Rotary dampers, such as the one described in U.S. Pat. No. 4,411,341 have been used to dampen movement in a variety of applications from automobile suspensions to motorcycle steering. These dampers typically operate by having chambers in a sealed body containing a viscous fluid; concentric with that body is a shaft with radially disposed sealed vanes protruding into and dividing each chamber. Damping is effected through rotation of the shaft connected to the vanes which forces the viscous fluid through restricting orifices of various designs and locations in the body. Most damper designs have been complex and bulky with many intricate parts to maintain or fail.
The present invention is a rotary damper which provides an effective, lightweight and inexpensive means to restrict and regulate flow between the chambers. The damper uses a rotor with a hollow center and passages that allow flow between chambers through the center of the rotor. Regulation is accomplished by means of a centrally located valve that is vertically adjustable by means of a threaded shaft operable by a knob on the top of the damper. This arrangement significantly reduces the complexity and weight of the damper.
Accordingly, it is an object of the present invention to simplify and lighten the rotary damper for use in applications where weight is a significant design parameter, such as racing motorcycles.
Other objects and advantages of the present invention will be apparent from the following description, the accompanying drawings and the appended claims.
As shown in
The inner body 18 has a number of chambers 19 equal to the number of vanes on the rotor 11. Each vane 13,14 divides each chamber 19 into two discrete volumes, one compressing fluid and one expanding as the rotor 11 rotates. The inner body 18 has a central hole 18A in its lower portion for the base of the rotor 12 to protrude through and provision for o-rings around the inner circumference 20A of hole 18A for sealing against rotor 12 at surface 12A. Another o-ring is provided for sealing in the outer surface of inner body 18 at 20B to allow sealing against the inside of the outer shell 22.
Threaded holes 21 are provided in the inner body 18 for securing an outer shell 22. A hole 23 is provided in the inner body 18 that communicates with of one of the bolt holes 21 in the inner body 19 to allow introduction of a viscous fluid into the chambers after the damper is assembled. Removal of a bolt or screw at 24 will allow fluid to be poured into the damper, and with means at 25 to allow air to escape during the filling process by removing another bolt at 26.
Rotor 11 has a concentric cylindrical cutout 28 that extends down just below a plurality of orifices 27. As shown in
The outer shell 22 is machined to provide close tolerances between the rotor 11 and the inner body 19 and when assembled provides a sealed unit that allows fluid to flow only through orifices 27 from one chamber to another (through the center of the rotor 28).
Changes in damping effect could be attained by varying the viscosity of the fluid in the damper or by changing the size of the orifices 27.
The preferred embodiment contemplates a centrally located flow regulator 29 that is machined to fit tightly inside the cylindrical cutout 28 of the rotor 11. This regulator 29 can be adjusted vertically by means of a threaded shaft 30 that is turned by a knob 31 on top of the damper. The shaft 30 is sealed by means of an o-ring at 32. The regulator 29 has a cylindrical surface on its circumference at 33 that will move vertically up and down blocking a portion and therefore reducing or increasing the size of the orifices 27 thereby causing variation in the damping effect.
As shown in FIG. 1 and also with reference to
This applications claims the benefit of the filing date of the previously filed provisional application 60/339,801 “Rotary Steering Stabilizer”.
Number | Name | Date | Kind |
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933076 | Houdaille | Sep 1909 | A |
1256215 | Eycleshymer | Feb 1918 | A |
1294112 | Keeler et al. | Feb 1919 | A |
1540341 | Kirby | Jun 1925 | A |
1904040 | Chapin | Apr 1933 | A |
1976796 | Milner | Oct 1934 | A |
2021428 | Peo | Nov 1935 | A |
2043489 | Peo | Jun 1936 | A |
2301318 | Peo | Nov 1942 | A |
2329923 | Magrum | Sep 1943 | A |
2819062 | Tack | Jan 1958 | A |
5901821 | Hanawa | May 1999 | A |
6082507 | Forster | Jul 2000 | A |
6318522 | Johnston et al. | Nov 2001 | B1 |
6536565 | Oliver et al. | Mar 2003 | B2 |
Number | Date | Country | |
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20030111308 A1 | Jun 2003 | US |
Number | Date | Country | |
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60339801 | Dec 2001 | US |