Claims
- 1. A method of manufacturing a switch comprising the steps of:
- (a) assembling a pair of stator support plates and spaced parallel phase barrier separation plates to form a slip-in unit defining a plurality of volumes for receiving an electrically insulating gas, each of said phase barrier separation plates having a central opening with all of said central openings being axially aligned in said slip-in unit;
- (b) installing into the assembly of step (a) a rotary shaft extending through the aligned central openings of said phase barrier separation plates;
- (c) mounting a movable contact and an impeller blade having a nozzle thereon onto said rotary shaft with orientations which determine combinations and sequences of contact operations, there being at least one contact and one impeller blade between each pair of said phase barrier separation plates, said nozzle being directed toward said contact;
- (d) slipping said assembly of steps (a)-(c) into a cylindrical shell, the dimensions of said parts being such that operation of said rotor shaft compresses an insulating gas in front of said impeller blade from which gas escapes through said nozzle; and
- (e) mounting stationary contacts through said shell and at a point in a path followed by said movable contacts, said point being located to receive said compressed gas escaping through said nozzle, said escaping gas striking an extended region in which an, arc might form when said contacts open.
- 2. The method of claim 1 and the added step of making parts which become hot during operation from thermosetting plastic and of making parts which do not become hot during operation from thermoplastic material.
- 3. The method of claim 1 and the added steps of making at least some of said parts from notched plastic whereby said assembly of at least step (a) can be completed by slipping notches on one of said parts into notches on other of said parts.
- 4. A method of manufacturing a rotary puffer switch assembly comprising the steps of:
- forming a hollow cylindrical shell;
- forming a rotor assembly adapted to be rotatably received within the interior of said shell, said rotor assembly comprising a rotary shaft and at least two phase barrier plates mounted on said rotary shaft perpendicularly thereto and in spaced relation to each other;
- installing at least one stationary contact means in the interior of said shell between said phase barrier plates;
- mounting at least one movable contact on said rotary shaft between said phase barrier plates in a location to move into electrical contact with said stationary contact means when said rotor assembly is received and rotated within said interior of said shell;
- mounting on said rotary shaft adjacent said movable contact a gas impeller blade and gas nozzle assembly adapted to force a flow of any gas contained in said hollow shell across any arc created between said movable contact and said stationary contact when said rotary shaft is rotated;
- and inserting said rotor assembly, with said movable contact and said gas impeller blade and gas nozzle assembly mounted thereon, into said hollow interior of said shell in such manner that said rotor assembly may be rotated relative to said shell to move said movable contact into and out of electrical contact with said stationary contact means and simultaneously to cause said gas impeller blade and gas nozzle assembly to force said flow of gas.
- 5. The method of claim 4 wherein said step of forming said rotor assembly comprises the steps of:
- forming said phase barrier plates with central openings adapted to receive said rotary shaft; and
- inserting said rotary shaft through said central openings in said phase barrier plates.
- 6. The method of claim 5 wherein said step of forming said rotor assembly comprises the steps of:
- forming each of said phase barrier plates with at least one notch;
- forming at least one support plate adapted to be received by said notch in each of said phase barrier plates; and
- inserting at least a portion of said support plate into said notch in each of said phase barrier plates to support said phase barrier plates in spaced relation to one another.
- 7. The method of claim 6 wherein said step of forming said rotor assembly comprises the steps of:
- forming said support plate with a plurality of notches, said notches in the support plate corresponding to respective notches formed in said phase barrier plates so that said notches in said support plate interfit with respective notches in said phase barrier plates.
- 8. The method of claim 4 wherein said step of mounting at least one movable contact on said rotary shaft comprises the steps of:
- forming said rotary shaft with an aperture adapted to receive said movable contact; and
- inserting at least a portion of said movable contact through said aperture in said rotary shaft.
- 9. The method of claim 4 wherein said step of mounting said gas impeller blade and gas nozzle assembly on said rotary shaft comprises the steps of:
- forming said assembly with at least one appendage;
- forming said rotary shaft with at least one slot adapted to receive and appendage; and
- inserting at least a portion of said appendage through said slot on said rotary shaft.
- 10. The method of claim 9 wherein said step of mounting said gas impeller blade and gas nozzle assembly on said rotary shaft comprises the steps of:
- forming said gas impeller blade and gas nozzle assembly with a pair of spaced substantially parallel baffle plates mounted on said assembly substantially perpendicularly thereto and defining said gas nozzle between said baffle plates.
- 11. The method of claim 10 wherein the step of forming said pair of baffle plates comprises the step of locating said baffle plates on said impeller blade in such a manner that said baffle plates extend asymmetrically from said assembly.
- 12. The method of claim 4 wherein said step of installing at least one stationary contact in the interior of said shell comprises the steps of:
- forming said hollow cylindrical shell with at least one aperture adapted to receive said stationary contact; and
- inserting at least a portion of said stationary contact through said aperture in said cylindrical shell.
