02—Constructional details
- H05G1/04—Mounting the X-ray tube within a closed housing
- H05G1/06—X-ray tube and at least part of the power supply apparatus being mounted within the same housing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
- F01B9/00—Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups
- F01B9/04—Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups with rotary main shaft other than crankshaft
- F01B9/06—Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups with rotary main shaft other than crankshaft the piston motion being transmitted by curved surfaces
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/16—Engines characterised by number of cylinders, e.g. single-cylinder engines
- F02B75/18—Multi-cylinder engines
- F02B75/22—Multi-cylinder engines with cylinders in V, fan, or star arrangement
- F02B75/222—Multi-cylinder engines with cylinders in V, fan, or star arrangement with cylinders in star arrangement
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
- F01B9/00—Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups
- F01B9/04—Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups with rotary main shaft other than crankshaft
- F01B9/06—Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups with rotary main shaft other than crankshaft the piston motion being transmitted by curved surfaces
- F01B2009/061—Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups with rotary main shaft other than crankshaft the piston motion being transmitted by curved surfaces by cams
- F01B2009/068—Quadri-lobe cams
-
- 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
- Y10T74/00—Machine element or mechanism
- Y10T74/21—Elements
- Y10T74/2101—Cams
Definitions
- This invention relates to improvements in internal combustion or gas engines, the principal object being to so design and arrange the parts of the engine, partlcularly one of the four cycle type, that each cylinder will have two power strokes for every revolution of the shaft, so that for the same bore of the cylinders and R. P. M. of the shaft, I obtain four times the horse power obtained with four cycle engines of the ordinary type withan equal number of cylinders, since in this type a power stroke is had only once for every two revolutions of the shaft.
- a further object is to devise an englne which will take up very little space longitudinally, in proportion to the power developed, and in which, by certain features of construction, I am enabled to combine the flywheel with the piston and cam. operating means, thus doing away with a separate flywheel, and so cutting down the weight and the total number of parts used.
- Another object is to produce a simple and relatively inexpensive engine, and yet one which will be exceedingly eflicient in its operation.
- Pig. 2 is a cross section taken on a line 2-2 of ig. 1.
- the numeral 1 denotes a cylindrical casing, preferably split on a vertical transverse center line for ease of manufacture and assembly, and connected together along this line by bolts 2.
- This casing is adapted to be mounted, by means of cars 3 projecting from the sides, on suitable supports 4,"such as the frame of automobile, engine bed of a boat, and the Projecting centrally through the casing, and turnable in bearings 5 therein, is a shaft 6 on which inside the casing, are keyed a pair of disks 7 arranged in opposed order and spaced apart a certain distance by reason of their abutting hubs 8 projecting therebetween.
- cylinders 9 Secured to the casing on the outside thereof and positioned radially from the shaft 6, are cylinders 9, whose center lines are on a vertical .plane bisecting the space between the two disks 7, and which are preferably positioned at an angle of 45 to each other.
- Pistons 10 are mounted in the cylinders, to which pistons are rigidly connected rods 11 extending radially in the direction of the shaft 6.
- the rods are also guided in sleeves 12 formed with or secured to the inner ends of the cylinders, the connecting members of the sleeves of course permitting a free circulation of air therepast, so as not to form a compression space between them and the pistons.
- Each groove is substantia lystar-shaped, and has four. oints A adjacent the outer edge of the disk, and eriually spaced apart, or 90.
- the pistons 10 are then in their to most position in the cylinders.
- the high or outer points "A are the inner or low points B of the groove, which are positioned centrally between the points A With the rollers 14 at these points, the pistons are then in their lowermost position in the cylinders, the radial distance between the points A and B being equal of course to the piston stroke.
- Each cylinder has of course intake and exhaust valves 16 and 17 respectively, and valve actuating rods 18. and 19 proyecting radially toward the casing 1, being operatively connected to tappets 20 and 21 slidably and radially mounted in the casing.
