Claims
- 1. A method of forming an internal helical auger for a rotary retort furnace comprising, forming a number of toroids from a resilient material, making a radial cut in each of said toroids, slightly deforming each of said radially cut toroids to form a single flight of a helix, fastening one of the edges of each of said flights resulting from said radial cut to an opposite edge of another of said flights resulting from said radial cut to form a helix subassembly, said subassembly having a free edge of a flight resulting from said radial cut at each end, axially expanding while radially compressing said subassembly by screwing said subassembly onto a shaft having a number of guide pins at preselected intervals, inserting said subassembly and said shaft into a cylindrical retort member of a predetermined length, fastening one of said free ends of said subassembly to the one end of said retort, removing said shaft by unscrewing it from the subassembly while forcing the shaft and the subassembly axially into the retort member permitting and urging said resilient subassembly to radially expand into contact with the inside walls of said retort member, and upon removal of said shaft securing the other of said free ends of said subassembly to the other end of said retort.
- 2. A method of manufacturing a rotary retort having an internal helical auger flight comprising making a cylindrical retort member having a predetermined inside diameter and a predetermined length, forming an axially compressed helical subassembly having an outside diameter greater than said inside diameter of said retort, axially expanding while radially contracting said subassembly by screwing said subassembly onto a shaft having guide pins set at preselected distances along the axis of said shaft, inserting said subassembly and shaft into said retort, securing one end of said subassembly to one end of said retort, removing said shaft from said subassembly and retort by unscrewing it from said subassembly, forcing said shaft and subassembly axially into said retort by impact while unscrewing said shaft from said subassembly, securing the other end of said subassembly to the other end of said retort upon removal of said shaft.
- 3. A method of making a rotary retort having an internal auger flight as defined in claim 2 wherein said retort is preheated to a temperature of approximately 200.degree. to 300.degree. F. to expand the said inside diameter prior to inserting said subassembly and said shaft into said retort.
Parent Case Info
This is a division of application Ser. No. 615,281, filed Sept. 22, 1975, now U.S. Pat. No. 4,025,297.
US Referenced Citations (3)
Divisions (1)
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Number |
Date |
Country |
Parent |
615281 |
Sep 1975 |
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