- 13. The method of claim 4 wherein said step of installing at least one stationary contact in the interior of said shell includes the step of forming means on said hollow cylindrical shell for thermally protecting said shell from said stationary contact.
- 14. The method of claim 13 wherein said step of forming thermal protecting means on said shell includes the step of forming said thermal protecting means from a thermosetting material.
- 15. The method of claim 4 wherein said step of mounting at least one movable contact on said rotary shaft includes the step of forming means on said rotary shaft for thermally protecting said rotary shaft from said movable contact.
- 16. The method of claim 15 wherein said step of forming thermal protecting means on said rotary shaft includes the step of forming said thermal protecting means from a thermosetting material.
- 17. The method of claim 4 wherein said step of installing said stationary contact comprises the step of forming said stationary contact with a gap adapted to receive and securely grip said moving contact.
- 18. The method of claim 17 wherein said step of forming said stationary contact includes the step of forming said gap with an angled chute for receiving said moving contact.
- 19. The method of claim 4 wherein said step of installing said stationary contact in the interior of said shell comprises the step of forming said stationary contact from a plurality of laminated conductive plates.
- 20. The method of claim 19 wherein said step of installing said stationary contact in the interior of said shell comprises the step of forming means in association with said stationary contact for limiting flexure along at least a portion of said stationary contact.
- 21. The method of claim 4 wherein said step of mounting at least one movable contact on said rotary shaft comprises the step of forming said movable contact from a body of conductive material having a generally blade-like shape.
- 22. The method of claim 21 wherein the step of mounting said movable contact on said rotary shaft comprises the step of forming said movable contact with a tapered profile along at least a portion thereof for engaging said stationary contact.
- 23. The method of claim 4 wherein the steps of mounting said movable contact on said rotary shaft and installing said stationary contact in the interior of said shell comprise the steps of forming said movable contact and stationary contact each with a contact region for applying mechanical force against one another in such a manner that said mechanical force is substantially equally distributed throughout said contact regions.
- 24. A method of manufacturing a rotary puffer switch assembly comprising the steps of:
- forming a hollow cylindrical shell;
- forming a rotor assembly adapted to be rotatably received within the interior of said shell, said rotary assembly comprising a rotary shaft and at least two phase barrier plates mounted on said rotary shaft substantially perpendicular thereto and in spaced relation to each other;
- installing at least two stationary contact means in the interior of said shell between said phase barrier plates;
- mounting at least two movable contacts on said rotary shaft between said phase barrier plates in positions to be operatively associated with respective ones of said stationary contacts to cause said movable contacts to move into simultaneous electrical contact with said stationary contacts when said rotor assembly is received and rotated within the interior of said shell;
- mounting on said rotary shaft a pair of gas impeller blade and gas nozzle assemblies, and positioning said assemblies adjacent respective ones of said movable contacts whereby to force a flow of any gas contained in said hollow shell across any arc created between any pair of said movable contacts and said stationary contacts; and
- inserting said rotor assembly, with said movable contacts and said gas impeller blade and gas nozzle assemblies mounted thereon, into said hollow interior of said shell in such manner that said rotor assembly may be rotated relative to said shell to move said movable contacts into and out of contact with said stationary contact means and simultaneously to cause said gas impeller blade and gas nozzle assemblies to force said flow of gas.
- 25. The method of claim 14 wherein said step of mounting said pair of gas impeller blade and nozzle assemblies on said rotary shaft comprises the step of forming said assemblies in such a manner that they must be aligned in a selected orientation in order to be mounted properly on said rotary shaft.
- 26. The method of claim 25 wherein said step of mounting said pair of gas impeller blade and nozzle assemblies on said rotary shaft comprises the steps of:
- forming each of said gas impeller blade and nozzle assemblies with at least one appendage;
- forming said rotary shaft with slots adapted to receive said appendages; and
- inserting at least a portion of each of said appendages through one of said slots on said rotary shaft.
- 27. The method of claim 26 wherein said step of mounting said pair of gas impeller blade and nozzle assemblies on said rotary shaft comprises the steps of:
- forming said appendages and said slots with complementary shapes that permit insertion of said appendages through said slots only when said appendages are aligned in a selected orientation.
Parent Case Info
This application is a division of prior application Ser. No. 07/606,332, filed Nov. 6, 1990 now U.S. Pat. No. 5,153,399.
US Referenced Citations (9)
Foreign Referenced Citations (1)
Number |
Date |
Country |
0171352 |
Feb 1986 |
EPX |
Non-Patent Literature Citations (1)
Entry |
Siemens 8DJ10 Ring Main Units--Catalog HA 45.1-1986. |
Divisions (1)
|
Number |
Date |
Country |
Parent |
606332 |
Nov 1990 |
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