Abstract
A tangential force internal combustion engine invention utilizes the four cycle internal combustion engine process. Working gas chambers are formed via a torroid in the housing and two adjacent piston assemblies. Pistons, ring seals, and inner seal plate elements seal this chamber. The four gas cycles are spaced over the 360 degree torroid chamber with gas ports appropriately placed. One power vane (PV) and one reaction vane (RV) connect to a central shaft with pistons attached to each vane end. The PV produces driving torque on a central shaft through an Overrunning Clutch System (OCS). At specific angles and for controlled durations the PV and VN are slowed, stopped, held to the housing, and then accelerated and coupled to the shaft. Vane movement is controlled by gears, cam ramps, and pin mechanisms operating via three independent but time-coordinated systems. The power vane has no controlled acceleration; combustion pressure serves to immediately couple this vane to the shaft via the OCS. This immediateness and direct-coupling are thought to provide efficiency.
Claims
1. an internal combustion engine is which relies on two types of vanes, each of which has cyclic movement incorporating holds such that four Otto cycles can occur within a moving chamber formed by the ends of two adjacent pistons at the vane ends and located in a torroid chamber enclosed via multiple seals.
2. a method of moving an engine vane directly with a shaft by locking an overrunning clutch roller element via ramps that push a pin through a hole in said vane thus inserting a finger end into the clearance side of the roller element cavity.
3. a vane slot, gears, pin assemblies, and ramps such that a pin is pushed across a timing gear and into a vane slot via a fixed ramped cam in the housing thus initiating or halting movement of said vane upon 90 degrees of timing gear rotation.
4. a method of holding vanes to the housing via a circumferential end face ramp in a timing gear such that a pin is pushed completely thru the housing and into a matching hole in the vane.
Description
BRIEF DESCRIPTION OF VIEWS OF THE DRAWINGS
[0017] FIG. 1 shows a longitudinal section and a cross section of the invention.
[0018] FIG. 2 shows a different longitudinal section and different cross section of the invention.
[0019] FIG. 3 shows a different longitudinal section and different cross section of the invention with a different possible combustion chamber shape than previous two figures.
[0020] FIG. 4 shows a cross section of the combustion chamber and sealing components and a longitudinal view of same.
[0021] FIG. 5 shows two views of the same vane-roller element-shaft area under different loading conditions.
[0022] FIG. 6 depicts the operational cycles and derives the timing gear equation.
[0023] FIG. 7 plots the timing gear equation for inch sizing of gears and continuous gear sizes.
DETAILED DESCRIPTION OF THE INVENTION
[0024] The present invention is named a Tangential Force Internal Combustion Engine (TFICE) and it utilizes the typical four OTTO cycles over the 360 degrees of the torroid chamber. Typical intake and compression cycles of approximately 9:1 are utilized and the power duration is 90 degrees shaft or less in the present manifestation. Intake and exhaust flows into the torroidal combustion chambers are thru ports that are covered and uncovered by piston motions. A one way flow valve may be used at each port to prevent wrong gases from entering the wrong port.
[0025] The best description of the TFICE begins with Section A-A of FIG. 1 and Section B-B of FIG. 2. There are two sets of vanes that are each essentially symmetrical across the centerline of the engine. One is termed the Power Vane (PV) and the other is the Reaction Vane (RV). These vanes are designed and assembled onto the shaft much like the hinges of a door in that the vanes share shaft space by being segmented at the shaft bore. The biggest deviation from the door hinge analogy is that the vanes continue across the shaft, each vane being a single assembly with arms and pistons going outward from the shaft in both directions encompassing the diameter of the engine section. There is complete symmetry of the arm surface features across the centerline as shown in Section B-B. Symmetry is lost at sections A-A and C-C since each vane has just one OCS pin assembly. The OCS pin assembly for the Reaction Vane (RV) is shown in Section C-C. The combustion chamber is shown in FIG. 1 left view as an oval cross section and a torroid around the housing best seen in FIG. 2 Section B-B. This oval cross section is changed to a circular cross section in FIG. 3 as this would provide easier piston sealing. However the oval combustion section would provide easier sealing of the inner torroid area, a more difficult sealing problem. Higher complexity of the piston is hinted at in FIG. 4 but is not fully developed in any drawing herein as a slot is needed for each piston to fit a tab for each vane end. FIG. 4 provides a simplified shape of the piston and provides a sketch of a possible combustion chamber as ignition is to occur. FIG. 4 acknowledges that the combustion chamber needs seal elements for the torroid inner area to fully close it. The seal elements and piston shown are only a first thought and serve to complete possible component design for vital functions. Somewhat standard piston rings could be needed at both ends with the combustion chamber side certainly needing more than the single ring shown. FIG. 4 shows the inside seal elements as discrete plates that are set onto the narrow opening on the inner portion of the torroid. This opening is needed for the vanes but the opening can be narrow as internal bending of the vane arm is best resisted in the circumferential direction anyway.
