US20180112594A1 - Balanced rotary engine - Google Patents

Balanced rotary engine Download PDF

Info

Publication number
US20180112594A1
US20180112594A1 US15/331,395 US201615331395A US2018112594A1 US 20180112594 A1 US20180112594 A1 US 20180112594A1 US 201615331395 A US201615331395 A US 201615331395A US 2018112594 A1 US2018112594 A1 US 2018112594A1
Authority
US
United States
Prior art keywords
cylinder
rotary engine
drive
engine
piston
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.)
Abandoned
Application number
US15/331,395
Other languages
English (en)
Inventor
Michel Arseneau
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Quebec Engine Technologies LLC
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US15/331,395 priority Critical patent/US20180112594A1/en
Priority to CA2982945A priority patent/CA2982945C/en
Priority to AU2017346955A priority patent/AU2017346955A1/en
Priority to JP2019521730A priority patent/JP2019532218A/ja
Priority to EP17862693.3A priority patent/EP3510249B1/en
Priority to MX2019004504A priority patent/MX2019004504A/es
Priority to KR1020197011032A priority patent/KR102454944B1/ko
Priority to PCT/CA2017/000228 priority patent/WO2018072007A1/en
Priority to CN201780065214.9A priority patent/CN110139970A/zh
Priority to SG11201903375PA priority patent/SG11201903375PA/en
Priority to TW106136149A priority patent/TWI763726B/zh
Publication of US20180112594A1 publication Critical patent/US20180112594A1/en
Priority to US16/412,344 priority patent/US10954851B2/en
Assigned to QUEBEC ENGINE TECHNOLOGIES, LLC reassignment QUEBEC ENGINE TECHNOLOGIES, LLC ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: ARSENEAU, MICHEL
Abandoned legal-status Critical Current

Links

Images

Classifications

    • 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
    • F02B75/26—Engines 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
    • 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
    • F01B3/00—Reciprocating-piston machines or engines with cylinder axes coaxial with, or parallel or inclined to, main shaft axis
    • F01B3/0002—Reciprocating-piston machines or engines with cylinder axes coaxial with, or parallel or inclined to, main shaft axis having stationary cylinders
    • F01B3/0017—Component parts, details, e.g. sealings, lubrication
    • F01B3/0023—Actuating or actuated elements
    • 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
    • F01B9/02—Reciprocating-piston machines or engines characterised by connections between pistons and main shafts and not specific to preceding groups with crankshaft
    • 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
    • F02B75/06—Engines with means for equalising torque
    • F02B75/065—Engines with means for equalising torque with double connecting rods or crankshafts
    • 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
    • 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
    • F02B75/32—Engines characterised by connections between pistons and main shafts and not specific to preceding main groups
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/22—Compensation of inertia forces
    • F16F15/24—Compensation of inertia forces of crankshaft systems by particular disposition of cranks, pistons, or the like