- the tappets have rollers 22 thereon riding on the circular surfaces of disks 23 and 24 respectively formed inte al with and outside the disks 7 but somew at smaller in diameter than the latter. These disks take the place of the flywheel usually supplied to give momentum and absorb vibration.
- Each of the disks 23 and 24 is provided with a pair of came 25 and 26 respectively adapted to engage the corresponding tappet roller, since as stated, each cylinder functions twice with every revolution of the shaft.
- Each disk must ofcourse be ofsufiicient width to accommodate four such pairs of cams, transversely, or one air for'the corresponding valve of each cy 'nder employed, an -the valve rods and tappets properly almed with their respective cams, since the time of o ening of the valves of each cylinder is di erent.
- An exhaust manifold 27 may connect all the exhaust ports.
- the ignition system of the engine I have not shown, since this may be run from the shaft and timed accordm to the firing strokes of each c linder in t e usual manner.
- a four cycle gas engine com rising a casin a shaft turnably mounted t erein, a plura ity of cylinders secured to the casing in radial alinement with the shaft, pistons in the cylinders, spaced disks fixed to the shaft, means for movin the pistons in and out with the rotation o the disks, circular extensions rojecting from the outer faces of the dis S, each c linder havin valve tappets rojecting ra ially toward 1; e shaft and sli ably mounted in the casing, and each tappet on a side being in ofi'set alinement from-the remainder, and-cams on the extensions positioned to lift each tappet at predetermined periods in the rotation of the disks.
- a gas engine comprisin a casing, a shaft turnably mounted therein, a plurality of cylinders secured to the casing in radial alinement' with the shaft and in a common plane at right angles thereto,pistons'in the cylinders, spaced disks fixed to the shaft, means for reciprocating the pistons with the rotation of the disks, valve tappets projecting from the valves of each cylinder, and a separate cam for each tappet formed with the disks and arranged to ift only the corresponding tappet at a predetermined time in the rotation of said disk.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Valve-Gear Or Valve Arrangements (AREA)
Description
H. A. NORDWICK.
INTERNAL comausmm ENGINE.
ARPLICATION HLED NOV. 20. I919.
Patented Apr. 5, 1921.
2 SHEEN-SHEET I.
INVENTOR. MnzyAJVordvc/c W TTORNEY BYQ 11/1/1111, 1 I 1 z I 4 I r 4 I 9 I I I I/ H. A. NORDWICK.
INTERNAL COMBUSTION ENGINE.
APPucAnoN FILED NOV-20,1919.
2 SHEETSSHEET 2.
IN VEN TOR.
HezuyA.Mrdwic/c BY Q) E g TTORNEY UNITED STATES PATENT OFFICE.
HENRY A. NORDWICK, OF STOCKTON, CALIFORNIA, ASSIGNOR OF ONE-HALF TO FRANK SEPPI, OF STOCKTON, CALIFORNIA.
IN TERNAL-GOMBUSTION Specification of Letters Patent.
ENGINE.
Application filed November 20, 1919. Serial No. 339,279.
To all whom it may concern Be it known that I, HENRY A. NoRnwIoK, a citizen of the United States, residing at Stockton, in the county of San Joaquin, State of California, have invented certain new and useful Improvements in Internal- Combustion Engines; and I do declare the following to be a full, clear, and exact description of the same, reference being had to the accompanying drawings, and to the characters of reference marked thereon, which form a part of this application.
This invention relates to improvements in internal combustion or gas engines, the principal object being to so design and arrange the parts of the engine, partlcularly one of the four cycle type, that each cylinder will have two power strokes for every revolution of the shaft, so that for the same bore of the cylinders and R. P. M. of the shaft, I obtain four times the horse power obtained with four cycle engines of the ordinary type withan equal number of cylinders, since in this type a power stroke is had only once for every two revolutions of the shaft.
This proportion of power obtains whether I construct a single or a multi-cylinder engine.
A further object is to devise an englne which will take up very little space longitudinally, in proportion to the power developed, and in which, by certain features of construction, I am enabled to combine the flywheel with the piston and cam. operating means, thus doing away with a separate flywheel, and so cutting down the weight and the total number of parts used.