[0026] The seal elements for the torroid found in FIG. 4 are individual plates that are set out and held in place against a ledge and against each other during combustion. They are collected during exhaust. This concept presents multiple concerns and so more thought needs to be given to this problem of forming a complete chamber that expands or contracts as vanes move through various cycles. This sealing function must resist both combustion pressures and chamber vacuums during the intake cycle. No claims are made herein for the sealing design of FIG. 4.
[0027] An Overrunning Clutch System (OCS) is integral to the operation of this engine. Vane movement must be controlled so that vanes can move fixed with the shaft, as during power transfer or for other cycles needs. At various times a vane will need controlled deceleration and then holding to the housing for fixed lengths of time. The OCS allows these events but cannot perform all above mentioned requirements. FIG. 5 shows the roller element in operation for the case of the vane being held to the housing and the case where combustion locks the vane assembly (vane plus OCS assembly) to the shaft. Besides allowing free vane motions the OCS of this invention has an additional feature that forces the roller element into the locked position, see items 8 in FIGS. 1 and 3. Each vane has one pin that is controlled by item 9 (OCS ramp). The ramp is designed to move the pin into the roller element free space once the vane has fully accelerated to shaft speed.
[0028] FIGS. 1 to 3 show the components for controlling acceleration or deceleration of the vanes. Note that the PV has no controlled acceleration; it benefits fuel efficiency that the Power Vane locks quickly to the shaft upon the start of combustion through the overrunning clutch. The Reaction Vane (RV) has controlled acceleration and deceleration through assigned gears, pins, ramps, and slots in the end of the vane for receiving the well timed pin insertion. Both PV and RV have timing gears with pins that are placed and timed so that the pin is pushed into the lower length of the vane slot, where the angular velocity of the vane's slot point is lowest and best matches that of the pin. As the timing gear rotates the pin looses angular velocity with respect to the engine centerline and thus the vane decelerates. After 90 degrees of timing gear rotation the pin angular velocity is zero wrt to the engine centerline. Thus the vane is momentarily stopped. This pin is allowed out via the ramp and spring. Coincidentally, another pin, located in the housing, (item 4) is pushed into a corresponding hole in the vane via a ramp on the gear face. Said ramp holds the pin for the prescribed time for the completion of combustion (RV being held) or exhaust (PV being held). As the PV has no controlled acceleration, this vane's angular motion is too fast compared to the cycle of controlled acceleration of the RV. Thus the PV must be held longer during exhaust to compensate and bring the two vanes into timing sync.
[0029] A complete development of the steady state engine operation is seen in overview in FIG. 6. The events begin in the upper left with the start of combustion. Subsequent events move to the right and the vane being fixed or moved is showed via comparison of events. It was important to develop an equation that related the length of the power stroke to the sizing of gears that control vane motion. This equation is developed in FIG. 6 and the ratio of shaft to timing gear sizes is plotted in FIG. 7. FIG. 7 was derived from inputting fixed inch diameter gears (easily obtainable) in simple ratios. This simple gearing serves to make a prototype easier but a developed engine would likely have gearing that varies by a single or a few teeth between the shaft gear and timing gear.
[0030] The present invention will need proper sizing and metallurgy of the shaft and OCS components for adequate life against contact fatigue. It's thought that the detail design will incorporate pressing together 180 degree sectional assemblies containing the OCS mechanism while bolting together vane halves, akin to crushing a rod bearing on the conrod assembly. Hardened (or surface hardened) shafts, roller elements, and OCS housing will be needed. Assembly of the shaft, vanes, and OCS subassembly will need to be done outside the housing. There will need to be temporary means of holding roller pin elements, perhaps grease that could be flushed before running. Torroidal shaped pistons could be fitted that are slotted to accept the fitting of vane ends that are essentially tabs. Excess axial clearance is needed in each piston so as to prevent axial loading of the pistons thru thermal growth of vanes. This engine will bring new thought patterns to the details of component design and assembly. The most basic principles of good engine design will still apply but in unique ways. It cannot be the goal of this first patent to foresee and design in detail for all possibilities.
[0031] This TFICE engine will need a strategy for starting since designed steady state operation relies on combustion alone for movement of the PV for a small portion of its travel. Detailed drawings have not been made but the thought process is to have a starter motor that turns the shaft and another starting only system that moves the Power Vane via a pin in slot similar to that of the three acceleration/deceleration mechanisms. Alternatively the PV could be moved via liner actuator to put it on the ramp of the OCS pin prior to turning the shaft.