Definitions

  • the present relates to internal combustion engines, and more particularly to a balanced rotary engine.
  • each of the cylinders includes a piston with a spark, or compression, that combusts a hydrocarbon fuel causing explosive power sufficient to reciprocally drive the piston in the cylinder.
  • the power generated by this driven piston can drive a shaft, which when used in traction moves an object, such as a motor vehicle, forwards or rearwards.
  • the power generated can be used statically to move parts in machinery, or can it can generate more power, for example through the use of a generator.
  • this simple mode of operation has been modified such as for example, in the so-called the Wankel engine, which uses one or more specially shaped rotors mounted on a drive shaft. Fuel is combusted to provide the motive power to turn the rotor(s) to drive the drive shaft.
  • a so-called rotary engine was introduced and used in a number of aircraft. The rotary engine included a piston casing, which drove a propeller, rather than a crankshaft. Since the first examples of the rotary engine, other rotary engines have been tested in motorcycles and in early road vehicles. However, the principal surviving type of rotary engine is still the Wankel engine, a version of which remains commercially available in some MazdaTM cars.
  • U.S. Pat. No. 6,357,397 to Kull describes an axial bevel gear generated control motion. This motion is used to control an accelerating-decelerating vane motion in a cylindrical central axis main pressure chamber using a limited angle differential gear whose reversing gear receives an axial crank controlled motion from an orbiting bevel gear or, in a modified version, from an oscillation controlling barrel cam.
  • the same bevel gear crank generated axial motion can also be used to provide an axial piston motion in cylinders with one or more pistons which can be in a stationary or rotating cylinder housing.
  • a valveless port communicates with a radial or axial flow distribution control, which is used for a pressurized fluid flow. This design is suited to external pressure or internal combustion engines in which the energy conversion comes from a fluid or combustion pressure to a powered output shaft rotation or in a reverse energy conversion mode.
  • a rotating cylinder valve engine which includes an engine casing having two casing sections, a double piston and rotating cylinder assembly.
  • the casing section has an internal chamber that extends from a open-end of circular cross-section towards a closed-end of the casing section.
  • a circular flange extends radially outward from the open-end of the casing section.
  • the flange has four lobe portions each formed with a bolt hole, and is formed with a circular radially inner recess.
  • the casing section is formed with a fuel inlet port, port for a spark plug and an exhaust port.
  • a balanced rotary engine for applying torque to a drive shaft, the rotary engine comprising:
  • a piston mounted for longitudinal movement within the cylinder
  • each connecting arm having a first connecting end and a second connecting end, the first connecting ends being connected to the piston;
  • crankshafts each crankshaft being rotably connected to the second connecting end of the connecting arms
  • first and second drive wheels contra-rotably connected to the respective first and second crankshafts
  • a fixed drive ring having a circumferentially disposed drive member surface, the fixed drive ring being mounted in the main drive case so that the drive member surface is disposed towards the piston, the first and second drive wheels meshing with the drive ring.
  • a drive assembly includes the connecting arms, the cranks shafts, the drive wheels and the fixed drive ring, the drive shaft being connected to the drive assembly and extending away therefrom.
  • the cylinder has a cylinder opening with a first longitudinal axis and a cylinder base, the cylinder base having first and second semi-circular indents located opposite each other, the cylinder base being sized and shaped for cooperation with the drive assembly.
  • the first and second drive wheels are mounted for contra-rotation about a second axis of rotation, the second axis of rotation being disposed orthogonal to the first axis of rotation.
  • the cylinder has a cylinder circumference, and the cylinder base having a cylinder base circumference, the cylinder base circumference being greater than the cylinder circumference.
  • first and second drive wheels are first and second gear pinions each having a plurality of circumferentially disposed teeth, each of the gear pinions are beveled towards each other.
  • the fixed drive ring has a plurality of circumferentially disposed inwardly beveled teeth, the beveled teeth of the gear pinions and the fixed drive ring being cooperable for meshing during contra-rotation of the gear pinions.
  • first and second cranks shafts each have a throw for connecting the crank shaft to the connecting arm, and a curvature located away from the throw.
  • a piston pin connects the first connecting ends of the connecting arms to the piston, the piston pin being disposed orthogonal to a cylinder opening first longitudinal axis.
  • the piston, the connecting arms and the crankshafts are triangulated when the piston is located in the cylinder at mid stroke so as to balance the engine.
  • an arm spacer is located between the first and second connecting arms, the spacer extending from between the connecting arms to between the first and second crankshafts.
  • a first crankshaft bearing is connected to both the first crankshaft and the first gear pinion, the first crankshaft bearing being located therebetween; and a second crankshaft bearing is connected between the second crankshaft and the second gear pinion and located therebetween.
  • First and second end bearings are connected to the respective first and second gear pinions.
  • a cylinder bearing is connected between the cylinder and the outer casing, the cylinder being sealingly connected to the outer casing.
  • the outer casing includes a base body and a mid section body, the base body having a base body opening, the drive shaft being sealingly connected to the base body opening.
  • Drive shaft bearings are located between the drive shaft and the base body.
  • the rotary engine further comprises: a cylinder head having located therein at least one inlet port, at least one outlet port, and an ignition source port, the cylinder head being connected to an upper portion of the cylinder for rotatable movement therewith; and a cylinder rotary disc sealingly connected to the cylinder head and the upper portion of the cylinder, the cylinder rotary disc being located therebetween.
  • the cylinder rotary disc includes a cylinder rotary disc opening, and a cylinder rotary disc ignition source port, the ports in the cylinder head being sequentially registered with the cylinder rotary disc opening as the cylinder rotates within the outer casing.
  • An underside of the cylinder head includes first and second seal rings circumferentially spaced apart and concentric with the ignition source port for sealingly mounting with the cylinder; and at least two seal rings are mounted in corresponding seal grooves located around the inlet port and the outlet port in the cylinder head, the seal rings being eccentrically located relative to the cylinder head.