I also do away with the expensive forged crankshaft commonly used.
Another object is to produce a simple and relatively inexpensive engine, and yet one which will be exceedingly eflicient in its operation.
The foregoing objects I accomplish by means of such structure and relative arrangement of parts as will fully appear from a perusal of the following specification and claims.
In the drawings, similar characters of reference indicate corresponding parts in the several views, in whic F lgure 1 is a front end elevation of my improved engine, half being in section.
Pig. 2 is a cross section taken on a line 2-2 of ig. 1.
I eferring now more particularly to the figures of reference on the drawings, the numeral 1 denotes a cylindrical casing, preferably split on a vertical transverse center line for ease of manufacture and assembly, and connected together along this line by bolts 2. This casing is adapted to be mounted, by means of cars 3 projecting from the sides, on suitable supports 4,"such as the frame of automobile, engine bed of a boat, and the Projecting centrally through the casing, and turnable in bearings 5 therein, is a shaft 6 on which inside the casing, are keyed a pair of disks 7 arranged in opposed order and spaced apart a certain distance by reason of their abutting hubs 8 projecting therebetween. Secured to the casing on the outside thereof and positioned radially from the shaft 6, are cylinders 9, whose center lines are on a vertical .plane bisecting the space between the two disks 7, and which are preferably positioned at an angle of 45 to each other.
In the present instance I show and describe four cylinders, all mounted above the.
horizontal center line of the casing, but it will be understood that I may emplo any number of cylinders from 1 to 8, without changing in any way the functioning of the engine, or the construction of the cooperating features.
Also, I have shown cylinders having overhead valves, though the L or T head construction would serve equally as well.
At the lower ends of the rods 11 are transverse pins 13 parallel to the shaft 6, and pro jecting equally on both sides of the rods. On such pro'ecting ends are rollers 14 adapted to ri e in inclosed cam eyes 15 formed in the adjacent faces of t e dlSkS 7.
In orderto fulfil the conditions stated as the principal object of the invention, that is, obtaining two power strokes for each cylinder for every revolution of the shaft, the cam rooves, bothof which are symmetrical, are esigned in the followin manner:
Each groove is substantia lystar-shaped, and has four. oints A adjacent the outer edge of the disk, and eriually spaced apart, or 90. When the rol ers 14 are at such oints in the grooves, the pistons 10 are then in their to most position in the cylinders. Interme late the high or outer points "A are the inner or low points B of the groove, which are positioned centrally between the points A With the rollers 14 at these points, the pistons are then in their lowermost position in the cylinders, the radial distance between the points A and B being equal of course to the piston stroke.
All eight points are therefore 45 apart about the shaft as an axis, which of course totals 360, or acomfilete circumference.
Therefore, since t e length of a piston stroke is had durin the travel of the piston rod rollers from a high point in the cam to the adjacent low point, or vice-versa, there will'be eight such tion of the shaft, or in other words, two complete c cles of four strokes each, on which basis all four-cycle engines operate.
Each cylinder has of course intake and exhaust valves 16 and 17 respectively, and valve actuating rods 18. and 19 proyecting radially toward the casing 1, being operatively connected to tappets 20 and 21 slidably and radially mounted in the casing. The tappets have rollers 22 thereon riding on the circular surfaces of disks 23 and 24 respectively formed inte al with and outside the disks 7 but somew at smaller in diameter than the latter. These disks take the place of the flywheel usually supplied to give momentum and absorb vibration.
Each of the disks 23 and 24 is provided with a pair of came 25 and 26 respectively adapted to engage the corresponding tappet roller, since as stated, each cylinder functions twice with every revolution of the shaft.
Each disk must ofcourse be ofsufiicient width to accommodate four such pairs of cams, transversely, or one air for'the corresponding valve of each cy 'nder employed, an -the valve rods and tappets properly almed with their respective cams, since the time of o ening of the valves of each cylinder is di erent.
I feel, however, that the construction strokes for every revolu-- shown We me a more counterbalanced engine t an by employing the alternate arrangement.
