Internal combustion engine with variable compression ratio and variable engine displacement

Abstract

A hypocycloidal internal combustion engine containing at least one alternative displacement piston connected through a connecting rod to a crankshaft, which is connected to an epicyclic gear train. In this gear train, the planet gear carrier is connected to the output shaft, and the ring gear can be rotated (in a controlled manner) in relation to the engine block. The present invention allows the control of the compression ratio and engine displacement of the engine by adjusting the angular position of the ring gear, which can be done continuously and instantaneously, even with the engine in operation.

Claims

1. A variable compression ratio internal combustion engine comprising: a cylinder, a piston, a connecting rod, a ring gear, a planet gear, an endless screw and a crankshaft; wherein said ring gear comprises a plurality of internal teeth and a plurality of external teeth; the piston, connected by the connecting rod to the planet gear, which, in turn, is connected to the crankshaft, the planet gear is configured to engage the plurality of internal teeth of the ring gear and to travel around an inside of the ring gear, the plurality of external teeth of the ring gear is configured to engage the endless screw; wherein the endless screw is configured to rotate the ring gear in a controlled manner through a plurality of angular positions, ; said piston is configured to travel inside said cylinder between a top dead center position and a bottom dead center position as the crankshaft rotates; and said endless screw alters the angular position of the ring gear, which, in turn, alters an angular position of the planet gear when the piston is at said top dead center position and at said bottom dead center position as follows: to allow the piston reach its maximum top dead center position, the planet gear can be at =0 when the crankshaft is at =0 and to allow the piston to reach its minimum bottom dead center position, the planet gear can be at =180 when the crankshaft is at =180, and to restrict the piston from reaching its maximum top dead center position, the planet gear can be positioned at >0 when the crankshaft is at =0 and to restrict the piston from reaching its minimum bottom dead center position, the ring gear can be positioned at >180 when the crankshaft is at =180; wherein this variable positioning of the ring gear via the endless screw allows for the compression ratio to be continuously varied in response to engine operating conditions.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1shows the exploded view of the invention.

(2) FIG. 2shows the front section view of the invention.

(3) FIG. 2Ashows the lateral section view of the invention.

(4) FIG. 3shows the main components of the invention, represented as a three rod mechanism, where the point O is fixed to the origin, the rod OA (main shaft) can only rotate at the point O and the point C (piston) can only translate along the y-axis;

(5) FIG. 4shows the mechanism position at each stroke of the engine cycle;

(6) FIG. 5shows the piston movement during the engine cycle, for different angular positions () of the ring gear;

(7) FIG. 6shows the angular movement of the connecting rod during the engine cycle, for different angular positions () of the ring gear;

(8) FIG. 7illustrates the movement of the engine components at different stages of the engine cycle, when in the maximum compression ratio configuration (ring gear angular position is =0);

(9) FIG. 8illustrates the movement of the engine components at different stages of the engine cycle, when the ring gear angular position is =45;

(10) FIG. 9shows the TDC and BDC positions for different angular positions () of the ring gear;

(11) FIG. 10shows the clearance volume and engine displacement for different angular positions () of the ring gear (for an engine with maximum compression ratio of 15:1);

(12) FIG. 11shows the compression ratio for different angular positions () of the ring gear (three curves are displayed, for engines built as described by this invention but with different maximum compression ratios of 20:1, 15:1 and 10:1);

(13) FIG. 12show modification of the engine displacement with the compression ratio (three curves are displayed, for engines built as described by this invention but with different maximum compression ratios of 20:1, 15:1 and 10:1);

(14) FIG. 13illustrates a variant of the present invention with more than one planet gear in the epicyclic gearbox;

(15) FIG. 13Aillustrates a detailed view of the variant of the present invention with more than one planet gear in the epicyclic gearbox;

(16) FIG. 14illustrates a multi-cylinder variant of the present invention, where each cylinder is connected to a crankshaft, which is connected to two epicyclic gearboxes.

(17) FIG. 14Aillustrates a detailed view of the multi-cylinder variant of the present invention, where each cylinder is connected to a crankshaft, which is connected to two epicyclic gearboxes.

DETAILED DESCRIPTION OF THE INVENTION

(18) The present invention refers to a hypocycloidal internal combustion engine with variable compression ratio and variable cylinder capacity. The main components of this invention are illustrated on the FIG. 1 and FIG. 2. It is important to note that this invention can be presented in several variants which are discussed later.