  • a plurality of first resilient members are connected to the cylinder rotary disc and the cylinder head.
  • one or more thermal transfer members are located between the cylinder head and the cylinder rotary disc.
  • the seal grooves include a plurality of second resilient members.
  • the rotary engine further includes a cooling assembly located at an upper end of the cylinder, the cooling assembly includes a plurality of air-cooled fins, the fins being circumferentially disposed about the cylinder and projecting outwardly therefrom.
  • the outer casing includes a plurality of circumferentially disposed openings.
  • the openings are angled.
  • the openings are in fluid communication with the air inlet
  • the cooling assembly includes an air inlet passageway which extends through the cylinder head to the fins
  • the cooling assembly further includes a plurality of thermal transfer pads in communication between the cylinder head and the ring.
  • a plurality of cooling openings located on an upper portion of the cylinder head.
  • a drive assembly for use with a rotary engine, the assembly comprising:
  • a piston having a piston pin, the piston being located in a rotatable cylinder for recirpocal movement therein;
  • first and second connecting arms connected to the piston pin and moveable relative to each other;
  • gear assembly located away from the piston and in communication therewith, the gear assembly having first and second contra-rotatable crankshafts connected to two gear pinions;
  • a fixed gear ring having a plurality of teeth, the teeth being disposed such that they face the piston, the gear pinions meshingly engage with the fixed gear ring teeth when the crankshafts move in a contra-rotatable fashion.
  • a seal assembly for use with a cylinder head and a cylinder, the seal assembly comprising:
  • a cylinder head underside having an inlet opening, an outlet opening and an ignition source opening, each of the openings having circumferentially disposed an outlet opening groove, an inlet opening groove; an ignition source groove, the openings being disposed equidistant from each other;
  • the cylinder disc having a cylinder disc igntion opening and an aperture therein registerable with either of the inlet opening or the outlet opening in the cylinder head when the cylinder rotates about a longitudinal axis, the cylinder disc being sealingly mountable between the cylinder head and the cylinder.
  • a cooling system for use with a rotary engine comprising:
  • a cylinder disk having at least one thermal transfer pad mounted thereon for cooperation with the cylinder head, the thermal transfer pad being located to transfer thermal energy form the cylinder to the cylinder head.
  • a cooling system for use with a rotary engine comprising:
  • the fan being mounted for rotation such that cool air is drawn into the first and second inlet openings and is forced onto the fan, the fan being in communication with hot surfaces in the engine, such that cool air moving across the fan causing thermal transfer thereto, the warm air being moved away from the engine via the outlet openings.
  • FIG. 1 is perspective view of an embodiment of a balanced rotary engine
  • FIG. 2 is a side view of the engine as illustrated in FIG. 2 ;
  • FIG. 3 is a top view of the rotary engine of FIG. 1 showing an air inlet port, an exhaust outlet port and a plurality of circumfernetially disposed body bolts;
  • FIG. 4 is a longitudinal cross-sectional detailed view of the engine of FIG. 2 showing a piston at a top of a cylinder;
  • FIG. 5 is a longitudinal cross-sectional detailed view of the engine showing a rod spacer with the piston at the top of the cylinder;
  • FIG. 6 is a longitudinal cross-sectional detailed view of the engine with the piston at the bottom end of the cylinder;
  • FIG. 7 is another longitudinal cross-sectional detailed view of the engine with the piston at the bottom end of the cylinder;
  • FIG. 8 is a simplified longitudinal cross-sectional detailed view of the engine with the piston at the bottom end of the cylinder;
  • FIG. 9 is a perspective view the engine showing the location of the drive assembly
  • FIG. 10 is a simplified longitudinal cross-sectional view of the engine with the piston located at the mid-position in the cylinder showing the connecting arm;
  • FIG. 11 is a simplified longitudinal cross-sectional view of the engine with the piston at mid-stroke showing the crankshafts;
  • FIG. 12 is a simplified side view of a drive assembly showing a gear pinion meshed with a fixed gear ring;
  • FIG. 13 is a top perspective view of the drive assembly of FIG. 12 ;
  • FIG. 14 is another side view of the drive assembly showing two beveled gear pinions and a fixed gear ring;
  • FIG. 15 is a simplified side view of showing a crankshaft and two connecting arms
  • FIG. 16 is a simplified perspective view of FIG. 15 ;
  • FIG. 17 is a simplified top view of FIG. 15 ;
  • FIG. 18 is a side view of the gear assembly
  • FIG. 19 is a perseoctve view of the gear assembly
  • FIG. 20 is a top view of the gear assembly showing an axis of rotation
  • FIG. 21 is a longitudinal cross sectional detailed view of the gear assembly
  • FIG. 22 is a side view of the gear assembly showing the location of the drive shaft
  • FIG. 23 is a detailed bottom view of the gear assembly
  • FIG. 24 is a perspective exploded partial view of a single crankshaft and gear pinion
  • FIG. 25 is a top view of the exploded view of FIG. 24 ;
  • FIG. 26 is a top view of FIG. 25 ;
  • FIG. 27 is another top view of FIG. 25 ;
  • FIG. 28 is an exploded view showing the cylinder and the drive shaft around the drive assembly
  • FIG. 29 is another exploded view of FIG. 28 ;
  • FIG. 30 is a perspective exploded view showing the cylinder and the drive assembly
  • FIG. 31 is a bottom view of the drive assembly
  • FIG. 32 is an exploded side view of the cylinder, the drive assembly and the drive shaft;
  • FIG. 33 is an exploded, simplified view of FIG. 32 ;
  • FIG. 34 is an exploded perspective view of a cylinder head and cylinder
  • FIG. 35 is an a bottom view of the cylinder head
  • FIG. 36 is an exploded side view of the cylinder head and cylinder
  • FIG. 37 is an exploded perspective view of FIG. 36 ;
  • FIG. 38 is an exploded bottom perspective view of FIG. 36 ;
  • FIG. 39 is a longitudinal cross sectional view of the cylinder head
  • FIG. 42 is a exploded detailed side view of the cylinder head
  • FIG. 43 is a partially exploded bottom perspective view of the cylinder head
  • FIG. 44 is a longitudinal cross sectional view of the cylinder head and cylinder showing a thermal pad
  • FIG. 45 is a side view of the assembled cylinder head and the cylinder
  • FIG. 47 is a detailed side view of the cylinder head showing a collar with a plurality of angled air flow openings
  • FIG. 48 is a longitudinal cross sectional view of FIG. 47 ;
  • FIG. 49 is a perspective view of the assembled cylinder head
  • FIG. 50 is a longitudinal cross sectional view of the cylinder head showing an air flow pathway (arrows);
  • FIG. 51 is a simplified side view of the cylinder head and collar showing the location of the angled air flow openings
  • FIG. 52 is a top view of the cylinder head showing the location of the rotating cooling fins
  • FIG. 53 is a perspective view of a fully assembled rotary engine showing the location of deflector caps
  • FIG. 54 is a side view of FIG. 53 ;