An exhaust manifold 27 may connect all the exhaust ports.
The ignition system of the engine I have not shown, since this may be run from the shaft and timed accordm to the firing strokes of each c linder in t e usual manner.
It will be evi ent that the same principle of 0 eration may be em loyed in an engine of to two cycle ty e, in which case each cylinder will fire our times with every revolution of the shaft, which is still four times the power obtainable with such an en ine built in the usual manner.
rom the foregoin description it will be readily seen that I ave roduced such a device as substantially ful is the objects of the invention as set forth herein.
While this specification sets forth in detail the present and preferred embodiment of the invention, still 1n practice such deviations from such detail may be resorted tb as do not form a departure from the spirit of the invention, as defined by the appended claims. 7
Havin thus described my invention, what I c aim .as new and useful and desire to secure by Letters Patent is 1. A four cycle gas engine com rising a casin a shaft turnably mounted t erein, a plura ity of cylinders secured to the casing in radial alinement with the shaft, pistons in the cylinders, spaced disks fixed to the shaft, means for movin the pistons in and out with the rotation o the disks, circular extensions rojecting from the outer faces of the dis S, each c linder havin valve tappets rojecting ra ially toward 1; e shaft and sli ably mounted in the casing, and each tappet on a side being in ofi'set alinement from-the remainder, and-cams on the extensions positioned to lift each tappet at predetermined periods in the rotation of the disks.
2. A gas engine comprisin a casing, a shaft turnably mounted therein, a plurality of cylinders secured to the casing in radial alinement' with the shaft and in a common plane at right angles thereto,pistons'in the cylinders, spaced disks fixed to the shaft, means for reciprocating the pistons with the rotation of the disks, valve tappets projecting from the valves of each cylinder, and a separate cam for each tappet formed with the disks and arranged to ift only the corresponding tappet at a predetermined time in the rotation of said disk. In testimony whereof I affix my signature in presence, of a witness. i
HENRY A. NORDWICK,
Witness:
BERNARD PBIVAT.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US339279A US1374164A (en) | 1919-11-20 | 1919-11-20 | Internal-combustion engine |
FR27084D FR27084E (en) | 1919-11-20 | 1922-11-21 | Advanced chi-ray machines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US339279A US1374164A (en) | 1919-11-20 | 1919-11-20 | Internal-combustion engine |
Publications (1)
Publication Number | Publication Date |
---|---|
US1374164A true US1374164A (en) | 1921-04-05 |
Family
ID=23328277
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US339279A Expired - Lifetime US1374164A (en) | 1919-11-20 | 1919-11-20 | Internal-combustion engine |
Country Status (2)
Country | Link |
---|---|
US (1) | US1374164A (en) |
FR (1) | FR27084E (en) |
Cited By (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1997024518A1 (en) * | 1995-12-26 | 1997-07-10 | Tritec Power Systems Ltd. | Tri-lobed cam engine |
WO2001065072A1 (en) * | 2000-02-29 | 2001-09-07 | Fantuzzi Reggiane Corporation S.A. | Internal-combustion engine with improved reciprocating action |
WO2003021082A1 (en) * | 2001-08-28 | 2003-03-13 | Fantuzzi Reggiane Corporation Holding S.A. | An improved reciprocating internal combustion engine |