(19) In the present invention, a piston (2) inside the cylinder (1) is connected by a connecting rod (4) to the crankpin journal (6) of a crankshaft (5), whose main journal (7) is fixed concentrically to the planet gear (14) of an epicyclic gear train (16). This gear train also contains a ring gear (13), which can rotate (in a controlled manner) in relation to the engine block (9) and a main shaft (15) which carries the planet gears (14) (it can have one or more planet gears). Thus, the combustion energy at the cylinder (1) is transmitted to the piston (2) to the main shaft (15) through an epicyclic gear train (16). Also, there is a mechanism (10) capable to rotate the ring gear (13) in a controlled manner. This mechanism can be constituted of an auxiliary engine (11) that actuates an endless screw (12), which is connected to a quantity of external tooth at the ring gear (13). Thus, the system has only two degrees of freedom, one being the main shaft rotation (which determines the piston position) and the other being the angular position of the ring gear.

(20) To support the kinematic analysis, the FIG. 3 shows the main components of the present invention, where the basic mechanism is represented by three rods (OA, AB, BC) on the x-y plane.

(21) The FIG. 4 illustrates different stages of the engine's cycle. The point O is fixed to the origin; the rod OA (main shaft) can only rotate around the point O; the point C (piston) can only translate along the y-axis.

(22) It is noted that in FIG. 3 and FIG. 4, the rods OA and AB have length R, the satellite gear has primitive diameter 2R and the ring gear has primitive diameter 4R. This implies that the distance between the centre lines of the crankpin journal and the main journal (19, in FIG. 2) is equal to a half of the primitive diameter (18) of the planet gears. The primitive diameter (18) of the planet gears is equal to a half of the primitive diameter (17) of the ring gear. Consequently, the radial mounting position of a planet gear axis at the main shaft (planet carrier) must correspond to a half of the primitive diameter (18) of the planet gear.

(23) Because of this configuration, the hypocycloid curve drawn by the point B is restricted to a straight-line segment that passes through the system origin (represented by the dashed line in FIG. 4). When =0, the point B draws a line collinear to the vertical axis. Consequently, the connecting rod (represented by BC) does not show any angular movement and the piston has maximum displacement. The maximum stroke of the piston is equal to the primitive diameter of the ring gear (4R). On the other hand, when the ring gear is positioned with an angle >0, as shown in FIG. 4, the point B draws a straight line that makes an angle with the vertical axis. Consequently, the connecting rod has some angular movement during the engine cycle and the piston stroke is reduced (equal to 4R cos ).

(24) It is important to note that, for the correct operation of the system, the components must be initially assembled as shown in FIG. 2. The rods OA, AB and BC shown in FIG. 4 must be aligned to the vertical axis when =0. In the context of this invention, this configuration (when =0) is noted as maximum compression ratio configuration. Similarly, the configuration when =90 is noted as minimum compression ratio configuration. Also, by convention, it is defined that the angular position () of the ring gear is positive when realized in the same direction as the main axis rotation, when the engine is in operation. These denominations are useful for the better understanding of the equations and plots described below.

(25) The FIG. 5 shows the position, velocity and acceleration of the piston relative to the main shaft angular position (), for different ring gear angular positions (). In this example, it is considered R=20 mm, L=100 mm and a constant main shaft speed of 1500 rpm. For comparison purposes, the position, velocity and acceleration of an equivalent conventional internal combustion engine are shown (identical piston maximum stroke, identical connecting rod length, crankshaft radius of 2R).

(26) The position of the piston (point C) with respect to the origin, its velocity and its acceleration can be described by the equations (1), (2) and (3), respectively. the equation (4) describes the piston position with respect to the TDC (Top Dead Center).

(27) $\begin{array}{cc}{y}_c\left(\right)=R\cos +R\cos \left(-2\right)+L\cos & \left(1\right)\\ v_{y_c}\left(,\right)=R\left[\sin \left(2-\right)-\sin \right]-\frac{R}{2n}\left\{\left[{\left(\cos 2-1\right)}^2-{\left(\sin 2\right)}^2\right]\left(\sin \sin 2\right)-2\left(\cos \cos 2-1\right)\left(\sin \sin 2\right)\left(\cos \cos 2\right)\right\},n=L/R& \left(2\right)\\ a_{y_c}\left(,\right)=-{}^{2}R\left[\cos \left(2-\right)+\cos \right]-\frac{{}^{2}R}{n}\left\{\left[{\left(\cos 2-1\right)}^2-{\left(\sin 2\right)}^2\right]\left(\cos \cos 2\right)+2\left(\cos \cos 2-1\right)\left(\sin \sin 2\right)\left(\cos \cos 2\right)\right\},n=L/R& \left(3\right)\\ s_c\left(\right)=y_c-\left(L+2R\right)& \left(4\right)\end{array}$

(28) It is noted that the piston spends more time near the TDC when compared to the conventional combustion engine. This is advantageous when in the combustion stage, which gets closer to a constant volume process, contributing to increase the amount of work generated and the efficiency of the thermal cycle. It is important to note that, when the angular position () of the ring gear is modified, the TDC and BDC (Bottom Dead Center) are delayed by an angle with respect to the main shaft, while the time period of the piston cycle is maintained.