  • FIG. 55 is a top view of FIG. 53 ;
  • FIG. 56 is a simplified longitudinal cross sectional view of the cylinder showing the location of the cylinder cap
  • FIG. 57 is a perspective view of FIG. 56 ;
  • FIG. 58 is top view of FIG. 57 ;
  • FIG. 59 is longitudinal cross sectional view of the rotary engine showing location of seals and an oil lubrication system
  • FIG. 60 is a partial cut away side view of the engine showing an oil inlet
  • FIG. 61 is aside view of the drive assembly showing two spacer rod supports
  • FIG. 62 is a simplified perspective view of the drive assembly showing the spacer bar
  • FIG. 63 is a simplified top view of the spacer bar showing two curved ends abutting the two spacers;
  • FIG. 64 is a bottom view of the drive assembly showing the location of the two supports
  • FIG. 65 is a detailed top view of the drive assembly showing the spacer rod, the two curved ends and the direction of rotation;
  • FIG. 66 is another top view of the drive assembly showing the location of the curved ends after 180 degree rotation.
  • the rotary engine 10 includes a domed cylinder head 12 , an outer casing 14 , and a drive shaft 16 extending away from the outer casing 14 .
  • the outer casing 14 includes a mid body section 18 , a base body section 20 and a base body opening 22 .
  • a cylinder 24 located in the outer casing 14 is a cylinder 24 , which is sealingly mounted therein for rotation about a longitudinal axis 26 ; a piston 28 ; two connecting arms (rods) 30 , 32 ; and a drive assembly 34 .
  • the drive shaft 16 is in communication with the drive assembly 34 and extends away from the base body section 20 of the outer casing 14 .
  • the cylinder head 12 is referred to as being an upper or top part of the engine 10
  • the base body section 20 is referred to as being located at a lower or bottom part of the engine 10 .
  • the rotary engine 10 is essentially a modular construction, which allows easy replacement of parts and interchangeability. Additionally, the modular construction affords versatility in power train design and function.
  • a main drive case (cradle) 36 is located in the base body section 20 of the outer casing 14 .
  • the cylinder 24 has a chamber 38 in which is the piston 28 is mounted.
  • a combustion chamber 40 is located between the cylinder head 12 and the piston 28 .
  • the piston 28 is mounted within the chamber 38 for longitudinal movement along the longitudinal axis 26 that bisects the rotary engine 10 .
  • a cylinder bearing 44 is located between an outer surface 46 of the cylinder 24 and an inner surface 48 of the mid body section 18 of the outer casing 14 .
  • a cylinder seal 50 is located adjacent the cylinder bearing 44 to prevent leakage of, for example, lubricant.
  • the cylinder bearing 44 and the cylinder seal 50 are located adjacent a junction 52 between the mid body section 18 and the base body section 20 and in a cavity 49 located in the mid body section 20 .
  • the cylinder bearing 44 in this case, is a ball race, although one skilled in the art will recognize that other types of bearings are available.
  • the mid body section 18 is narrower at the junction 52 compared to an upper part 54 of the base body section 20 .
  • the base body section 20 tapers down to the base body opening 22 and ultimately towards the drive shaft 16 .
  • the outer casing 14 is, in essence, a sidewall that envelops the moving parts of the rotary engine 10 . As seen in FIG. 1 , this gives the impression of a compact, symmetrical and aesthetically pleasing rotary engine 10 .
  • each of the connecting arms 30 , 32 extend from the piston 28 towards the drive assembly 34 .
  • Each of the connecting arms 30 , 32 are rods that each have a first arm connecting end 56 and a second arm connecting end 58 .
  • the first connecting ends 30 of each connecting arm 30 , 32 is connected to the piston 28 .
  • a single piston pin 58 is located in the piston and disposed orthogonal to the longitudinal axis 26 .
  • the drive assembly 34 is located away from the piston 28 and disposed within the main drive case 36 .
  • the drive assembly 34 includes first and second crankshafts 60 , 62 , each of the crankshafts being rotably connected to the second arm connecting end 58 of the connecting arms 30 , 32 .
  • crankshafts 60 , 62 has a throw 67 , 69 (or crankshaft pin) connected to the gear pinions 68 , 70 , located at the end of a crankshaft connecting member 75 , 77 .
  • first and second crankshaft bearings 64 , 66 are connected to the respective first and second crankshafts 60 , 62 .
  • First and second beveled gear pinions (gear drive wheels) 68 , 70 are secured to the first and second crankshaft bearings 64 , 66 and to the second arm connecting end 58 of the connecting arms 30 , 32 using crank gear bolts 72 , 74 .
  • the beveled gear pinions 68 , 70 are tapered towards the each other and towards the connecting arms 30 , 32 .
  • the first and second gear pinions 68 , 70 are mounted for contra-rotation about a second axis of rotation 76 that is disposed orthogonal to the first longitudinal axis 26 .
  • the first and second gear pinions 68 , 70 each has a first drive member which is, on each gear pinion a plurality of circumferentially disposed gear pinion teeth 69 , 71 , as best seen in FIG. 13 .
  • the first and second gear pinions 68 , 70 are contra-rotably connected to the respective first and second crankshafts 60 , 62 .
  • the drive assembly 34 is held together using first and second end bearings 78 , 80 that are bolted together using bolts 79 , 81 to ensure a compact arrangement.
  • a rod spacer 82 is located between the first and second connecting arms 30 , 32 and extends from between the arms to between the first and second crankshafts 60 , 62 .
  • the rod spacer 82 help maintain the two connecting arms 30 , 32 and the crankshaft bearings 64 , 66 on the crank gear bolts 72 , 74 and stops them from loosening and becoming free.
  • the drive shaft 16 is connected to the drive assembly 34 and is co-axial with the first longitudinal axis 26 .
  • the drive shaft 16 includes a drive shaft projection 84 and a circumferentially disposed flange 86 having a plurality of holes 88 therein.
  • the drive assembly 34 includes a drive assembly connecting member 90 having a centrally disposed opening 92 located therein to receive the drive shaft projection 84 and a plurality of circumferentially disposed holes 94 , as best seen in FIG. 23 .
  • the drive shaft 16 is mechanically secured to the drive assembly 34 using bolts driven through the holes 88 and the holes 94 .
  • drive shaft bearings 96 surround the drive shaft 16 and abut the underside of the circumferentially disposed flange 86 .
  • the drive shaft bearings 96 are located adjacent the base body opening 22 and are sandwiched between the drive shaft 16 and the base body section 20 , as best seen in FIGS. 5 and 10 .
  • the drive shaft bearings 96 are ball races.
  • the drive assembly 34 further includes a fixed gear drive ring 100 , which has a circumferentially disposed drive member surface with a plurality of circumferentially disposed teeth 102 .
  • the fixed gear ring 100 is fixably mounted in the main drive case 36 so that the teeth 102 are disposed towards the piston 28 .
  • the circumferentially disposed teeth 102 are inwardly beveled to permit cooperable meshing thereof with the corresponding gear pinion teeth 69 , 71 during contra-rotation of the gear pinions 68 , 70 .
