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Method of correcting a number of revolution of a screw propeller

Assignee: Kawasaki Heavy Industries Ltd
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Filing: 1970-10-15
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Granted: 1972-12-05
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Expires: 1990-10-15
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Abstract

Abstract A method of adjusting the number of revolutions of a screw propeller having the steps of cutting the trailing edge of each blade of the propeller from and along the trailing edge, and working and shaping the face of the blade to a curvature to provide a proper setback.

Inventors

  • 👤 Hiroshi Okamoto

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-23 11:35
CPC Classifications
B; B63; B63H; B63H1/00; B63H1/02; B63H1/12; B63H1/14; B63H1/26; Y; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/49316; Y10T29/49332; Y10T29/49718; Y10T29/49748

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 127 words
A method of adjusting the number of revolutions of a used, fixed pitch screw propeller of an ocean going marine vessel without removing the same from said vessel, said method comprising the steps of: smoothly reducing the trailing edge only of each blade of the propeller, a predetermined amount, the maximum extent of reduction of said trailing edge at any one point along said edge being, in terms of blade width, between 0.7 to 0.9 percent, and working and shaping the face of the blade along said trailing edge to a predetermined curvature providing a setback from the trailing edge of which the maximum extent of the same at any one point along said trailing edge, in terms of blade length, is between 0.6 to 0.7 percent.
Claim 2
Independent Claim 127 words
A method of adjusting the number of revolutions of a used, fixed pitch screw propeller of an ocean going marine vessel without removing the same from said vessel, said method comprising the steps of: smoothly reducing the trailing edge only of each blade of the propeller, a predetermined amount, the maximum extent of reduction of said trailing edge at any one point along said edge being, in terms of blade width, between 0.7 to 0.9 percent, and working and shaping the face of the blade along said trailing edge to a predetermined curvature providing a setback from the trailing edge of which the maximum extent of the same at any one point along said trailing edge, in terms of blade length, is between 0.6 to 0.7 percent.

References Cited (Backward Citations)

US18853A Cited
US1882164A Cited
US2450383A Cited
US3002266A Cited
US3295190A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1975-12-05 1976-06-05 1976-12-05 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1979-12-05 1980-06-05 1980-12-05 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1983-12-05 1984-06-05 1984-12-05 $7700.00 Window Closed / Lapsed

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