US855131A - Screw-propeller. - Google Patents

Screw-propeller. Download PDF

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Publication number
US855131A
US855131A US29039305A US1905290393A US855131A US 855131 A US855131 A US 855131A US 29039305 A US29039305 A US 29039305A US 1905290393 A US1905290393 A US 1905290393A US 855131 A US855131 A US 855131A
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United States
Prior art keywords
propeller
blades
ring
screw
tips
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Expired - Lifetime
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US29039305A
Inventor
Wenzel Preidel
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Individual
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Priority to US29039305A priority Critical patent/US855131A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D3/00Axial-flow pumps
    • F04D3/005Axial-flow pumps with a conventional single stage rotor

Definitions

  • This invention relates to im rovements in screw propellers, the object eing to so construct the same that lateral slip between the propeller and the medium in which it rotates is obviated.
  • I provide a cylindrical, conical or similar ring around the outside of the pro eller, the tips of the blades being connecte to the inner surface of the said ring, the axis of which is coinci dent with that of the propeller boss; ring may be continuous, or it may be broken at one ormore points, in which case it isin the form of a number of segments attached to the tips of the propeller blades.
  • the ring is open at both sides and those portions between the adj acentblades are recessed or cut away at one side, the recesses extending to say about the center of the boss of the propeller.
  • Figure 1 is a side elevation of a ropeller *ig. 2 is a section on the line 2-2, Fig. 1.
  • Fig. 3 is a plan view thereof.
  • Fig. 4 is a development of a art of the ring.
  • Fig. 5 is a view similar to Fig. 3 illustrating a modification, and
  • Fig. 6 is a lan view thereof.
  • ring 0 is the ring which is provided around the outside of the propeller and the axis of which is coincident with that of the boss a.
  • the ring 0 is continuous and the tips of the blades 1), b are connected to its inner surface as clearly shown, the inner or inside end of the said ring being cut away so as to form the recesses d, d between the propeller blades b, b;
  • the water (or air) in which the propeller is revolving is forced through the ring more or less like a solid column in a direction opposite to that in which the vessel to which the propeller is attached is to move, thus obviati'ng lateral slip from the propeller blades.
  • the ring made'in two parts, e and f, the portion 6 being composed of segments forming the recesses d, d and attached to the tips of the propeller blades b and the portion f being fixed so as not to rotate with the propeller, that is to say, being secured in place by means of the stays g to the rear of the vessel.
  • a discontinuous ring that is to say, of a number of segments which are attached to the tips of the propeller blades. I prefer, however, to use a continuous ring as above described.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Mixers Of The Rotary Stirring Type (AREA)

Description

PATENTED MAY 28, 1907. W. PREIDEL. V
SCREW PROPELLER.
APPLICATION FILED DEO.5.1905.
2 SHEETS-SHEET 1'.
W. PREIDEL.
SCREW PROPBLLBR. APPLICATION FILED 13110.5.1905.
2 SHEETS-SHEET 2. 1 2 5 g Y PATBNTED MAY 28, 1907.
'made according to my invention.
UNITED STATES PATENT OFFIOE.
SCHEW-PROPELLER.
Specification of Letters Patent.
Patented May 28, 1907.
Application filed December 5, 1905. Serial No. 290,393.
To all whom it may concern.-
Be it known that I, WENZEL PREIDEL, a subject of the Emperor of Austria, residing at 4 Magdalen Parade, Garratt Lane, Earlsfield, London, England, have invented new and useful Im rovements in Screw-Propellers of which the fbllowing is a specification.
This invention relates to im rovements in screw propellers, the object eing to so construct the same that lateral slip between the propeller and the medium in which it rotates is obviated.
According to the invention I provide a cylindrical, conical or similar ring around the outside of the pro eller, the tips of the blades being connecte to the inner surface of the said ring, the axis of which is coinci dent with that of the propeller boss; ring may be continuous, or it may be broken at one ormore points, in which case it isin the form of a number of segments attached to the tips of the propeller blades. The ring, is open at both sides and those portions between the adj acentblades are recessed or cut away at one side, the recesses extending to say about the center of the boss of the propeller.
To enable the invention to be fully understood I will describe it by reference to the accompanying drawings, in which Figure 1 is a side elevation of a ropeller *ig. 2 is a section on the line 2-2, Fig. 1. Fig. 3 is a plan view thereof. Fig. 4 is a development of a art of the ring. Fig. 5 is a view similar to Fig. 3 illustrating a modification, and Fig. 6 is a lan view thereof.
Re errin first to the arrangement illustrated in Figs. 1 to 4 a is the boss of the propeller and b, b, b the blades thereof. 0 is the ring which is provided around the outside of the propeller and the axis of which is coincident with that of the boss a. In the arrangement illustrated in the drawing the ring 0 is continuous and the tips of the blades 1), b are connected to its inner surface as clearly shown, the inner or inside end of the said ring being cut away so as to form the recesses d, d between the propeller blades b, b;
The
these recesses extend, as above mentioned, to about the center of the boss (I of the propeller.
By constructing a propeller as above described, the water (or air) in which the propeller is revolving, is forced through the ring more or less like a solid column in a direction opposite to that in which the vessel to which the propeller is attached is to move, thus obviati'ng lateral slip from the propeller blades.
In the arrangement illustrated in Figs. 5 and 6 I have shown the ring made'in two parts, e and f, the portion 6 being composed of segments forming the recesses d, d and attached to the tips of the propeller blades b and the portion f being fixed so as not to rotate with the propeller, that is to say, being secured in place by means of the stays g to the rear of the vessel. With this construction it will be clear that a certain amount of friction between the rotating ring and the water is avoided.
In some cases, in lieu of a recessed continuous ring, I may make use of a discontinuous ring, that is to say, of a number of segments which are attached to the tips of the propeller blades. I prefer, however, to use a continuous ring as above described.
Having now particularly described and ascertained the nature of my said invention and in what manner the same is to be performed, I declare that what I claim is 1. In a screw propeller, the combination with blades of a ring encircling the ends of said blades and secured thereto, said ring being of greater width than the width of said blades and extending rearwardly therefrom, the front edge of said ring being provided with notches between said blades, substantial] y as described.
2. In a screw propeller, the combination with blades, of a two part ring encircling said blades, said ring being concentric with the axis of rotation and having one part thereof secured to said blades, the other part thereof being adapted to remain stationary, substantially as described.
3. In a screw propeller, the combination with blades, of a two part ring encircling said blades, said ring being concentric with the axis of rotation and of greater Width than thewidth of said blades, and having one part thereof secured to said blades, the other part thereof being adapted to remain stationary, substantially as described.
4. In a screw propeller, the combination with blades, of a two part ring encircling said blades, said ring being concentric with the axis of rotation and of greater Width than the Width of said blades and having one part 50- 1o cured to said blades, the front edge of said part being notched between said blades, the other of said parts being adapted to remain stationary, substantially as described.
VENZEL PREIDEL. Witnesses:
JOHN E. BoUsFIELn, O. Gr. REDFERN.
US29039305A 1905-12-05 1905-12-05 Screw-propeller. Expired - Lifetime US855131A (en)

