The present application is based on, and claims priority from, Israel Application No. 176,534, filed Jun. 25, 2006, the disclosure of which is hereby incorporated by reference herein in its entirety.
The present invention relates to a rotary-vane machine (RVM) useable as a blower, as a one-stage air or gas compressor, as a separate pressure stage in multistage air or gas compressor plants, including plants for gas liquification, for a wide range of cooling machines and for combustible gas mains, as a vacuum pump, a liquid pump and as a pneumatic or hydraulic motor, and will be referred to as HADMI RVM.
A first embodiment of the HADMI RVM according to the invention produces pressure ratios of 1.4 to 3, while a second heavy-duty embodiment is capable of producing one-stage pressure ratios of 2 to 6, particularly useful in gas compressor plants and in the cooling industry, which works with mediums having lower adiabatic coefficients.
Conventional low-pressure compressors producing pressure ratios of 1.8 to 2.1 are characterized by low efficiency, large dimensions, weight and prime costs.
A rotary-vane blower disclosed in U.S. Pat. No. 6,113,370 which has a tubular rotor rotating at uniform speed to which are fixedly attached two first vanes. Two second vanes, forming with the first vanes four chambers for the working medium, perform inside the tubular rotor an oscillatory movement whereby the volume of the chambers is alternatively reduced and increased. This oscillatory movement is produced by a camming mechanism driven by the main shaft. While this blower works at an efficiency much higher than that of conventional blowers of all types, the camming mechanism with its high contact pressure is a serious drawback when high overpressures and high pressure ratios are desired.
Another known rotary-vane device is the Kauertz engine, in which the oscillating motion is obtained by a planetary gear arrangement including large and heavy overhanging cranks and levers, and including heavy vanes, all having large moments of inertia which, given the relatively high speeds of internal-combustion engines, produce intolerably high inertial loading, strictly limiting RPM and substantially impairing the usefulness of this design.
It is thus one of the objects of the present invention to overcome the drawbacks and disadvantages of the prior art devices and to provide a mechanically efficient HADMI RVM generating minimal inertial forces, and thus, safely operatable at high speed.
In accordance with the invention, this is achieved by a rotary-vane machine, comprising a stationary, tubular housing having two sections constituted by a first section containing oil and a second, oil-free section and two pairs of ports through which a working gas may enter or exit, a housing cover plate fixedly attachable to the end of said first section and provided with a central boss member located inside said housing, a sun gear fixedly attached to said boss member, a cover disc fixedly attachable to the end of said second section and adapted to define, together with said cover plate, the longitudinal axis of said tubular housing, a tubular rotor to the inside of which are fixedly attachable two tapering vanes rotatable, together with said rotor, at a uniform speed, said rotor being provided with four ports through which a working gas may enter or exit, a first rotor end plate fixedly attached to said rotor or to its tapering vanes, a drive shaft fixedly attached to, or integral with, said first end plate connectable to an external source of rotary power and supported by at least one ball bearing located in said cover disc, a second rotor end plate fixedly attached to said rotor or to its tapering vanes and having two diametrically opposite projections, a support ring, having two post-like projections, fixedly connectable via adjustment shims to the two projections of said second end plate, a hollow oscillatable main shaft mounted in bearings seated in said first end plate, said second end plate and said housing cover plate, and being concentric with said rotor, said main shaft having a solid end of a reduced diameter, two substantially tapering vanes fixedly attached to either side of said hollow shaft by means of rods, and defining with said hollow shaft, said tubular rotor, said tapering vanes and said first and second end plates, four chambers, at least one shaft unit which rotates in bearings mounted in said second end plate and said support ring respectively, each shaft unit having attached thereto or integral therewith, an eccentric or a crank-like section, and a planet gear, at least one connecting rod having a big end and a small end, the big end being associated with said eccentrics and the small end being associated via pivots with a rocker arm pinned to said reduced main shaft end, wherein rotation of said drive shaft at a uniform speed causes said rotor, including said tapering vanes, to be rotated at the same uniform speed, while an oscillatory motion is superposed on said hollow shaft and said tapering vanes, whereby the volume of said four chambers is made to successively vary between a minimum and a maximum.
