US199550A - Improvement in screw-propellers - Google Patents

Improvement in screw-propellers Download PDF

Info

Publication number
US199550A
US199550A US199550DA US199550A US 199550 A US199550 A US 199550A US 199550D A US199550D A US 199550DA US 199550 A US199550 A US 199550A
Authority
US
United States
Prior art keywords
blades
wheel
screw
helicoidal
backward
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
Publication date
Application granted granted Critical
Publication of US199550A publication Critical patent/US199550A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/02Units comprising pumps and their driving means
    • F04D25/08Units comprising pumps and their driving means the working fluid being air, e.g. for ventilation
    • F04D25/088Ceiling fans

Definitions

  • Figure l is a rear view of my propellerscrew.
  • Fig. 2 is a side view;
  • Fig. 3, a section of the blade, illustrating its position on the arm;
  • Fig. 4, a detailed view, showing the process of construction of the blades;
  • Fig. 5, a rear view, showing the bracing for the extension of the blades.
  • My invention relates to the construction and relative position of the blades of a propellerscrew, by which not only increased progressive power is obtained, but said power is augmented relatively as the revolution is increased.
  • My invention consists, first, in constructing the blades of mypropeller-wheel of a helicoidal form, as will be described; secondly, inclining the operating-surface of the blades backward Vtoward the outer end of the shaft-that is, in
  • my invention consists in securing said helicoidal-shaped blades to the outer ends/of radial arms extending from the revolving shaft, said outer ends of the arms inclining backward at a similar angle to preserve the aforesaid position of the blades.
  • A represents the revolving shaft of a propeller-engine
  • B the boss or hub of the propeller-wheel.
  • Extending outward radially from the hub B are the arms C C, attached to the hub B in any of the well-known ways.
  • These arms C are preferably perpendicular to the shaft A, except at the outer ends, where the part c, for a distance the width of the blades of the wheel, are inclined backward, or toward the outer. end of the shaft, thus making the rear side of the wheel concavethat is, if a line parallel to the part c of the arm C be produced until it meets the axis of rotation of the shaft A, it will meet it at an acute angle.
  • D in theV drawings are the blades of the wheel, secured to the part c of the arm C.
  • the blades D are of a helicoidal form, and are cut in blanks, as d, from the sheet, forming the segment of an annular ring the size of the Wheel to be formed. Said segment d, after being cut, is straight transversely, as seen at di; then it is bent in a curve, as seen at d2; and then the alternate corners are bent in opposite directions, forming the helicoidal shape, as seen at d3, with one corner straightened, as at y.
  • This blade D is then properly secured to the part c of the arm C, with the helicoidal surface inclinin g backward, so that a section of this surface made by a plane passing through the axis of rotation shall be inclined backward :at a constant angle with the axis, as seen in Figs. 2 and 3, wherein the dotted lines are drawn in planes passing through the axis of rotation i, and show the inclination backward of the blades D.
  • the length of the blades D is arbitrary; but if blades much extended should be desired, an elongated or double hub would be necessary, with two or more sets of arms, as seen in Fig. 5; but this is ⁇ no part of my present application for a patent.
  • the helicoidal blade of a propeller-wheel constructed asfrom a segmentof a flat annular ring, lirst bent in a curve transversely, and then its alternate corners bent in opposite directions, with one corner straightened, substantially as described.