(29) In the configuration with =0, the maximum velocity of the piston is 6.4% lower than the conventional engine and the acceleration at TDC is 28.6% lower than the conventional engine.

(30) The FIG. 6 shows the angular position () of the connecting rod when the ring gear is rotated by an angle , as in equation (5). It is noticed that the connecting rod does not have any angular movement when =0, contributing to the mitigation of undesired lateral vibrations and lateral loads at the piston, thus reducing significantly the friction losses, heat generation and cylinder wear. This configuration is illustrated in FIG. 7.

(31) As the angular position of the ring gear is modified (>0), the connecting rod shows certain angular movement during the cycle, although in a lesser magnitude than the angular movement seen in an equivalent conventional engine.

(32) $\begin{array}{cc}\left(\right)=\left\{\frac{1}{n}\left[\sin \sin \left(-2\right)-\sin \sin \right]\right\},n=L/R& \left(5\right)\end{array}$

(33) FIG. 8 illustrates how the present invention behaves at an intermediate compression ratio configuration (=45). Comparing the FIG. 7 and FIG. 8, it is clear the modification of the movement of the piston (TDC and BDC positions, for instance) and of the movement of the connecting rod, by the change in the ring gear position.

(34) The TDC and BDC positions are determined by the ring gear angular position () and can be obtained by the equations (6) and (7). The FIG. 9 shows these positions for 090. The equation (8) describes the piston stroke length, being the distance between TDC and BDC. The equation (9) represents the angular position () of the connecting rod when the piston is at TDC (or BDC).

(35) $\begin{array}{cc}\mathrm{TDC}=L\cos {}_{\mathrm{TDC}}+2R\cos & \left(6\right)\\ \mathrm{BDC}=L\cos {}_{\mathrm{BDC}}-2R\cos & \left(7\right)\\ S=\mathrm{TDC}-\mathrm{BDC}=4R\cos & \left(8\right)\\ {}_{\mathrm{TDC}}=-{}_{\mathrm{BDC}}=\left(-\frac{R}{L}\sin \right)& \left(9\right)\end{array}$

(36) The engine displacement, clearance volume and compression ratio can be calculated by the equations (10), (11) and (13). Given an engine with maximum compression ratio (given by tc.sub.0) and a piston of diameter d, the maximum engine displacement is V.sub.d.sub.0=4Rd, and the respective clearance volume (V.sub.m.sub.0) can be obtained by the equation (12).

(37) $\begin{array}{cc}{V}_d=d\left(\mathrm{TDC}-\mathrm{BDC}\right)=4Rd\cos & \left(10\right)\\ V_m=V_{m_0}+d\left(L+2R-\mathrm{TDC}\right)& \left(11\right)\\ V_{m_0}=\frac{V_{d_0}}{\left({\mathrm{tc}}_o-1\right)}& \left(12\right)\\ \mathrm{tc}=\frac{V_d+V_m}{V_m}& \left(13\right)\end{array}$

(38) Then, starting with =0, as the ring gear is rotated, the TDC and BDC positions are modified (FIG. 9) in such a way that the engine displacement is reduced, and the clearance volume is increased (FIG. 10). Therefore, it is obtained a modification of the compression ratio, as shown in FIG. 11 and FIG. 12. FIG. 12 shows the compression ratio curves for engines built as in the present invention, but with maximum compression ratios of 20:1, 15:1 and 10:1.

(39) Thus, the present invention allows the control of the compression ratio and engine displacement of the engine by adjusting the angular position of the ring gear, which can be done continuously and instantaneously, even with the engine in operation.

(40) The engine presented here can be designed in several configurations, containing more than one cylinder in different layouts. Some of these variations are exemplified by the FIGS. 13 and 14. The FIG. 13 shows a variant with more than one satellite gear on the epicyclic gearbox, reducing the loads at the gears. The FIG. 14 shows a multi-cylinder variant, where each crankshaft is connected to two epicyclic gearboxes. Moreover, its concept can be extended to compressors, pumps, generators and similar equipment.