  • This new orientation of the fixed gear ring 100 towards the piston 28 allows considerable reduction in engine size because all the available inner space of the lower casing is used to house the drive assembly 34 .
  • the perfect balance of the engine 10 with the piston 28 at mid-stroke is achieved because the two contra-rotatable crankshafts 60 , 62 are orientated such that the curvature 63 , 65 of each crankshaft 60 , 62 are located 90 degrees to the first longitudinal axis 26 .
  • the two connecting arms 30 , 32 and the two crankshafts 60 , 62 are triangulated with the pin 58 being located at the apex of the triangle.
  • the curvatures 63 , 65 of the crankshafts 60 , 62 are co-planar.
  • the cylinder 24 has an upper cylinder portion 104 having a cylinder circumference, and a cylinder base 105 that has a cylinder base circumference.
  • the cylinder base 105 circumference is greater than the upper cylinder portion 104 circumference.
  • the cylinder base 105 includes two semi-circular indents 106 , 108 which are located on opposite sides of the cylinder base 105 .
  • the semi-circular indents 106 , 108 are sized and shaped to cooperate with the drive assembly 34 , which helps to align the cylinder 24 with the drive assembly 34 simply and precisely during assembly. Furthermore, this precise assembly creates a rigid assembly with receded vibration compared to convention assemblies.
  • the cylinder base 105 includes four bolting holes 109 to help secure the cylinder 24 to the drive shaft 16 .
  • the cylinder base 105 with the semi-circular indents 106 , 108 allows for accurate, quick and easy assembly of the cylinder 24 with the drive assembly 34 .
  • the connecting arms 30 , 32 act individually and translate contra-rotation to the respective first and second crankshafts 60 , 62 .
  • the rotary engine 10 with the piston 28 at a mid stroke position, as seen in FIGS. 11, 15, 15 and 16 with the connecting arms 30 , 32 allow significant reduction of the side loading from the piston 28 and the wall of cylinder 24 because of the perfect symmetrical balance achieved.
  • the piston 28 moves reciprocally within the cylinder 24 .
  • the piston 28 is carried through the agency of the piston pin 52 by the two connecting arms 30 , 32 which extend from their respective throws or crank pins carried on the two separate and contra-rotating crankshafts.
  • Each of the crankshafts carries the bevel gear pinion respectively, which meshes with the fixed bevel gear ring fixed.
  • a cylinder head assembly 109 is mounted on the upper cylinder portion 104 of the cylinder 24 so that the assembly 109 is connected to the cylinder 24 and the outer casing 14 .
  • the cylinder head assembly 109 includes the cylinder head 12 and a cylinder rotary disc 110 .
  • the cylinder rotary disc 110 is sealingly connected to the upper cylinder portion 104 and to an underside 112 of the cylinder head 12 .
  • the cylinder rotary disc 110 is therefore sandwiched between the cylinder head 12 and the cylinder 24 .
  • the diameter (and of course the circumference) of the cylinder head 12 when sealingly mounted on the cylinder 24 is larger than the diameter of the cylinder 24 .
  • the cylinder head 12 has a fluid (air) inlet port 114 , a fluid outlet (exhaust) port 116 , and an ignition source port 118 .
  • the ignition source port 118 houses an ignition source such as a spark plug (not shown).
  • the fluid inlet port 114 is located adjacent the exhaust port 116 .
  • the cylinder rotary disc 110 includes a cylinder rotary disc opening 120 , and a cylinder rotary disc ignition source port 122 .
  • the fluid ports 114 , 116 in the cylinder head 12 are each sequentially registered with the cylinder rotary disc opening 120 as the cylinder 24 rotates within the outer casing 14 .
  • a sealing assembly is shown generally at 123 .
  • Three seal rings 124 , 126 , 128 are mounted in corresponding deep seal grooves 130 , 132 , 134 located adjacent the inlet port 114 and the exhaust port 116 in the cylinder head 12 .
  • An ignition port seal ring 136 is located in a seal groove 138 located around the ignition source port 122 .
  • the seal rings 124 , 126 , 128 are equidistant from each other and are located around the ignition port seal ring 136 .
  • the underside 112 of the cylinder head 12 also includes first and second concentric grooves 138 , 140 , the second groove 140 being smaller than the first groove 138 .
  • Located between the two concentric grooves 138 , 140 is a plurality of spaced apart air flow openings 142 , the air flow openings 142 being concentric with the second groove 140 .
  • the cylinder rotary disc 110 has a circumferentially disposed seal 144 that fits snuggly in the deep second groove 140 and allows a sealing engagement with the upper cylinder portion 104 .
  • the seal 144 also includes a backup ring seal 146 with cut at least one location 147 and is located outside the second groove 140 .
  • Resilient wave springs 148 are mounted on top of the cylinder rotary disc 110 .
  • Each of the seal rings 124 , 126 , 128 , 136 do not have a cut, but instead include a back up ring 149 located on the inside of the seal grooves 130 , 132 , 134 .
  • the outer surface of the ring seals 124 , 126 , 128 , 136 are chamfered at the upper and lower ends (not shown).
  • the ring seal designs are part of a high pressure rotary valve in which the resilient wave springs 148 provide a light downward force; the backup ring seal 149 with the cut at least one location 147 seals on the diameter of the seal groove; the seal rings 124 , 126 , 128 push downwardly on the outside of the respective grooves; the medium sized ring push downwardly on the inside of the groove; and the main rings 124 , 126 , 128 are chamfered so that they fit the backup ring better without needing a cut.
  • the ring seals seal in different directions to provide a perfect seal.
  • the three ring set is fixed with the head rotary top cylinder.
  • a dual unique fan and thermal energy exchange system is located opposite the drive assembly 34 to provide very efficient self cooling using air flow and thermal contact to exchange heat to the air as cool, fresh air moves across the thermal exchange surfaces.
  • the ability to efficiently remove heat from the engine prevents engine overheating, which can ultimately cause engine failure.
  • a dual cooling system is illustrated generally at 200 .
  • the first part of the dual cooling system 200 relies on thermal energy transfer from a hot surface to cool air as the cool air is forced across the hot surface.
  • the second part of the dual cooling system 200 relies on thermal transfer from a hot surface via a heat exchanger.
  • three heat transfer pads 202 spaced apart and equidistant from each other and connected to the cylinder rotary disc 110 .
  • the heat transfer pads 202 are upstanding from the cylinder rotary disc 110 .
  • the three heat transfer pads 202 act as independent heat exchangers to remove heat from the engine.
  • the heat transfer pads 202 radiate away from the cylinder rotary disc ignition source port 122 and are angled away from each other at about 120 degrees. As best seen in FIG. 44 , each of the heat transfer pads 202 includes two light resilient spaced apart (spring) members 204 , 206 extending upwardly therefrom. Each of the heat transfer pads 202 and the spaced apart spring members 204 , 206 insert snuggly into a cylinder head cavity 208 . The thermal energy produced during combustion of the fuel and operation of the rotary engine 10 generates considerable thermal energy in the form of heat.
