US736952A - Screw-propeller. - Google Patents

Screw-propeller. Download PDF

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Publication number
US736952A
US736952A US13825303A US1903138253A US736952A US 736952 A US736952 A US 736952A US 13825303 A US13825303 A US 13825303A US 1903138253 A US1903138253 A US 1903138253A US 736952 A US736952 A US 736952A
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Prior art keywords
propeller
blades
screw
blade
hub
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Expired - Lifetime
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US13825303A
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Edward Fox
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Priority to US13825303A priority Critical patent/US736952A/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/16Blades
    • B64C11/20Constructional features
    • B64C11/24Hollow blades
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S415/00Rotary kinetic fluid motors or pumps
    • Y10S415/914Device to control boundary layer

Definitions

  • n-u dams PETERS c0. Pnu'raLlTna. WASHINGTQN, n, c.
  • FIG. 1 is a rear elevation of a propeller constructed in accordance with myinvention
  • Fig. 2 a horizontal section taken in the plane indicated by the line 2 20f Fig. 1
  • Fig. 3 a detail front elevation illustrating one of the blades of the propeller and a modification.
  • A is the hub of my improved propeller, and B B the blades.
  • B B the blades.
  • I desire it distinctly understood that I do not limit myself to any number of blades on the propeller or toany certain pitch of screw or to forming the blades integral with the hub, as shown in Figs. 1 and 2.
  • the blades may be bolted, Fig. 3, or otherwise secured to the boss or hub on propeller-shaft, so as to permit of their disconnection from said boss or hubwhen necessary.
  • the blades are each provided with a passage 0. These passages are similar, and therefore a detailed description of the one shown in Fig. 3 will suffice to impart a clear understanding of all.
  • Said passage 0 has its receiving end (indicated by a) disposed in the forward edge of the blade, with reference to the direction in which the propeller is rotated to drive a vessel forward, at a point adjacent to the hub A, and from said point a it extends in the direction of the I accomplish length of the blade and across the same to the point b,where it terminatesin a discharge formed in the forward side of the blade adjacent to the rear edge and the outer end of the same.
  • the discharge 1) is disposed at an approximate obtuse angle to the intermediate portion 0 of the passage, as best shown in Fig. 2, and hence is enabled when the propeller is rotatedin the direction indicated by the large arrow in Fig. 1 to throw a solid stream of water outwardly-71. e., toward the outer end of the succeeding blade and forwardly against the rear face of said bladeafter the manner shown by arrows in Fig. 2,
  • a screw-propeller comprising a hub,and a plurality of blades, pitched at an angle to the longitudinal median line of the hub each of the said blades being provided with apassage which extends from the forward edge of the blade, with reference to the direction in which the propeller is rotated to drive a vessel forward, at a point adjacent to the hub, and in the direction of the length of the blade across the same, and terminates in a discharge 1) formed in the forward side of the blade adjacent to the rear edge and outer end of the same, and disposed at an obtuse angle to the intermediate portion of the passage;
  • a screw-propeller the combination of a boss or hub, and one or more blades detachably connected thereto; each of the said blades being provided with a passage which extends from the forward edge of the blade, with reference to the direction in which the EDWARD FOX.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Description

