Crankless reciprocating engine and gyroscopic power transmission system

• US 4,295,381 A
• Filed: 02/16/1979
• Issued: 10/20/1981
• Est. Priority Date: 04/08/1977
• Status: Expired due to Term

• Current Assignee: Virgil A. Hinds
• Original Assignee: Virgil A. Hinds
• Inventors: Hinds, Virgil A.
• Primary Examiner(s): Bonck, Rodney H.
• Application Number:
  US06/012,841
• Time in Patent Office: 977 Days
• Field of Search: 74/5 R, 74/5.22, 74/126, 60/DIG. 1, 60/516, 92/117 A
• US Class Current: 74/5.00R
• CPC Class Codes: F02G 1/0435 the engine being of the free piston type
• CPC Class Codes: G01C 19/02 Rotary gyroscopes
• CPC Class Codes: G01C 19/30 Erection devices, i.e. devices for restoring rotor axis to a desired position for instrument indicating the vertical G01C19/46
• CPC Class Codes: Y10T 74/12 Gyroscopes
• CPC Class Codes: Y10T 74/1218 Combined
• CPC Class Codes: Y10T 74/1526 Oscillation or reciprocation to intermittent unidirectional motion

Abstract

A constant torque power transmission consisting of a rotating mass, or gyroscope, rotating around a first axis and supported by a frame or enclosure in turn pivotally supported about a second axis at right angle to the first axis by a gimbal, the gimbal being pivotably supported around a third axis disposed at right angle to the second axis. The reciprocating member of a crankless reciprocating engine, of the free piston or free-cylinder type, oscillates the gimbal and the rotating mass about the third axis, causing the rotating mass frame or enclosure to develop a precessional force oscillating about the second axis. The oscillating precessional force is applied to an output shaft through a one-way clutch assembly.

Claims

1. A crankless reciprocating engine and power transmission system comprising means for supporting and substantially linearly guiding an oscillating member of said engine, a mass rotating about a first axis, said rotating mass being in a frame pivotably supported by a gimbal about a second axis at right angle to said first axis, pivot means pivotably supporting said gimbal about a third axis at right angle to said second axis and at variable angle relative to said first axis, means coupling said engine oscillating member to a point of said gimbal for oscillating said gimbal and said rotating mass frame about said third axis, power output means reciprocable by said rotating mass frame when precessionally oscillating about said second axis and biasing means urging said first axis to a position wherein said first axis is orthogonal to said third axis.

2. The system of claim 1 wherein said coupling means comprises a rigid link pivotally attached at one end to said gimbal at a point proximate to said second axis and at the other end to said oscillating member.

3. The system of claim 1 wherein said power output means comprises a rigid link pivotably attached at one end to said frame at a point substantially ninety degrees from said second axis and at its other end to a crank driving a one-way clutch member connected to a rotatable shaft.

4. The system of claim 3 wherein said power output means comprises a second rigid link pivotably attached at one end to said frame at a point substantially ninety degrees from said second axis and at its other end to a crank driving a one-way clutch member connected to said rotatable shaft.

5. The system of claim 1 further comprising a second crankless reciprocating engine, means for supporting and substantially linearly guiding an oscillating member of said engine, and means coupling said second engine oscillating member to said gimbal at a point substantially 180°

away from said first-mentioned point.

6. The system of claim 1 wherein said biasing means is a pair of tension springs diametrally connected between said gimbal and said frame.

7. The system of claim 1 wherein said biasing means is a pair of tension springs diametrally connected between said gimbal and a stationary support.