[0032] There is a possible concern with the PV loosing timing as it has a portion of its cycle left uncoupled and relying on combustion to lock it to the shaft. In realty this portion does not need to exist for any significant length as inserting the OCS pin in a timed manner with the start of ignition should be possible. Thus each change of event would be controlled essentially by the shaft and then starting could be in the usual manner. The changeover from being held to full shaft motion at ignition is a concern as it has no acceleration control. Good materials for contact stress (carburized shaft and roller element housing, 52100 pins) and a minimum of excess clearance should provide adequate life. This changeover during starting will be using a low speed, low torque starter motor and so should be less concern. Overlap of a hold and move mechanism occurring coincidently could be a possibility depending on tolerences, this must be considered in every case. As a safety the various pins could have a tapered end design and/or chamfered holes that prevent pin breakage at maximum material conditions.
[0033] Other mechanisms for safety, cooling, lubrication, other sealing functions, fuel and air mixture and delivery, ignition and noise suppression are generally not shown since standard design methodology can be applied. Additional features for facilitating assembly (ie ports and covers) are generally not shown. Fasteners have not been generally shown for this patent but should follow good Engineering practices.
[0034] The present application does not allow for unequal length cycles (ie Atkinson cycle equivalent). However the concept of an Atkinson cycle applied to a TFICE type engine could have huge efficiency benefit gains, perhaps more than that provided to piston engines. It is conceptual that a near 360 degree tangential force power stroke is possible but the current limitation is ability to seal the inside of the torroid chamber over those angles.
DETAILED DESCRIPTION OF DRAWINGS
[0035] Reference FIG. 1 for following major components: [0036] 1. Items (1), housing sections, a multiple piece design with the major two halves bolted around the circumference. Bore for the shaft (7) is precisely aligned, round and straight. This housing locates the shaft, three timing gears, two item (4) hold pins, a precisely located toroid (but shown with an oval section FIG. 1) which forms part of the combustion chamber, and multiple hold springs for the combustion chamber seal plates (not shown above). Circular based ramps controlling items (9) are located in one end of this housing. [0037] 2. Item (2), Power Vane (PV), is located on the shaft via items (6), roller elements, of which twelve are shown above for the PV. Another 12 of item (6) are not shown in FIG. 1 but are utilized to locate item (10), Reaction Vane, on the shaft. The PV fits mostly inside the RV and both vanes are fitted on the shaft like a door hinge. Unlike a door hinge both vanes continue across the shaft in a symmetrical fashion. Note that the combustion chamber is circular in later figures which is preferred to aid sealing. [0038] 3. Item (3), timing gear, is located on a shaft (not shown) bolted into (1). Each timing gear contains a ramp to control item (4) hold pin and item (5) pin assembly that controls acceleration or deceleration. [0039] 4. Item (4), hold pin assembly, is located in the housing. When the PV has slowed to zero velocity, the gear ramp pushes and holds this pin further across the housing and into a corresponding hole in the PV. (Note that the length of the vane where the pin enters is proportioned longer in a future figure as that provides for sealing functions). [0040] 5. Item (5), pin assembly, is located in the timing gear and is controlled by a ramp in the housing. This pin is pushed into the PV slot and slows the PV from max velocity to zero as the timing gears turns 90 degrees. Each of three timing gears havethis pin assembly for its respective PV or Reaction Vane. [0041] 6. Items (6), overrunning clutch roller elements, are located in the PV and Reaction Vane (RV). Details of item 6 are shown in a later figure. Precise geometry of this Overrunning Clutch System (OCS) is needed as it allows the vanes to either be held to the housing or be locked with the shaft. The OCS consists of a multitude of roller elements, either ball or needle rollers. Each is located in a hole or slot with precise geometry and one roller element in each vane can be locked between the shaft and vane by application of the pin of item (9). [0042] 7. Item (7), shaft, is located in a precise bore in the housing. The RV and PV are precisely located on it thru item (6) OCS. A shaft gear is bolted on one end to drive the three timing gears. Two locating plates and two sets of seals are used on the ends, per typical practice. Power is taken off the left end in FIG. 1. [0043] 8. Item (8), OCS pin assembly, one is located in each vane. This pin is controlled by item (9) and the pin acts to push the OCS roller element into a locked position when item (9) dictates. [0044] 9. Item (9), OCS ramp, is a circular ramp that actuates the OCS pin over a strategic portion of its 360 degrees. There is one OCS for each of the two vanes. Long movements of the RV are via actuation of the OCS pin via this ramp. The PV will drive the shaft with the start of combustion thru the OCS roller elements before its corresponding OCS ramp is activated. Activation of this OCS ramp for the PV shortly after combustion is part of a strategy to aid the starting procedure. [0045] 10. Item (10), Reaction Vane, is similar to the PV with one essential exception. The RV has two timing gears and associated mechanisms. The RV requires an acceleration timing gear and pin assemblies that is not used with the PV. Since the PV has no acceleration timing gear its hold time must account for this faster response by increasing the PV hold time as defined in a later figure. [0046] 11. Item (11) is a spring mechanism to hold individual sealing elements against the open rim of the torroid chamber
[0047] Reference FIG. 2 for the following: [0048] 1. Items (12) are two timing gears shown as dashed circles in the right side only of FIG. 2. These gears control RV acceleration or deceleration. Each timing gear is in mesh only with the shaft gear. [0049] 2. Item (3) timing gear serves to accelerate the RV from a fixed position to a position where the item (8) OCS pin assembly can take over control of vane movement. Vane acceleration is accomplished when the gear rotates the pin end onto the housing ramp and thus pushes the item (5) pin into the RV slot at the 90 degree mark (this mark is to the right of the 27 degree angular measurement shown on FIG. 2). There the pin has zero angular rotation wrt the engine shaft. Coincidentally the item (4) hold pin is released. After 90 degrees of timing gear rotation the angular acceleration is essentially the same as the shaft. At that point the ramp allows the pin assembly to move out of the vane slot and coincidentally the hold pin mechanism is inserted to hold the RV for a specified length of rotation.