  • the heat transfer pad 202 are located adjacent to or in direct contact with the thermal surfaces of the cylinder 24 means that they are able to absorb the thermal energy and transfer it to the cylinder head 12 for dissipation directly from the outer surfaces of the cylinder head 12 or by cool air flowing over the outer surfaces.
  • the thermal transfer pads 202 are made from material which have a high heat conductivity are which are well known to hose skilled in the art.
  • a collar 214 is connected between the cylinder head 12 and the upper part 54 of the base body section 20 .
  • the collar 214 includes a plurality of spaced apart, angled elongate openings 216 arranged as part of a dual cooling system, which will be described in more detail below.
  • Below the collar 214 are a plurality of horizontally disposed indents 217 which help to reduce the overall weight of the engine.
  • Below the indents 217 of which there are six, are a plurality of air inlet opening 221 .
  • the cylinder head 12 includes the plurality of spaced apart air flow openings 142 which are located equidistant between the seals 138 , 140 in the cylinder head 12 part of an air flow cooling system.
  • Located on the top part of the cylinder head 12 are a plurality of radially disposed elongate cooling air intake openings 210 adjacent a plurality of air inlet openings 212 that are disposed about the ignition source port 118 and radiate outwardly therefrom.
  • Each of the openings 210 are small elongate openings arranged in groups of three around the cylinder head 12 .
  • the collar 214 is connected between the cylinder head 12 and the upper portion of the outer casing.
  • the collar 214 includes the plurality of spaced apart, angled elongate openings 216 .
  • the openings 216 provide an outlet for air flow as it passes along a coolant flow pathway 218 (as indicated by the arrows in FIG. 50 ).
  • a fan 219 is mounted to rotate around the cylinder 24 to draw fresh air in through the inlets 210 , 212 and 225 .
  • the deflector located adjacent the inlet 225 pushes air onto the small diameter of the fan 219 , and then the warmed air exits through the opening 216 .
  • the fan 219 is made from lightweight aluminum and is screwed into the top of the cylinder disc and the top of the cylinder disc to the cylinder.
  • First and second deflector caps 220 , 222 are connected to the top of the cylinder head 12 and are located adjacent the intake fins 210 .
  • air is drawn in from around the cylinder head 12 and enters the plurality of air inlet openings 210 and the openings 212 is forced into the coolant flow pathway 218 .
  • the rotating fins push the air out through the angled elongate openings 216 .
  • thermal energy transfer takes place from the hot surfaces in the cylinder head 12 or adjacent to it to the cool air which absorbs the heat.
  • the forcing of air from the center of the cylinder head 12 then through the cylinder head provides superior cooling efficiency compared to conventional cooling methods.
  • a locking disk 224 is mounted on top of the cylinder and surrounds the cylinder rotary disc 110 using a plurality of locking bolts 226 (locking disk with the fin rings).
  • the plurality of holes 14 communicate from the cylinder head 12 to the fins 219 providing cooling to the cylinder head 12 .
  • the fins on the rotary cooling fan are angled towards the spark plug hole.
  • a plurality of circumferentially disposed bolt holes 113 are located top help secured the cylinder head to the outer casing.
  • cool fresh air is drawn into the cylinder head 12 at the openings 210 , 212 , and 225 .
  • the deflectors brings cooling flow to the small diameter of the rotary fins 219 .
  • the intake is through the cylinder head 12 to the small diameter of the fins 219 .
  • Exit air flows to cool off the body of the engine.
  • the fixed fins on the cylinder head also aid cooling.
  • a lubrication system is needed to allow the parts movement across each other's surfaces to prevent ceasing.
  • the lubricant used is a typical oil (synthetic or natural) known to those skilled in the art for the purpose of lubrication.
  • a lubrication system is shown generally at 300 .
  • An oil inlet port 302 is shown adjacent the gear assembly and is connected to an oil pump (not shown).
  • the spacer rod 82 between the two connecting arms 30 , 32 has two curves 306 , 308 at either end towards the outer casing so that the oil entering the gear assembly is induced to the middle of the engine as the engine rotates in the direction of an arrow 304 .
  • This simple curvature of the spacer rod 82 allows for a more even distribution of the oil to all the moving parts during operation of the engine. Absent the rod spacer curvatures 306 , 308 , the oil's final destination would depend largely on the pump force.
  • An oil outlet port ensures continuous recycling of the oil.
  • the seals 50 , 98 between the cylinder 24 and the outer casing 14 and between the lower base portion and the drive shaft 16 prevent the oil from leaking out from the engine.
  • the curved ends 306 , 308 of the spacer rod 82 abut two supports 310 , 312 which project outwardly from the engine 10 .
  • the cylinder 24 and the gear assembly 34 is a closed system, which maintains oil so that it remain in contact with the rotary parts.
  • the oil inlet port 302 moves the oil to the base body which is induced by the rod spacer 82 .
  • the balanced rotary engine 10 provides a rotational force (torque) to the drive shaft 16 , which when coupled to a load of some description is able to efficiently move that load.
  • the rotational power is used to rotate wheel axles causing the vehicle to move forward or rearwards.
  • a fuel supply such as gasoline or diesel, would be coupled to the cylinder head 12 (valving block) via an appropriate fuel distributor, such as a carburetor.
  • An ignition source such as a spark plug (not shown) is provided to initiate ignition of the fuel. When ignition occurs, sufficient explosive force is generated to drive the piston 28 longitudinally along the first longitudinal axis 26 within the cylinder 24 .
  • first and second crankshafts 60 , 62 are caused to rotate synchronously in opposite directions by the downward thrust of the piston 28 on the connecting arms 30 , 32 .
  • the rotation of the crankshafts 60 , 62 triggers rotation of the beveled pinion gears 68 , 70 , which contra-rotate about the second axis of rotation 76 , and through the meshing engagement with the static fixed beveled gear ring 100 , the piston 28 and the cylinder 24 together with the other moving parts rotate about the cylinder first longitudinal axis 26 .
  • the drive assembly 34 rotates the drive shaft 16 to transmit drive to the working load (not shown).
  • the contra-rotation of the connecting arms 30 , 32 provides a balanced power transmission that minimizes vibration and therefore noise generation. All components illustrated in FIGS. 4 and 5 rotate about the first cylinder longitudinal axis 26 during operation of the engine 10 . As a result of this, the fuel economy is advantageously improved.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
  • Transmission Devices (AREA)
US15/331,395 2016-10-21 2016-10-21 Balanced rotary engine Abandoned US20180112594A1 (en)