The invention further provides a rotary-vane machine, comprising a stationary, tubular housing having two different diameter sections constituted by a first section containing oil and a second, oil-free section, a housing cover plate fixedly attachable to the end of said first section and provided with a central boss member located inside said housing, a sun gear fixedly attached to said boss member, a tubular rotor to the inside of which are fixedly attachable at least two tapering vanes, rotatable together with said rotor, at a uniform speed, a first end plate fixedly attachable to said rotor or its tapering vanes and having four ports through which a working gas may enter or exit, a drive shaft pinned or made integral with said first end plate and adapted to be connected to an external source of rotary power, a stationary flange member fixedly attachable to the end of said second section and provided with two pairs of ports through which a working gas can enter or exit and adapted to define together with said cover plate a longitudinal axis of said tubular housing, a second rotor end plate fixedly attached to said rotor or to its tapering vanes and having two diametrically opposite projections, a support ring mounted on said boss member and having two post-like projections fixedly connectable via adjustment shims to the two projections of said second rotor end plate, a hollow oscillatable main shaft mounted in bearings seated in said first end plate, said second end plate and said housing cover plate and being concentric with said rotor, said hollow main shaft having a solid end portion of a reduced diameter, two wedge-like vanes fixedly attached to either side of said hollow shaft by means of rods and defining with said hollow shaft, said tubular rotor, said tapering vanes and said first and second end plates, four chambers, at least one shaft unit which rotates in bearings mounted in said second end plate and said support ring respectively, each shaft unit having attached thereto or integral therewith, an eccentric or a crank-like section, and a planet gear, at least one connecting rod having a big end and a small end, the big end being associated with said eccentrics and the small end being associated via pivots with a rocker arm pinned to said reduced main shaft end, wherein rotation of said drive shaft at a uniform speed causes said rotor, including said tapering vanes, to be rotated at the same uniform speed, while an oscillatory motion is superposed on said hollow shaft and said wedge-like vanes, whereby the volume of said four chambers is made to successively vary between a minimum and a maximum.
The invention will now be described in connection with certain preferred embodiments with reference to the following illustrative figures, so that it may be more fully understood. With specific reference now to the figures in detail, it is stressed that the particulars shown are by way of example and for purposes of illustrative discussion of the preferred embodiments of the present invention only, and are presented in the cause of providing what is believed to be the most useful and readily understood description of the principles and conceptual aspects of the invention. In this regard, no attempt is made to show structural details of the invention in more detail than is necessary for a fundamental understanding of the invention, the description taken with the drawings making apparent to those skilled in the art how the several forms of the invention may be embodied in practice.
In the drawings:
Referring now to the drawings, there is seen in
Tubular rotor 10 includes two tapering vanes 11 (seen to better advantage in
End plate 14 is fixedly attached to rotor 10 or vanes 11 by per-se known fastening means (not shown).
Drive shaft 15 is fixedly attached to end plate 14 through pin 16. Electric motor 17 mounted on shaft 15 is supported by bearings 18 and 19.
End plate 21 is provided with two projections 22 and is fixedly attached to rotor 10 and/or vanes 11 by known fastening means (not shown).
Support plate 23, seen to better advantage in
Tapering vanes 11 and flat vanes 36 define between them and the inside of rotor 10 four chambers Ch1, Ch2, Ch3 and Ch4 (see
In
Further seen are two connecting rods 45, the big end of which is connected via bearings 46 to each of the eccentrics 42, and the small end of each of which is connected via bearings 47 and pivot 48 to rocker arm unit 49, the sleeve 50 is pinned by means of pin 51 to the solid, reduced-diameter part of oscillating shaft 29 (see also
Eccentrics 42 could also be replaced by a per-se known crank design.
In
The HADMI RVM described in detail in the aforegoing functions as follows:
Electric motor 17 drives drive shaft 15, end plate 14, tubular rotor 10 including tapering vanes 11, end plate 21 and support ring 23 at uniform speed. Two shaft units 39 disposed symmetrically relative to the RVM axis also rotate at that uniform speed. Integral with shaft units 39 are planet gears 43 meshing with stationary sun gear 7 and forcing shaft unit 39 to rotate also about their own axes at a speed that is twice as large as the speed of the RVM. Integral with shaft units 39, two eccentrics 42, via connecting rods 45, rock rocker arm unit 49, thus, via shaft end 50 superposing an oscillatory motion on hollow shaft 29, causing the latter to force flat vanes 36, which rotate together with the above RVM components, to simultaneously rock between the two tapering vanes 11 and to change the respective volumes of working chambers Ch1, Ch2, Ch3 and Ch4.
If in
Another embodiment of the RVM according to the present invention is illustrated in
There is seen in
Also seen in
While the oscillating vanes 36 of the first embodiment are substantially flat, vanes 96 of the present embodiment are wedge-shaped, as can be seen in
Further seen in
It will be appreciated that as opposed to the first embodiment of the invention, the present embodiment provides no ports in rotor 78, all ports being located in end plate 80 (
All unnumbered parts are identical to the parts having identical functions in the first embodiment.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrated embodiments and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein.
Number | Date | Country | Kind |
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176534 | Jun 2006 | IL | national |
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3169487 | Namikawa | Feb 1965 | A |
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4169697 | Doundoulakis | Oct 1979 | A |
4257752 | Fogarty | Mar 1981 | A |
5366356 | Volftsun | Nov 1994 | A |
6113370 | Volftsun | Sep 2000 | A |
6210135 | Rassin et al. | Apr 2001 | B1 |
6321693 | Kim et al. | Nov 2001 | B1 |
Number | Date | Country | |
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20070297928 A1 | Dec 2007 | US |