US7219631B1 (en) * | 2003-02-24 | 2007-05-22 | O'neill James Leo | High torque, low velocity, internal combustion engine |
US20090313984A1 (en) * | 2008-06-24 | 2009-12-24 | Rez Mustafa | Hydraulic hybrid turbo transmission |
US20090313990A1 (en) * | 2008-06-24 | 2009-12-24 | Rez Mustafa | Pneumatic hybrid turbo transmission |
US20100064675A1 (en) * | 2008-06-24 | 2010-03-18 | Rez Mustafa | Hydraulic hybrid turbo-transmission |
US20100071640A1 (en) * | 2008-09-25 | 2010-03-25 | Rez Mustafa | Internal combustion engine with dual-chamber cylinder |
US20100116578A1 (en) * | 2008-11-12 | 2010-05-13 | Rez Mustafa | Hybrid turbo transmission |
US20100192878A1 (en) * | 2008-09-25 | 2010-08-05 | Rez Mustafa | Air hybrid engine with dual chamber cylinder |
CN102926868A (en) * | 2012-10-16 | 2013-02-13 | 黎湘平 | Power output mechanism of automotive engine |
US8622032B2 (en) | 2008-09-25 | 2014-01-07 | Mustafa Rez | Internal combustion engine with dual-chamber cylinder |
US9080498B2 (en) | 2012-04-11 | 2015-07-14 | Mustafa Rez | Combustion engine with a pair of one-way clutches used as a rotary shaft |
US20170342898A1 (en) * | 2016-04-08 | 2017-11-30 | James L. O'Neill | Asymmetric cam transmission |
US20180156108A1 (en) * | 2016-04-08 | 2018-06-07 | James L. O'Neill | Asymmetric cam transmission with coaxial counter-rotating output shafts |
CN109026380A (en) * | 2014-01-15 | 2018-12-18 | 纽勒诺有限公司 | Piston arrangement, internal combustion engine and its assemble method |
WO2020183126A1 (en) * | 2019-03-11 | 2020-09-17 | Newlenoir Limited | Piston arrangement |
US11261946B2 (en) * | 2016-04-08 | 2022-03-01 | James L. O'Neill | Asymmetric cam transmission with coaxial counter rotating shafts |
-
1919
- 1919-11-20 US US339279A patent/US1374164A/en not_active Expired - Lifetime
-
1922
- 1922-11-21 FR FR27084D patent/FR27084E/en not_active Expired
Cited By (34)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1997024518A1 (en) * | 1995-12-26 | 1997-07-10 | Tritec Power Systems Ltd. | Tri-lobed cam engine |
WO2001065072A1 (en) * | 2000-02-29 | 2001-09-07 | Fantuzzi Reggiane Corporation S.A. | Internal-combustion engine with improved reciprocating action |
WO2003021082A1 (en) * | 2001-08-28 | 2003-03-13 | Fantuzzi Reggiane Corporation Holding S.A. | An improved reciprocating internal combustion engine |
US20040261732A1 (en) * | 2001-08-28 | 2004-12-30 | Luciano Fantuzzi | Reciprocating internal combustion engine |
JP2005501993A (en) * | 2001-08-28 | 2005-01-20 | ファンツッジ レッギアネ コーポレーション ホールディング エス.エー. | Improved reciprocating internal combustion engine |
US6976467B2 (en) | 2001-08-28 | 2005-12-20 | Fantuzzi Reggiane Corporation Holding S.A. | Reciprocating internal combustion engine |
US7219631B1 (en) * | 2003-02-24 | 2007-05-22 | O'neill James Leo | High torque, low velocity, internal combustion engine |
US8336304B2 (en) | 2008-06-24 | 2012-12-25 | Rez Mustafa | Hydraulic hybrid turbo-transmission |
US20100064675A1 (en) * | 2008-06-24 | 2010-03-18 | Rez Mustafa | Hydraulic hybrid turbo-transmission |
US8235150B2 (en) | 2008-06-24 | 2012-08-07 | Rez Mustafa | Pneumatic hybrid turbo transmission |
US20090313984A1 (en) * | 2008-06-24 | 2009-12-24 | Rez Mustafa | Hydraulic hybrid turbo transmission |
US20090313990A1 (en) * | 2008-06-24 | 2009-12-24 | Rez Mustafa | Pneumatic hybrid turbo transmission |
US8622032B2 (en) | 2008-09-25 | 2014-01-07 | Mustafa Rez | Internal combustion engine with dual-chamber cylinder |
US20100071640A1 (en) * | 2008-09-25 | 2010-03-25 | Rez Mustafa | Internal combustion engine with dual-chamber cylinder |