Priority Applications (12)

Application Number Priority Date Filing Date Title
US15/331,395 US20180112594A1 (en) 2016-10-21 2016-10-21 Balanced rotary engine
CA2982945A CA2982945C (en) 2016-10-21 2017-10-18 Balanced rotary engine
PCT/CA2017/000228 WO2018072007A1 (en) 2016-10-21 2017-10-19 Balanced rotary engine
JP2019521730A JP2019532218A (ja) 2016-10-21 2017-10-19 平衡型ロータリエンジン
EP17862693.3A EP3510249B1 (en) 2016-10-21 2017-10-19 Balanced rotary engine
MX2019004504A MX2019004504A (es) 2016-10-21 2017-10-19 Motor rotativo equilibrado.
KR1020197011032A KR102454944B1 (ko) 2016-10-21 2017-10-19 평형 로터리 엔진
AU2017346955A AU2017346955A1 (en) 2016-10-21 2017-10-19 Balanced rotary engine
CN201780065214.9A CN110139970A (zh) 2016-10-21 2017-10-19 平衡转缸式发动机
SG11201903375PA SG11201903375PA (en) 2016-10-21 2017-10-19 Balanced rotary engine
TW106136149A TWI763726B (zh) 2016-10-21 2017-10-20 平衡旋轉式引擎
US16/412,344 US10954851B2 (en) 2016-10-21 2019-05-14 Balanced rotary engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US15/331,395 US20180112594A1 (en) 2016-10-21 2016-10-21 Balanced rotary engine

