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US3787944A Expired / Lapsed US ⏱️ 0.0 years remaining

Method of assembling a gas turbine regenerator assembly

Assignee: Ford Motor Co
•
Filing: 1972-11-08
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Granted: 1974-01-29
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Expires: 1992-11-08
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Abstract

Abstract Assembly method for a gas turbine regenerator assembly are described. The regenerator assembly comprises a cylindrical regenerator core, an annular drive member surrounding the cylindrical surface of the regenerator core and separated from it to define an annular space, and a resilient material positioned in the annular space between the drive member and regenerator core. A mounting ring is also located in the annular space. The mounting ring has a discontinuity in it which permits its diameter to be varied to compress the resilient material during assembly. The assembly method includes the steps of surrounding the cylindrical surface of the regenerator core with the resilient material, placing the annular mounting ring around the resilient material and regenerator core, applying forces to the mounting ring to reduce its diameter, positioning the drive member around the mounting ring, and reducing the previously applied forces to permit the mounting ring diameter to increase.

Inventors

  • 👤 J Mittman

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-25 19:37
CPC Classifications
F; F28; F28D; F28D19/00; F28D19/04; F28D19/048; Y; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/4935; Y10T29/49357; Y10T29/49826; Y10T29/49863; Y10T29/4987; Y10T29/49872

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 118 words
A method for assembling a gas turbine regenerator assembly, said assembly comprising a cylindrical regenerator core, an annular drive member, and a resilient material positioned between said drive member and said regenerator core, said method including the steps of: surrounding the cylindrical surface of said regenerator core with said resilient material; placing an annular mounting ring, said mounting ring having a discontinuity to permit its diameter to be varied, around said resilient material and regenerator core; applying forces to said mounting ring to reduce its diameter and simultaneously to compress said resilient material; positioning said drive member around said mounting ring; and reducing the forces previously applied to said mounting ring, thereby, to permit its diameter to increase.
Claim 2
Independent Claim 118 words
A method for assembling a gas turbine regenerator assembly, said assembly comprising a cylindrical regenerator core, an annular drive member, and a resilient material positioned between said drive member and said regenerator core, said method including the steps of: surrounding the cylindrical surface of said regenerator core with said resilient material; placing an annular mounting ring, said mounting ring having a discontinuity to permit its diameter to be varied, around said resilient material and regenerator core; applying forces to said mounting ring to reduce its diameter and simultaneously to compress said resilient material; positioning said drive member around said mounting ring; and reducing the forces previously applied to said mounting ring, thereby, to permit its diameter to increase.
Claim 3
Dependent Claim 61 words
A method in accordance with claim 1, which includes the additional steps of applying a force to said drive member and to said resilient material and regenerator core in an axial direction, and withdrawing said mounting ring in a direction axially opposite to the direction of said force applied to said drive member and to said resilient material and regenerator core.
Claim 4
Dependent Claim 34 words
A method in accordance with claim 1, wherein said annular mounting ring has at least one axially extending tab, said method including the additional step of bending said tab to a radially extending position.

References Cited (Backward Citations)

US2060565A Cited
US2272900A Cited
US2325132A Cited
US2689397A Cited
US3342530A Cited
US3525384A Cited
US3688835A Cited
US3666000A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1977-01-28 1977-07-30 1978-01-29 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1981-01-28 1981-07-30 1982-01-29 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1985-01-28 1985-07-30 1986-01-29 $7700.00 Window Closed / Lapsed

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