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US29039305A US855131A (en) 1905-12-05 1905-12-05 Screw-propeller.

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US29039305A US855131A (en) 1905-12-05 1905-12-05 Screw-propeller.

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Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3258245A (en) * 1964-07-20 1966-06-28 Gen Electric Blade stiffening means
US4505641A (en) * 1980-03-07 1985-03-19 Aisin Seiki Kabushiki Kaisha Cooling fan for internal combustion engine
US5044884A (en) * 1989-09-05 1991-09-03 Trustees Of The University Of Pennsylvania Safety propeller
US5096382A (en) * 1989-05-17 1992-03-17 Gratzer Louis B Ring-shrouded propeller
US5405243A (en) * 1990-12-14 1995-04-11 Stealth Propulsion Pty. Ltd. Propeller with shrouding ring attached to blade
US20070071603A1 (en) * 2005-09-27 2007-03-29 Denso Corporation Fan and blower unit having the same
US20080064274A1 (en) * 2006-09-11 2008-03-13 Brentnall Jesse Higgs Boat propeller
US20130115087A1 (en) * 2011-11-09 2013-05-09 Johnson Electric S.A. Axial Fan
US20130209242A1 (en) * 2010-08-05 2013-08-15 Mitsuba Corporation Cooling fan
US20140169970A1 (en) * 2012-12-18 2014-06-19 Michael A. Celentano Attached duct propeller system
CN108591119A (en) * 2018-03-07 2018-09-28 常州祥明智能动力股份有限公司 A kind of axial flow fan vane wheel
US20190226747A1 (en) * 2018-01-25 2019-07-25 Johnson Controls Technology Company Condenser unit with fan
US11203413B2 (en) 2018-11-07 2021-12-21 N99 Llc Advanced propeller assemblies

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3258245A (en) * 1964-07-20 1966-06-28 Gen Electric Blade stiffening means
US4505641A (en) * 1980-03-07 1985-03-19 Aisin Seiki Kabushiki Kaisha Cooling fan for internal combustion engine
US5096382A (en) * 1989-05-17 1992-03-17 Gratzer Louis B Ring-shrouded propeller
US5044884A (en) * 1989-09-05 1991-09-03 Trustees Of The University Of Pennsylvania Safety propeller
US5405243A (en) * 1990-12-14 1995-04-11 Stealth Propulsion Pty. Ltd. Propeller with shrouding ring attached to blade
US20070071603A1 (en) * 2005-09-27 2007-03-29 Denso Corporation Fan and blower unit having the same
JP2007092562A (en) * 2005-09-27 2007-04-12 Denso Corp Cooling fan and blower
US7632063B2 (en) * 2005-09-27 2009-12-15 Denso Corporation Fan and blower unit having the same
JP4618077B2 (en) * 2005-09-27 2011-01-26 株式会社デンソー Cooling fan and blower
US20080064274A1 (en) * 2006-09-11 2008-03-13 Brentnall Jesse Higgs Boat propeller
US9803645B2 (en) * 2010-08-05 2017-10-31 Mitsuba Corporation Cooling fan
US20130209242A1 (en) * 2010-08-05 2013-08-15 Mitsuba Corporation Cooling fan
CN103104552A (en) * 2011-11-09 2013-05-15 德昌电机(深圳)有限公司 Axial fan
US9206816B2 (en) * 2011-11-09 2015-12-08 Johnson Electric S.A. Axial fan
US20130115087A1 (en) * 2011-11-09 2013-05-09 Johnson Electric S.A. Axial Fan
US20140169970A1 (en) * 2012-12-18 2014-06-19 Michael A. Celentano Attached duct propeller system
US20190226747A1 (en) * 2018-01-25 2019-07-25 Johnson Controls Technology Company Condenser unit with fan
US10962275B2 (en) * 2018-01-25 2021-03-30 Johnson Controls Technology Company Condenser unit with fan
CN108591119A (en) * 2018-03-07 2018-09-28 常州祥明智能动力股份有限公司 A kind of axial flow fan vane wheel
US11203413B2 (en) 2018-11-07 2021-12-21 N99 Llc Advanced propeller assemblies

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