Balancer control device for multiple-cylinder four-cycle engine

• US 4,608,952 A
• Filed: 07/15/1985
• Issued: 09/02/1986
• Est. Priority Date: 07/18/1984
• Status: Expired due to Fees

• Current Assignee: Mazda Motor Corporation
• Original Assignee: Mazda Motor Corporation
• Inventors: Tanaka, Hideki, Umemura, Kyoichi, Morita, Shigeru
• Primary Examiner(s): Lazarus Ira S.
• Application Number:
  US06/754,997
• Time in Patent Office: 414 Days
• Field of Search: 123/198 F, 123/192 B, 123/DIG. 6, 123/DIG. 7
• US Class Current: 123/198.00F
• CPC Class Codes: F02B 2075/027 four
• CPC Class Codes: F02B 2075/1808 two
• CPC Class Codes: F02D 17/02 Cutting-out cutting-out engines in multiple engine arrangements F02D25/04
• CPC Class Codes: F16F 15/264 Rotating balancer shafts F16F15/262 takes precedence
• CPC Class Codes: G01M 1/36 by adjusting position of masses built-in the body to be tested

Abstract

A multiple-displacement engine which can be operated either in a full-displacement operation in which all the cylinders are operative or a two-cylinder operation in which only two of the cylinders are operative is provided with a balancer control device. The balancer control device comprises a balancer which is driven at the same rpm as the engine output shaft during the two-cylinder operation and reduces the primary vibration generating moment imparted to the engine structure due to explosion, an engine load sensor for detecting engine load, an engine rpm sensor for detecting the engine speed and a balancer changing mechanism which changes the vibration generating moment of the balancer according to the operating condition of the engine so that the vibration generating moment of the balancer approximates the primary component of the vibration generating moment of the engine structure due to explosion thereby suppressing the primary vibration generating moment of the engine structure over the entire operating range during two-cylinder operation.

Claims

1. In a multiple-cylinder four-cycle engine which can be operated in two-cylinder operation in which two cylinders are operated so that the power stroke of one cylinder occurs with a crank angle phase difference of 360°

with respect to the power stroke of the other cylinder,

a balancer control device comprising a balancer which is driven during the two-cylinder operation of the engine to generate a primary vibration generating moment which reduces the primary vibration generating moment imparted to the engine structure due to explosion during the two-cylinder operation, an engine load detecting means for detecting engine load, an engine rpm detecting means for detecting the engine speed and a balancer changing means which changes the primary vibration generating moment of the balancer according to the operating condition of the engine so that the primary vibration generating moment of the balancer approximates the primary vibration generating moment of the engine structure due to explosion thereby suppressing the primary vibration generating moment of the engine structure over the entire operating range during the two-cylinder operation.

2. A balancer control device as defined in claim 1 in which said balancer is provided on a balancer shaft extending in parallel to the crankshaft of the engine and is rotated at the same speed as the crankshaft, and said balancer changing means reduces the product of the rotational radius of the center of gravity of the balancer and the mass of the balancer for a given engine load with increase in engine speed and increases the same for a given engine speed with increase in the engine load.

3. A balancer control device as defined in claim 2 in which said balancer comprises a plurality of balancer pieces which are mounted on the balancer shaft and the centers of gravity of which are deviated from the axis of the balancer shaft, and said balancer changing means is arranged to rotate at least one of the balancer pieces about the axis of the balancer shaft.

4. A balancer control device as defined in claim 3 in which said at least one balancer piece to be rotated by the balancer changing means is provided with splines and said balancer shaft is provided with splines which are engaged with the splines of the at least one balancer piece so that the at least one balancer piece is rotated about the axis of the balancer shaft by moving the balancer piece in the axial direction of the balancer shaft.

5. A balancer control device as defined in claim 4 in which said balancer comprises a pair of balancer pieces respectively provided with splines, and said balancer shaft is provided with first and second splines the helix angles of which intersect with each other, the first splines of the balancer shaft being engaged with the splines of one of the balancer pieces and the second splines of the balancer shaft being engaged with the splines of the other balancer pieces so that the balancer pieces are rotated about the axis of the balancer shaft in opposite directions by moving them in the axial direction of the balancer shaft.

6. A balancer control device as defined in claim 2 in which said balancer changing means changes the product of the center of gravity of the balancer and the mass of the balancer to satisfy the following formula;

space="preserve" listing-type="equation">Pe=[Thlm.p.·

X-C2·

(Nm.p./N).sup.2 ]/C1·

(Nm.p./N).sup.2

wherein Pe represents the average effective pressure, N represents the engine speed, Nm.p. represents a preset engine speed, Thlm.p. represents the primary torque harmonic coefficient under a preset average effective pressure, C1 represents the rate of change in the torque harmonic coefficient with change in the average effective pressure, and C2 represents the value of the torque harmonic coefficient when the average effective value is zero.

7. A balancer control device as defined in claim 1 in which said engine has only two cylinders and said balancer is normally driven.

8. A balancer control device as defined in claim 1 in which said engine is a four-cylinder in-line engine two of the four cylinders of which are made inoperative in predetermined operating condition of the engine, and said balancer changing means changes at least one of the rotational radius of the center of gravity of the balancer or the mass of the balancer.

9. A balancer control device as defined in claim 8 further comprising a clutch mechanism which engages during two-cylinder operation of the engine to drivingly connect the balancer with the crankshaft and disengages to disconnect the balancer from the crankshaft during full-displacement operation of the engine.

10. A balancer control device as defined in claim 9 further comprising a retainer means which holds the balancer stationary when said clutch mechanism disengages.

11. A balancer control means as defined in claim 8 in which the rotational radius of the center of gravity of the balancer is nullified while the engine is operated in the full-displacement state.

12. A balancer mechanism for an engine comprising a balancer which is supported for rotation about a rotational axis in parallel to the output shaft of the engine and has a center of mass at a position deviated from the rotational axis, the balancer comprising at least one balancer piece having a center of mass at a position deviated from the rotational axis of the balancer;

means for rotating the balancer at a speed having a predetermined ratio to the rotational speed of the output shaft; and

a changing means for changing the distance between the rotational axis of the balancer and the center of mass of the overall balancer by rotating the balancer piece about the rotational axis of the balancer according to the operating condition of the engine.

13. A balancer mechanism as defined in claim 12 in which said at least one balancer piece is mounted on a balancer shaft extending along the rotational axis of the balancer and is provided with splines and the balancer shaft is provided with splines which are engaged with the splines of the at least one balancer piece so that the at least one balancer piece is rotated about the axis of the balancer shaft by moving the balancer piece in the axial direction of the balancer shaft.

14. A balancer mechanism as defined claim 12 in which said balancer comprises a pair of balancer pieces and said changing means changes the angular position of both the balancer pieces with respect to the overall balancer to change the distance between the rotational axis of the balancer and the center of mass of the overall balancer.

15. A balancer mechanism as defined in claim 14 in which said changing means changes the angular position of the balancer pieces in opposite directions by the same angle.

16. A balancer mechanism as defined in claim 14 in which said balancer pieces are respectively provided with splines, and said balancer shaft is provided with first and second splines the helix angles of which intersect with each other, the first splines of the balancer shaft being engaged with the splines of one of the balancer pieces and the second splines of the balancer shaft being engaged with the splines of the other balancer pieces so that the balancer pieces are rotated about the axis of the balancer shaft in opposite directions by moving them in the axial direction of the balancer shaft.