Continuously variable transmission

• US 7,163,486 B2
• Filed: 12/06/2004
• Issued: 01/16/2007
• Est. Priority Date: 04/26/2001
• Status: Expired due to Fees

• Current Assignee: Enviolo BV
• Original Assignee: Fallbrook Technologies Incorporated
• Inventors: Miller, Donald C., Allen, David John
• Primary Examiner(s): FENSTERMACHER, DAVID MORGAN
• Application Number:
  US11/006,316
• Publication Number:
  US 20050085337A1
• Time in Patent Office: 771 Days
• Field of Search: 476/40, 476/41, 476/42, 476/36, 476/37, 476/38, 476/45, 476/61
• US Class Current: 476/45
• CPC Class Codes: B62M 11/12 with frictionally-engaging wheels B62M11/14 takes precedence
• CPC Class Codes: F16H 15/28 with external friction surface
• CPC Class Codes: F16H 15/52 in which a member of uniform effective diameter mounted on a shaft may co-operate with different parts of another member
• CPC Class Codes: F16H 61/664 Friction gearings
• CPC Class Codes: F16H 61/6649 characterised by the means for controlling the torque transmitting capability of the gearing
• CPC Class Codes: F16H 63/067 mechanical actuating means

Abstract

A continuously variable transmission is disclosed for use in rotationally or linearly powered machines and vehicles. The transmission provides a simple manual shifting method for the user. Further, the practical commercialization of traction roller transmissions requires improvements in the reliability, ease of shifting, function and simplicity of the transmission. The present invention includes a continuously variable transmission that may be employed in connection with any type of machine that is in need of a transmission. For example, the transmission may be used in (i) a motorized vehicle such as an automobile, motorcycle, or watercraft, (ii) a non-motorized vehicle such as a bicycle, tricycle, scooter, exercise equipment or (iii) industrial equipment, such as a drill press, power generating equipment, or textile mill.

Claims

1. A helicopter comprising:

motor of the helicopter;

a continuously variable transmission coupled to the motor, the continuously variable transmission comprising;

a plurality of speed adjusters;

a drive disk frictionally contacting the speed adjusters;

a driven disk frictionally contacting the speed adjusters;

a support member between the drive disk and the driven disk and frictionally contacting the speed adjusters;

a bearing disk adapted to provide rotational force to the drive disk;

a threaded member attached to an inner bore of the drive disk; and

a screw for engaging the threaded member, the screw positioned coaxial with and about a longitudinal axis of the continuously variable transmission.

2. The helicopter of claim 1, wherein the screw is adapted to receive thrust from a thrust bearing to bias the screw away from the speed adjusters.

3. The helicopter of claim 1, further comprising:

a drive shaft having a set of drive shaft ramps;

a disk having a set of screw ramps, the disk operationally engaged to the screw; and

wherein the drive shaft ramps and screw ramps are adapted to operationally engage one another.

4. The helicopter of claim 3, wherein the screw and the threaded member transfer to the drive disk axial force produced by the drive shaft ramps and the screw ramps.

5. The helicopter of claim 3, further comprising a tension member, positioned between the drive shaft ramps and the screw ramps, the tension member adapted to maintain engagement of the drive shaft ramps and the screw ramps.

6. The helicopter of claim 1, further comprising a set of perimeter ramps attached to the bearing disk, the perimeter ramps adapted to produce an axial force that is transferred to the drive disk.

7. The helicopter of claim 6, further comprising a set of ramp bearings positioned between the bearing disk and the drive disk, the ramp bearings contacting the perimeter ramps.

8. A helicopter comprising:

motor of the helicopter;

a continuously variable transmission coupled to the motor, the continuously variable transmission comprising;

a plurality of speed adjusters;

a drive disk adapted to operationally engage the speed adjusters;

a bearing disk adapted to provide rotational force to the drive disk; and

a disengagement mechanism adapted to disengage the drive disk from the speed adjusters, the disengagement mechanism positioned between the bearing disk and the drive disk.

9. The helicopter of claim 8, wherein the disengagement mechanism comprises a toothed wheel and a pawl adapted to prevent the drive disk from rotating onto the speed adjusters until an input force is applied to the transmission.

10. The helicopter of claim 9, wherein the disengagement mechanism comprises at least two pawls.

11. The helicopter of claim 9, the disengagement mechanism further comprising:

a threaded connector functionally interposed between the drive disk and the bearing disk; and

wherein a rotation of the drive disk rotates the threaded connector to disengage the drive disk from the speed adjusters.

12. The helicopter of claim 8, wherein the disengagement mechanism comprises:

a preloader having first and second ends, the first end adapted to rotate about an axis at a different rotational speed than the second end;

a bearing cage;

a toothed wheel, wherein said first end supports the toothed wheel and engages the bearing cage;

a pawl, wherein said second end supports the pawl such as to allow the pawl to engage the toothed wheel to prevent the drive disk from engaging the speed adjusters until an input force is applied to the transmission.

13. The helicopter of claim 8, wherein the disengagement mechanism comprises:

a threaded connector functionally interposed between the drive disk and the bearing disk; and

wherein a rotation of the drive disk rotates the threaded connector to disengage the drive disk from the speed adjusters.

14. The helicopter of claim 13, wherein a rotation of the bearing disk causes the threaded member to rotate and thereby operationally engage the drive disk with the speed adjusters.

15. The helicopter of claim 13, wherein the threaded member is adapted to apply an axial force to the drive disk.

16. The helicopter of claim 13, further comprising a coiled spring adapted to engage the drive disk with the speed adjusters upon supply of an input rotation into the transmission.

17. A helicopter comprising:

motor of the threaded member;

a continuously variable transmission coupled to the motor, the continuously variable transmission comprising;

a generally tubular split shaft coaxial with a longitudinal axis of the transmission and having a threaded end;

a rod having first and second ends and located coaxially within the split shaft;

a worm screw attached to the first end of the rod and having a set of external threads;

a sleeve having a set of internal threads that fit around and engage the external threads of the worm screw; and

a shifting tube that engages the second end of the rod and has a set of internal threads that fit over and engage the threaded end of the split shaft.

18. The helicopter of claim 17, further comprising a worm spring adapted to bias the rotation of the rod.

19. The helicopter of claim 18, wherein the worm spring comprises a conical spring having a first end and a second end, wherein the conical spring fits coaxially over the longitudinal axis of the transmission and is attached at the first end to the rod and is attached at the second end to a stationary object.

20. The helicopter of claim 17, further comprising:

a generally tubular grooved screw, coaxial with the longitudinal axis, having a threaded outer surface, a longitudinally grooved inner surface, and a bearing race on an inner diameter thereof; and

an annular bearing in operable contact and coaxial with the bearing race.