US1366635A - Propeller - Google Patents

Propeller Download PDF

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Publication number
US1366635A
US1366635A US286525A US28652519A US1366635A US 1366635 A US1366635 A US 1366635A US 286525 A US286525 A US 286525A US 28652519 A US28652519 A US 28652519A US 1366635 A US1366635 A US 1366635A
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Prior art keywords
depressions
propeller
blades
blade
rotation
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Expired - Lifetime
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US286525A
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Edward P Conway
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Individual
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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

Definitions

  • My invention relates to the class of devicesabove described, and an object of the invention, among others, is to increase ciency of the propeller by a construction of blade that will cause the propeller to have increased hold upon the medium in which it may be rotated.
  • Figure 1 is a back view of my improved propeller when looking in the direction indicated by the arrows in Figs. 2 and 3.
  • Fig. 2 is an edge view of the same when looking in the direction indicated by the dotted line 2-2 and arrows in Fig. 1.
  • Fig. 3 is an end view of the device.
  • Fig. i is a View in section through the propeller on a plane denoted by dotted line H of Fig.
  • Fig. 5 is a View in section through the propeller on plane denoted by dotted line 55 of Fig. 2.
  • the numeral 5 denotes the hub of my improved propeller having blades 6 projecting there from in opposite directions and they may be inclined at an angle to the plane of rotation, as is common in devices of this class.
  • the blades of propellers have commonly been plain and smooth from the hub to the tip with a re suit that the air slips toward the end of the blade by centrifugal action and consequently the hold ofthe blade upon the air or other medium in whichit may be rotating is not so great as it would be did this outward movement of the medium by centrifugal action not take place, the term holding denoting the frictional resistance of the blade to movement of the fluid lengthwise of the blade, whereby diminished rarety of the air within the sphere of rotation of the blade is prevented.
  • I provide grooves or depressions '7 extending crosswise of the blades and located on the backs thereof, these depressions, in their preferred torm, being narrower at their front edges, or that edge of the blade in advance when the propeller is rotated, the direction of rotation being indicated by the arrow in Fig. 1.
  • the width of the depressions are illcreasedpreferably on curved lines, and said depressions are also formed on curved lines that are substantially uniform onopposite sides of a line extending centrally through thedepressions from end to end.
  • the onposlte sides of the blades are curved to a greater or lesser degree so that the depth of the depressions from front to rear is increased, although the formation of the depressions are such that the bottoms thereof are formed on straight lines from one end to the other thereof, that is, there is no curve in the depressions in a direction crosswise of the blades.
  • This formation of the bot toms of the depressions on straight lines lengthwise thereof presents no greater obstruction to the movement of the blade through the medium upon which it is acting than that inclination of the blade required to exert the proper hold upon such medium.
  • my invention is not limited in its scope to a depression or groove in the propeller of the specific shape herein shown and described, and they may be varied therefrom to some extent and yet embody the invention and in accordance with the provisions of the patent statutes, I have described the principles of operation of my invention, together with the device which I new consider to represent the best embodiment thereof; but I desire to have it understood that the device shown is only illustrative, and that the invention may be carried out by other means.
  • a propeller including a hub, blades on tending therefrom and smooth on one side, i
  • each blade on the opposite side and increasing in area from the front to the rear edge thereof, the dimensions of said depression being substantially equal on opposite sides of a line passing centrally therethrough, the bottom line of said depressions being straight and tangent to the curve of rotation thereof.
  • a propeller including a hub, blades eX-- tending therefrom, and a series of depressions arranged lengthwise of the blades, all
  • tom lines of said depressions being straight and parallel and tangent to the curve of rotation thereof.
  • a propeller including a hub, blades eX- tending therefrom and angularly disposed with respect to the plane of rotation thereof, and a series of depressions arranged lengthwise of the blades, each depression er:- tending' crosswise thereof and having its bottom formed on straight lines lengthwise thereof and crosswise of theiblade and tan gent to the curve of rotation and all ofsaid depressions increasing in area from the front to the rear.
  • a propeller including a hub, blades extending therefrom and smooth on one side, and a series of depressions extending across each blade on the side opposite the smooth side and increasing in area from the front to the rear edge'thereof, said depressions being curved lengthwise of the blade and substantially equal on opposite sides of a line passing centrally therethrough, the bottom line of said depressions being straight and tangent to the curve of rotationthereof.
  • a propeller including a hub, blades ex tending therefrom and smooth on one side
  • depressions extending across the blades, said depressions beingeurved lengthwise of the blade and increasing in width from the front to the rear and in depth also from the front to the rear edge, the bottom line of said depressions being straight and tangent to the curve of rotation thereof.

