This invention concerns rotor assemblies for devices such as compressors, pumps and rotary engines.
Rotor and vane assemblies, wherein a vane reciprocates transversely to an axis of rotation of a rotor as the rotor turns, find extensive use in devices such as pumps, compressors and rotary engines. The rotor and vane assembly rotates within a housing and the vane engages a sidewall of the housing which is eccentric to the axis of rotation of the rotor. This eccentric configuration allows the rotor assembly to pump liquids, compress gases, or derive power from combustion of fuel though a thermodynamic cycle.
Advantages, such as lighter weight, lower pressure forces and reduced dead space remainder volume may be obtained by making the vanes as thin as possible. However, one of the design constraints which limits the thickness of a vane is the design of the engagement between the vane and the eccentric cam arrangement which enables the vane's reciprocal motion. There is clearly an opportunity to improve the operation of rotor assemblies by improving the engagement between the vane and cam in a rotor and vane assembly.
The invention concerns a vane adapted for use with a rotor. In one example embodiment the vane comprises a plate. A slot extends transversely to one edge of the plate. The slot is defined by first and second oppositely disposed edges and a third edge oriented transversely to the first and second edges. An insert is removably mounted within the slot. By way of example the insert comprises a base engageable with the third edge of the slot. A first leg projects transversely to the base and is engageable with the first edge of the slot. A second leg projects transversely to the base and is engageable with the second edge of the slot.
In an example embodiment the vane may further comprise a fastener extending between the base and the third edge for removably securing the insert to the plate.
In another example embodiment the insert further comprises a first groove extending lengthwise along the first leg. The first groove is adapted to receive the first edge of the slot. By way of further example a second groove extends lengthwise along the second leg. The second groove is adapted to receive the second edge of the slot.
In an example embodiment the insert is “U” shaped. Further by way of example, a first support surface is positioned on the first leg. Also by way of example, a second support surface is positioned on the second leg. The first and second support surfaces are in facing relation with one another. In an example embodiment the first and second support surfaces have a width wider than a thickness of the plate.
The invention also encompasses a rotor and vane assembly engageable with an eccentric cam block. In an example embodiment, the rotor comprises a first hub. A second hub is coaxially aligned with the first hub. A vane housing is positioned between the first and second hubs. The vane housing comprises a cylindrical body having a longitudinal axis coaxially aligned with the first and second hubs. A slot extends through a diameter of the body and along the longitudinal axis. A shaft extends from the second hub and is coaxially aligned therewith. The vane is slidably positioned within the slot. IN an example embodiment the vane comprises a plate. A slot extends transversely to one edge of the plate. The slot is defined by first and second oppositely disposed edges and a third edge oriented transversely to the first and second edges. An insert is removably mounted within the slot. The insert is adapted to receive the eccentric cam block. In an example embodiment the insert comprises a base engageable with the third edge of the slot. A first leg projects transversely to the base and is engageable with the first edge of the slot. A second leg projects transversely to the base and is engageable with the second edge of the slot.
An example embodiment further comprises a fastener extending between the base and the third edge for removably securing the insert to the plate. In another example embodiment the insert comprises a first groove extending lengthwise along the first leg. The first groove is adapted to receive the first edge of the slot. By way of further example, a second groove extends lengthwise along the second leg. The second groove is adapted to receive the second edge of the slot.
In an example embodiment the insert is “U” shaped.
An example insert embodiment may further comprise a first support surface positioned on the first leg. A second support surface may also be positioned on the second leg. The first and second support surfaces are in facing relation with one another. In an example embodiment the first and second support surfaces have a thickness wider than a thickness of the plate.
A vane housing 26 is positioned between the first and second hubs 14 and 20. Vane housing 26 comprises a cylindrical body 28 having a longitudinal axis 30 coaxially aligned with the first and second hubs 14 and 20 and the rotor axis of rotation 22. A slot 32 extends through a diameter 34 of the body 28. Slot 32 also extends lengthwise along the longitudinal axis 30 of the body 28. A vane 36 is slidably positioned within the slot 32.
It is advantageous if insert 50 is removably mounted within the slot 40 on the plate 38 because it permits assembly of the rotor 12 and vane 36 when the rotor 12 is formed from a single billet or casting. As shown in
In the example embodiment shown in
In operation, vane 36 reciprocates within the slot 32 of the vane housing 26 as the rotor 12 rotates about its axis 22. This reciprocal motion is effected by coupling the vane 36 to a cam block 66 (see
This application is based upon and claims benefit of priority to U.S. Provisional Application No. 62/525,254, filed Jun. 27, 2017 and hereby incorporated by reference.
Number | Name | Date | Kind |
---|---|---|---|
3158103 | Eickmann | Nov 1964 | A |
3398884 | Kaatz | Aug 1968 | A |
20140112817 | Osaki | Apr 2014 | A1 |
20190017507 | Heaps | Jan 2019 | A1 |
Number | Date | Country |
---|---|---|
533897 | Mar 1922 | FR |
57059091 | Apr 1982 | JP |
9904141 | Jan 1999 | WO |
Number | Date | Country | |
---|---|---|---|
20180371913 A1 | Dec 2018 | US |
Number | Date | Country | |
---|---|---|---|
62525254 | Jun 2017 | US |