US20100192878A1 (en) * | 2008-09-25 | 2010-08-05 | Rez Mustafa | Air hybrid engine with dual chamber cylinder |
US8191517B2 (en) | 2008-09-25 | 2012-06-05 | Rez Mustafa | Internal combustion engine with dual-chamber cylinder |
US8490584B2 (en) | 2008-09-25 | 2013-07-23 | Rez Mustafa | Air hybrid engine with dual chamber cylinder |
US20100116578A1 (en) * | 2008-11-12 | 2010-05-13 | Rez Mustafa | Hybrid turbo transmission |
US8087487B2 (en) | 2008-11-12 | 2012-01-03 | Rez Mustafa | Hybrid turbo transmission |
US9080498B2 (en) | 2012-04-11 | 2015-07-14 | Mustafa Rez | Combustion engine with a pair of one-way clutches used as a rotary shaft |
CN102926868B (en) * | 2012-10-16 | 2015-11-18 | 黎湘平 | A kind of power output mechanism of automotive engine |
CN102926868A (en) * | 2012-10-16 | 2013-02-13 | 黎湘平 | Power output mechanism of automotive engine |
US10858938B2 (en) | 2014-01-15 | 2020-12-08 | Newlenoir Limited | Piston arrangement |
US11008863B2 (en) | 2014-01-15 | 2021-05-18 | Newlenoir Limited | Piston arrangement |
CN109026380A (en) * | 2014-01-15 | 2018-12-18 | 纽勒诺有限公司 | Piston arrangement, internal combustion engine and its assemble method |
EP3473803A1 (en) * | 2014-01-15 | 2019-04-24 | Newlenoir Limited | Piston arrangement |
US10472964B2 (en) | 2014-01-15 | 2019-11-12 | Newlenoir Limited | Piston arrangement |
US20180156108A1 (en) * | 2016-04-08 | 2018-06-07 | James L. O'Neill | Asymmetric cam transmission with coaxial counter-rotating output shafts |
US10598090B2 (en) * | 2016-04-08 | 2020-03-24 | James L. O'Neill | Asymmetric cam transmission |
US10473027B2 (en) * | 2016-04-08 | 2019-11-12 | James L. O'Neill | Asymmetric cam transmission with coaxial counter-rotating output shafts |
US20170342898A1 (en) * | 2016-04-08 | 2017-11-30 | James L. O'Neill | Asymmetric cam transmission |
US11261946B2 (en) * | 2016-04-08 | 2022-03-01 | James L. O'Neill | Asymmetric cam transmission with coaxial counter rotating shafts |
WO2020183126A1 (en) * | 2019-03-11 | 2020-09-17 | Newlenoir Limited | Piston arrangement |
US11603881B2 (en) | 2019-03-11 | 2023-03-14 | Newlenoir Limited | Piston arrangement |
Also Published As
Publication number | Publication date |
---|---|
FR27084E (en) | 1924-04-29 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US1374164A (en) | Internal-combustion engine | |
US2067049A (en) | Internal combustion engine | |
US3572209A (en) | Radial engine | |
US1528164A (en) | Internal-combustion engine | |
US1830046A (en) | Internal combustion engine | |
US2274097A (en) | Crankless engine | |
US1502291A (en) | Valve for motors | |
US1183777A (en) | Internal-combustion engine. | |
US2169236A (en) | Internal combustion engine | |
USRE16630E (en) | nordwick | |
US1580249A (en) | Internal-combustion engine | |
US2194022A (en) | Internal combustion engine | |
US1764147A (en) | Internal-combustion engine | |
US1523341A (en) | Two-stroke engine | |
US1835138A (en) | Internal-combustion engine | |
US2335252A (en) | Internal combustion engine | |
US1802881A (en) | Internal-combustion engine | |
US2852837A (en) | Internal combustion engines and methods of manufacturing such engines | |
US1776760A (en) | Internal-combustion engine | |
US2130529A (en) | Internal combustion engine | |
US1639333A (en) | Explosive engine | |
US1722950A (en) | Internal-combustion engine | |
US1885576A (en) | Internal combustion engine | |
US1422633A (en) | Counterbalance for the crank shafts of internal-combustion engines | |
US1389967A (en) | murphy |