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US16/412,344 Continuation US10954851B2 (en) 2016-10-21 2019-05-14 Balanced rotary engine

Publications (1)

Publication Number Publication Date
US20180112594A1 true US20180112594A1 (en) 2018-04-26

Family

ID=61968941

Family Applications (2)

Application Number Title Priority Date Filing Date
US15/331,395 Abandoned US20180112594A1 (en) 2016-10-21 2016-10-21 Balanced rotary engine
US16/412,344 Active US10954851B2 (en) 2016-10-21 2019-05-14 Balanced rotary engine

Family Applications After (1)

Application Number Title Priority Date Filing Date
US16/412,344 Active US10954851B2 (en) 2016-10-21 2019-05-14 Balanced rotary engine

Country Status (11)

Country Link
US (2) US20180112594A1 (zh)
EP (1) EP3510249B1 (zh)
JP (1) JP2019532218A (zh)
KR (1) KR102454944B1 (zh)
CN (1) CN110139970A (zh)
AU (1) AU2017346955A1 (zh)
CA (1) CA2982945C (zh)
MX (1) MX2019004504A (zh)
SG (1) SG11201903375PA (zh)
TW (1) TWI763726B (zh)
WO (1) WO2018072007A1 (zh)

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1193993A (en) * 1967-07-26 1970-06-03 Wilfred John Lewington A Rotary Reciprocatory Machine, such as an Internal Combustion Engine, Pump or Compressor
US4043301A (en) * 1975-06-20 1977-08-23 Templet Industries Incorporated Internal combustion engine
DE2857590A1 (de) * 1978-11-17 1980-12-11 Townsend Engineering Co Internal combustion engine
JPS61177217U (zh) * 1985-04-24 1986-11-05
JPS6345424A (ja) * 1986-08-13 1988-02-26 サミユエル・エム・ブラシントン 内燃機関
NZ270736A (en) * 1995-03-17 1998-12-23 Noel Stephen Duke Wobble plate engine with pairs of rotating cylinders around output shaft, with port plates in end covers
DE19620212A1 (de) * 1996-05-20 1996-12-12 Robert Ott Rotierender Verbrennungsmotor
US6810849B1 (en) * 1999-01-25 2004-11-02 Briggs & Stratton Corporation Four-stroke internal combustion engine
US6357397B1 (en) * 2000-05-08 2002-03-19 Leo Kull Axially controlled rotary energy converters for engines and pumps
GB0105570D0 (en) 2001-03-07 2001-04-25 Rcv Engines Ltd A rotating cylinder valve engine
US7428885B2 (en) 2005-01-13 2008-09-30 Advanced Engine Technologies, Inc. Rotary engine employing undulating ramp driven by paired reciprocating pistons
BRPI0606277A2 (pt) * 2005-03-16 2009-06-09 Searchmont Llc máquinas giratórias baseadas em eixo geométrico radial, esférico
KR20070058719A (ko) * 2005-12-05 2007-06-11 이병규 신귀한 엔진
CN101220764B (zh) * 2007-01-11 2011-06-22 光阳工业股份有限公司 引擎导风罩
EP2137379A4 (en) * 2007-04-09 2010-05-19 Michel Arseneau ROTARY ENGINE
DE102010024346A1 (de) * 2010-06-18 2011-12-22 Knorr-Bremse Systeme für Schienenfahrzeuge GmbH Luftgekühlter Kolbenkompressor mit spezieller Kühlluftführung
CN103061818B (zh) * 2011-10-18 2014-09-03 周登荣 具有补充压缩空气回路的压缩空气发动机总成

Also Published As

Publication number Publication date
WO2018072007A1 (en) 2018-04-26
AU2017346955A1 (en) 2019-04-18
KR20190108554A (ko) 2019-09-24
EP3510249A4 (en) 2020-01-15
SG11201903375PA (en) 2019-05-30
EP3510249A1 (en) 2019-07-17
EP3510249B1 (en) 2023-06-07
CA2982945A1 (en) 2018-04-21
US20190376448A1 (en) 2019-12-12
TW201819750A (zh) 2018-06-01
CA2982945C (en) 2020-12-22
WO2018072007A8 (en) 2018-09-20
TWI763726B (zh) 2022-05-11
CN110139970A (zh) 2019-08-16
JP2019532218A (ja) 2019-11-07
MX2019004504A (es) 2019-12-02
KR102454944B1 (ko) 2022-10-17
US10954851B2 (en) 2021-03-23

Similar Documents

Publication Publication Date Title
US7677207B2 (en) Rotary internal combustion engine
PT799371E (pt) Motor rotativo de pistoes axiais
TW561217B (en) Rotary engine
WO1996016282A1 (en) Geared reciprocating piston engine with spherical rotary valve
US20070125320A1 (en) Oil-cooled internal combustion engine with rotary piston wall
US5123394A (en) Rotary reciprocating internal combustion engine
CN102322338B (zh) 双转子旋转活塞发动机
US10954851B2 (en) Balanced rotary engine
US20100108034A1 (en) Rotary Engine
JP4521785B1 (ja) 回転ピストン機械
CN201934186U (zh) 旋转式活塞内燃机
US2650676A (en) Lubrication of wobble plate internal-combustion engines
US20060219193A1 (en) Optimized linear engine
WO2004072441A1 (en) Engine with rotary cylinder block and reciprocating pistons
CN218206853U (zh) 一种转子结构及具有该转子结构的新型转子发动机
CA2512396A1 (en) Optimized linear engine
RU2023896C1 (ru) Колесный силовой узел
CN116122957A (zh) 一种新型转子发动机结构及其工作方法
CN102656350A (zh) 高荣斯奇的相对径向旋转活塞发动机
CZ200348A3 (en) Reciprocating-piston engine
AU2004210876A1 (en) Engine with rotary cylinder block and reciprocating pistons

Legal Events

Date Code Title Description
STPP Information on status: patent application and granting procedure in general

Free format text: NON FINAL ACTION MAILED

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION

AS Assignment

Owner name: QUEBEC ENGINE TECHNOLOGIES, LLC, WASHINGTON

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:ARSENEAU, MICHEL;REEL/FRAME:052753/0029

Effective date: 20200316