No. 736,952. PATENTED AUG. 25, 1903.
E. FOX. I SCREW PROPELLER.
APPLICATION FILED JAN. 8, 1903.
H0 MODEL.
WWW '1 I amen ton /M 42. 'W
n-u: dams PETERS c0. Pnu'raLlTna. WASHINGTQN, n, c.
UNITED STATES Patented August 25, 1903.
PATENT OFFICE.
EDWARD FOX, OF BROOKLYN, NEW YORK, ASSIGNOR OF ONE-HALF TO WILLIAM LOGAN, OF ARLINGTON, NEW JERSEY.
SC REW-PROPELLER.
SPECIFICATION forming part of Letters Patent No. 736,952, dated August 25, 1903.. Application filed January 8, 1903. Serial No. 138,253. (No model.)
To all whom it may concern/.-
Be it known that I, EDWARD FOX, a citizen of the United States, residing at Brooklyn, in the county of Kings and State of New York, have invented certain new and useful Improvements in Screw-Propellers; and I do' blades of the screw by the centrifugal action of the revolving screw through the water.
With the foregoing in mind the invention will be fully understood from the following description and claims when taken in connection with the accompanying drawings, in which- Figure 1 is a rear elevation of a propeller constructed in accordance with myinvention; Fig. 2, a horizontal section taken in the plane indicated by the line 2 20f Fig. 1, and Fig. 3 a detail front elevation illustrating one of the blades of the propeller and a modification.
Referring by letter to the drawings, A is the hub of my improved propeller, and B B the blades. I desire it distinctly understood that I do not limit myself to any number of blades on the propeller or toany certain pitch of screw or to forming the blades integral with the hub, as shown in Figs. 1 and 2. In screw-propellers of large diameter the blades may be bolted, Fig. 3, or otherwise secured to the boss or hub on propeller-shaft, so as to permit of their disconnection from said boss or hubwhen necessary. The blades are each provided with a passage 0. These passages are similar, and therefore a detailed description of the one shown in Fig. 3 will suffice to impart a clear understanding of all. Said passage 0 has its receiving end (indicated by a) disposed in the forward edge of the blade, with reference to the direction in which the propeller is rotated to drive a vessel forward, at a point adjacent to the hub A, and from said point a it extends in the direction of the I accomplish length of the blade and across the same to the point b,where it terminatesin a discharge formed in the forward side of the blade adjacent to the rear edge and the outer end of the same. The discharge 1) is disposed at an approximate obtuse angle to the intermediate portion 0 of the passage, as best shown in Fig. 2, and hence is enabled when the propeller is rotatedin the direction indicated by the large arrow in Fig. 1 to throw a solid stream of water outwardly-71. e., toward the outer end of the succeeding blade and forwardly against the rear face of said bladeafter the manner shown by arrows in Fig. 2,
In the practical use of my improved propeller the same is rotated in the direction indicated by the large arrow in Fig. 1 in order to move a Vessel forwardly. In virtue of each of the blades of the propeller being provided with a passage 0 it will be observed that when the propeller is rotated as stated solid streams of water will be caused to take through the passages (see arrows in Fig. 1) and will be forcibly projected rearwardly and outwardly against the rear faces of the several blades. From this it follows that the ordinary tendency of the water to follow the blades and cause slip is overcome, also that a dense body of water is always present at the rear face of each blade, and in consequence the purchase and thrust of the blades is materially increased,as is also the efficiency of the propeller as a whole.
I am well aware that it is old, as shown in German Patent No. 17,146, to provide each blade of a screw-propeller with a passage which-extends from one edge of the blade at a point adjacent to the hub to the opposite edge of the blade at a point adjacent. to the outer end thereof and is adapted to discharge a stream of Water rearwardly parallel to the axis of the hub. I therefore make no claim to such construction.
What I claim, and desire to secure by Letters Patent, is
1. A screw-propeller comprising a hub,and a plurality of blades, pitched at an angle to the longitudinal median line of the hub each of the said blades being provided with apassage which extends from the forward edge of the blade, with reference to the direction in which the propeller is rotated to drive a vessel forward, at a point adjacent to the hub, and in the direction of the length of the blade across the same, and terminates in a discharge 1) formed in the forward side of the blade adjacent to the rear edge and outer end of the same, and disposed at an obtuse angle to the intermediate portion of the passage;
whereby it is adapted to discharge a stream of water against the rear face of the following blade.
2. In a screw-propeller, the combination of a boss or hub, and one or more blades detachably connected thereto; each of the said blades being provided with a passage which extends from the forward edge of the blade, with reference to the direction in which the EDWARD FOX.
Witnesses:
JOHN F. CoWEN, MARY B. LETTENBERGER.
US13825303A 1903-01-08 1903-01-08 Screw-propeller. Expired - Lifetime US736952A (en)

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Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2511156A (en) * 1946-08-07 1950-06-13 Richard J Glass Propeller
US2935245A (en) * 1956-12-10 1960-05-03 Westinghouse Electric Corp Gas reaction rotors
US3050282A (en) * 1958-04-03 1962-08-21 Gen Electric Turbine speed limiting arrangement
US3109499A (en) * 1961-05-29 1963-11-05 Klein Fritz Aircraft propeller with centrifugally induced air flow control features
US3385374A (en) * 1967-01-23 1968-05-28 Oceanics Inc Marine propeller
US3405865A (en) * 1966-10-18 1968-10-15 Lagelbauer Ernest Turbofan bladings
WO1992001911A1 (en) * 1990-07-20 1992-02-06 Sundstrand Data Control, Inc. Temperature transducer
US20030175120A1 (en) * 2002-03-12 2003-09-18 St. Clair Alexander Sasha Aqua / atmos propellor jet
US20220340258A1 (en) * 2021-04-26 2022-10-27 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Aircraft propeller and aircraft

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2511156A (en) * 1946-08-07 1950-06-13 Richard J Glass Propeller
US2935245A (en) * 1956-12-10 1960-05-03 Westinghouse Electric Corp Gas reaction rotors
US3050282A (en) * 1958-04-03 1962-08-21 Gen Electric Turbine speed limiting arrangement
US3109499A (en) * 1961-05-29 1963-11-05 Klein Fritz Aircraft propeller with centrifugally induced air flow control features
US3405865A (en) * 1966-10-18 1968-10-15 Lagelbauer Ernest Turbofan bladings
US3385374A (en) * 1967-01-23 1968-05-28 Oceanics Inc Marine propeller
WO1992001911A1 (en) * 1990-07-20 1992-02-06 Sundstrand Data Control, Inc. Temperature transducer
US5135312A (en) * 1990-07-20 1992-08-04 Sundstrand Data Control, Inc. Temperature transducer
US20030175120A1 (en) * 2002-03-12 2003-09-18 St. Clair Alexander Sasha Aqua / atmos propellor jet
US20220340258A1 (en) * 2021-04-26 2022-10-27 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Aircraft propeller and aircraft
US11679863B2 (en) * 2021-04-26 2023-06-20 Dr. Ing. H.C. F. Porsche Aktiengesellschaft Aircraft propeller and aircraft

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