[0050] Note that the PV gear will theoretically need to hold an extra 90(5/6)27=48 degrees since the RV moves 27 degrees during its gear-controlled acceleration as the shaft moves 90 degrees (with this particular 5:6 ratio of timing gear to shaft gear). This movement during its acceleration lets the RV get ahead of the PV from cycle to cycle. There is an assumed instantaneous acceleration of the PV from combustion. [0051] 3. Item (13) is the shaft gear that turns CCW in the right side view of FIG. 2. [0052] 4. Item (14) are location plates to define axial position of the shaft. [0053] 5. Item (15) are seal elements, typical for shafts running in housings containing oil.
[0054] Reference FIG. 3 for the following: [0055] 1. Item (8) OCS pin assembly and item (9) OCS ramp are shown for the RV. Note that the start of the ramp which clamps the RV and shaft together is separated from the hold position by the angular distance of the timing gear acceleration mechanism. This angular distance was shown to be 27 degrees in FIG. 2 (for shown gear ratio). The end of this ramp occurs at the point where the deceleration gear pin is first inserted (27 degrees prior to the hold point). [0056] 2. Item (16) is an exhaust port with a one way valve. [0057] 3. Item (17) is an intake port with a one way valve. The PV contains rings on each end to prevent mixing, shown in a later drawing.
[0058] Reference FIG. 4 for the following: [0059] 1. Item (18), seal pack, consists of a multitude of individual seal plate elements. Each has a single or compound bend. Ends are angled to fit into each other. Plates are spring steel and fit into the housing annulus. An end tang is located at one end to facilitate locating each element against the other or initial chamber seal. Items (11), springs, are screwed into the housing at the introduction point of the each seal element. Locations correspond to initial placement of seal elements within the combustion chamber and at corresponding spacings in the exhaust, intake, and compression chamber locations. [0060] 2. Item (19) is a spring assembly that pushes seal elements into the seal area. Items (18) and (19) are used two times in the PV symmetrically across the engine centerline.
[0061] Reference FIG. 5 for the following:
[0062] 1. Items 6, roller elements, are shown in operation for two cases: 1. where the vane is not making torque and 2. the case where the vane is making torque.
[0063] Steady State Operation Cycle
[0064] Steady state operation is shown in FIG. 6 and the equation developed in this figure follows:
RVC=2xr+2y Eqn 1.
[0065] Where [0066] RVC is the Reaction Vane Cycle, measured in shaft degrees. [0067] x=angle of timing gear to decelerate or accelerate a vane. In this invention x=90 degrees [0068] r=Timing Gear Dia./Shaft Gear Dia. [0069] y=Angular duration of the PV during combustion as it singularly drives the shaft with tangential torque
r=RVC/360 (this follows from the definition of r) Eqn 2.
[0070] Thus for the designs depicted in the present invention:
360r=180r+2y
y=90r Eqn 3.
[0071] Equation 3 is plotted in FIG. 7. It relates gear sizes to the angular locations where hold/move transitions begin.
[0072] The designs depicted herein utilize a single shaft gear and three timing gears driven directly from said gear. No intermediate gears are shown but these could be useful to limit the angular displacement of the vanes during acceleration or deceleration.
REFERENCES
[0073] 1. Overrunning Roller Clutch, Dietrich Reister Herzgenaurach and Wolfgang Pfluenger, Industiewerk Schaeffler, Herzodenauwach, Germany, U.S. Pat. No. 3,537,555 [0074] 2. Rotary Piston Engine, Tatsuya Kita, Mazda Motor Co. Hiroshima Jp. U.S. Pat. No. 4,926,816 [0075] 3. Improvements relating to the propulsion of aircraft and other vehicles, British patent no. 347206, filed 16 Jan. 1930