Description

' I1.VJ.HU LBBRT.
Screw-Propellers.
Np'. 199,550. V .Pafentedrlm 22,1878.
UNITED STATES lPET-ENT OFFICE.
EDwIN J, HULBEET, `or MIDDLETowN, CONNECTICUT,
IMPROVEMENT IN SCR-EWrPROPELLERS.
Specification forming part of Letters Patent No. 199,550, dated January 22, 18.78; application filed March 14, 1877.
To all 'whom/t may concern:
Be it known that I, EDWIN JAMES HUL- BERT, of Middletown, Connecticut, have invented Improvements in Screws for Propellin g Vessels; and I do hereby declare the following to be a full and correct description of the same, reference being had to the accompanying drawings, in which the same letters refer to corresponding parts.
Figure l is a rear view of my propellerscrew. Fig. 2 is a side view; Fig. 3, a section of the blade, illustrating its position on the arm; Fig. 4, a detailed view, showing the process of construction of the blades; and Fig. 5, a rear view, showing the bracing for the extension of the blades.
My invention relates to the construction and relative position of the blades of a propellerscrew, by which not only increased progressive power is obtained, but said power is augmented relatively as the revolution is increased.
My invention consists, first, in constructing the blades of mypropeller-wheel of a helicoidal form, as will be described; secondly, inclining the operating-surface of the blades backward Vtoward the outer end of the shaft-that is, in
such position that a section of this helicoidal surface made by a plane passing through the axis of rotation shall be inclined backward at a constant angle with the axis; and, thirdly, my invention consists in securing said helicoidal-shaped blades to the outer ends/of radial arms extending from the revolving shaft, said outer ends of the arms inclining backward at a similar angle to preserve the aforesaid position of the blades.
In the drawings, A represents the revolving shaft of a propeller-engine, and B the boss or hub of the propeller-wheel. Extending outward radially from the hub B are the arms C C, attached to the hub B in any of the well-known ways. These arms C are preferably perpendicular to the shaft A, except at the outer ends, where the part c, for a distance the width of the blades of the wheel, are inclined backward, or toward the outer. end of the shaft, thus making the rear side of the wheel concavethat is, if a line parallel to the part c of the arm C be produced until it meets the axis of rotation of the shaft A, it will meet it at an acute angle. (See Figs. 2 and 3.) D in theV drawings are the blades of the wheel, secured to the part c of the arm C. The blades D are of a helicoidal form, and are cut in blanks, as d, from the sheet, forming the segment of an annular ring the size of the Wheel to be formed. Said segment d, after being cut, is straight transversely, as seen at di; then it is bent in a curve, as seen at d2; and then the alternate corners are bent in opposite directions, forming the helicoidal shape, as seen at d3, with one corner straightened, as at y. This blade D is then properly secured to the part c of the arm C, with the helicoidal surface inclinin g backward, so that a section of this surface made by a plane passing through the axis of rotation shall be inclined backward :at a constant angle with the axis, as seen in Figs. 2 and 3, wherein the dotted lines are drawn in planes passing through the axis of rotation i, and show the inclination backward of the blades D. The length of the blades D is arbitrary; but if blades much extended should be desired, an elongated or double hub would be necessary, with two or more sets of arms, as seen in Fig. 5; but this is `no part of my present application for a patent.
The operation of my device is as follows: The wheel, as constructed, having been properly secured to the revolving shaft of the engine of a propeller, and rotated at a desired velocity, the blades D, being inclined backward, will tend to throw the water inward in a conical shape, while at the same time, the arms C giving but little resistance to the core of water passing centrally through the wheel between the blades, the Water of the core and the water from the blades, meeting, combine and assist to relieve the wheel from dead-water, and consequently tend to prevent that churning 7 of the water which is experienced in the ordinary wheels, especially at high velocities.
Having thus fully described my invention, what I claim, and desire to secure by Letters Patent, is-
1. The helicoidal blade of a propeller-wheel, constructed asfrom a segmentof a flat annular ring, lirst bent in a curve transversely, and then its alternate corners bent in opposite directions, with one corner straightened, substantially as described.
2. The blades of a screw-propeller, the helicoidal surface of which is of the form described, I
so that a section of 'its surface made by a plane passing through the. axis of rotation shall be inclined backward at a constant angle with the axis, substantially as set forth.
3. The revolving shaft of a screw-propeller,
' carrying one or more radial arms, said arms having their outer ends bent backward from a perpendicular, as and for the purpose set forth.
4. The blades of -a propeller fwheel of the helicoidal shape described, secured upon the outer ends of radial arms bent backward so Vas to retain the blades in their angular position, as described.
US199550D Improvement in screw-propellers Expired - Lifetime US199550A (en)

Publications (1)

Publication Number Publication Date
US199550A true US199550A (en) 1878-01-22

Family

ID=2268957

Family Applications (1)

Application Number Title Priority Date Filing Date
US199550D Expired - Lifetime US199550A (en) Improvement in screw-propellers

Country Status (1)

Country Link
US (1) US199550A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2422388A (en) * 1943-04-05 1947-06-17 Arthur W Billings Airplane propeller
DE102004035902B3 (en) * 2004-07-19 2006-03-02 Moros, Hans-Jürgen, Dipl.-Phys.Ing. Ring segment repeller used in wind power technology, aircraft manufacture and in ship building comprises thin-walled circular or elliptical ring segments formed as angle-adjusted repeller elements rotating about a rotational axis

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2422388A (en) * 1943-04-05 1947-06-17 Arthur W Billings Airplane propeller
DE102004035902B3 (en) * 2004-07-19 2006-03-02 Moros, Hans-Jürgen, Dipl.-Phys.Ing. Ring segment repeller used in wind power technology, aircraft manufacture and in ship building comprises thin-walled circular or elliptical ring segments formed as angle-adjusted repeller elements rotating about a rotational axis

Similar Documents

Publication Publication Date Title
US4531890A (en) Centrifugal fan impeller
JP2001509226A (en) Impeller and fan incorporating it
US199550A (en) Improvement in screw-propellers
US1371610A (en) Screw-propeller
US885109A (en) Screw-propeller.
US1138083A (en) Rotary fan.
US2240653A (en) Fan
US201650A (en) Improvement in screw-propellers
US698582A (en) Propeller-wheel.
US995562A (en) Propelling-wheel.
US1030047A (en) Propeller.
US384498A (en) bartlett
US1232795A (en) Circular-disk fan.
US350278A (en) Screw-propeller
US283592A (en) John f
US229270A (en) perkins
US199126A (en) Improvement in screw-propellers
US505402A (en) Screw-propeller
US156375A (en) Improvement in screw-propellers
US1323102A (en) Propeller
US204575A (en) Improvement in screw-propellers
US152973A (en) Improvement in screw-propellers
US528253A (en) Island
US887156A (en) Propeller-wheel.
US219837A (en) Improvement in propellers for vessels