Description

E. P. CONWAY.
PROPELLER. APPLICATION HLED MAR.31. 1919.
Patented Jan. 25, 1921.
IN VEN TOR.
EZTORNEY.
Ma's PETERS .n: um E c,
UNITED srA'res ZEIIJX7V'..4.R1) IE. CDNWAY, O1? "WATERBURY, CONNECTICUT.
PROPELLER.
Specification of Letters Patent.
Patented Jan. 25, 1921.
Application filed March 31, 1919. Serial No. 286,525.
To all whom it may concern."
Be it known that I, Enwnno P. CONWAY, a citizen of the United States, and a resident of lVaterbury, in the county of New Haven and dtate of Connecticut, have invented a new and Improved Propeller, of which the following is a specification.
My invention relates to the class of devicesabove described, and an object of the invention, among others, is to increase ciency of the propeller by a construction of blade that will cause the propeller to have increased hold upon the medium in which it may be rotated.
One form of device embodying my invention and in the construction and use of which the objects herein set out, as well as others, may be attained, is illustrated in the accompanying drawings, in which Figure 1 is a back view of my improved propeller when looking in the direction indicated by the arrows in Figs. 2 and 3.
Fig. 2 is an edge view of the same when looking in the direction indicated by the dotted line 2-2 and arrows in Fig. 1.
Fig. 3 is an end view of the device.
Fig. i is a View in section through the propeller on a plane denoted by dotted line H of Fig.
Fig. 5 is a View in section through the propeller on plane denoted by dotted line 55 of Fig. 2.
In the accompanying drawings the numeral 5 denotes the hub of my improved propeller having blades 6 projecting there from in opposite directions and they may be inclined at an angle to the plane of rotation, as is common in devices of this class.
Prior to my invention the blades of propellers have commonly been plain and smooth from the hub to the tip with a re suit that the air slips toward the end of the blade by centrifugal action and consequently the hold ofthe blade upon the air or other medium in whichit may be rotating is not so great as it would be did this outward movement of the medium by centrifugal action not take place, the term holding denoting the frictional resistance of the blade to movement of the fluid lengthwise of the blade, whereby diminished rarety of the air within the sphere of rotation of the blade is prevented.
To overcome this result and increase the hold of the blades of the propeller on the medium in which they rotate, I provide grooves or depressions '7 extending crosswise of the blades and located on the backs thereof, these depressions, in their preferred torm, being narrower at their front edges, or that edge of the blade in advance when the propeller is rotated, the direction of rotation being indicated by the arrow in Fig. 1. The width of the depressions are illcreasedpreferably on curved lines, and said depressions are also formed on curved lines that are substantially uniform onopposite sides of a line extending centrally through thedepressions from end to end. The onposlte sides of the blades are curved to a greater or lesser degree so that the depth of the depressions from front to rear is increased, although the formation of the depressions are such that the bottoms thereof are formed on straight lines from one end to the other thereof, that is, there is no curve in the depressions in a direction crosswise of the blades. This formation of the bot toms of the depressions on straight lines lengthwise thereof presents no greater obstruction to the movement of the blade through the medium upon which it is acting than that inclination of the blade required to exert the proper hold upon such medium. However, my invention is not limited in its scope to a depression or groove in the propeller of the specific shape herein shown and described, and they may be varied therefrom to some extent and yet embody the invention and in accordance with the provisions of the patent statutes, I have described the principles of operation of my invention, together with the device which I new consider to represent the best embodiment thereof; but I desire to have it understood that the device shown is only illustrative, and that the invention may be carried out by other means.
I claim- 1. A propeller including a hub, blades on tending therefrom and smooth on one side, i
and a depression extending across each blade on the opposite side and increasing in area from the front to the rear edge thereof, the dimensions of said depression being substantially equal on opposite sides of a line passing centrally therethrough, the bottom line of said depressions being straight and tangent to the curve of rotation thereof.
2. A propeller including a hub, blades eX-- tending therefrom, and a series of depressions arranged lengthwise of the blades, all
of said depressions increasing in area from the front to the rear edges of the blades,.
tom lines of said depressions being straight and parallel and tangent to the curve of rotation thereof.
' 3. A propeller including a hub, blades eX- tending therefrom and angularly disposed with respect to the plane of rotation thereof, and a series of depressions arranged lengthwise of the blades, each depression er:- tending' crosswise thereof and having its bottom formed on straight lines lengthwise thereof and crosswise of theiblade and tan gent to the curve of rotation and all ofsaid depressions increasing in area from the front to the rear.'
4. A propeller including a hub, blades extending therefrom and smooth on one side, and a series of depressions extending across each blade on the side opposite the smooth side and increasing in area from the front to the rear edge'thereof, said depressions being curved lengthwise of the blade and substantially equal on opposite sides of a line passing centrally therethrough, the bottom line of said depressions being straight and tangent to the curve of rotationthereof.
5. A propeller including a hub, blades ex tending therefrom and smooth on one side,
and depressions extending across the blades, said depressions beingeurved lengthwise of the blade and increasing in width from the front to the rear and in depth also from the front to the rear edge, the bottom line of said depressions being straight and tangent to the curve of rotation thereof.
' EDWARD P. CONWAY.
US286525A 1919-03-31 1919-03-31 Propeller Expired - Lifetime US1366635A (en)

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Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2899128A (en) * 1959-08-11 Vaghi
US4789117A (en) * 1986-12-29 1988-12-06 United Technologies Corporation Bodies with reduced base drag
US4813633A (en) * 1986-12-29 1989-03-21 United Technologies Corporation Airfoil trailing edge
US4830315A (en) * 1986-04-30 1989-05-16 United Technologies Corporation Airfoil-shaped body
DE9013099U1 (en) * 1990-09-14 1991-11-07 Moser, Josef, 8058 Pretzen, De
US20090013532A1 (en) * 2007-07-09 2009-01-15 Trevor Howard Wood Airfoils for use in rotary machines and method for fabricating same
CN101684773A (en) * 2008-09-26 2010-03-31 通用电气公司 Wind turbine blade
US20100266428A1 (en) * 2008-01-07 2010-10-21 Suguru Nakagawa Propeller fan
US20120114498A1 (en) * 2010-11-05 2012-05-10 Hsieh Chi-Hao Fan structure
US20140301860A1 (en) * 2013-04-09 2014-10-09 MTU Aero Engines AG Airfoil having a profiled trailing edge for a fluid flow machine, blade, and integrally blade rotor
EP2711558A3 (en) * 2012-09-24 2017-12-13 Samsung Electronics Co., Ltd Propeller fan
EP2759471A3 (en) * 2013-01-25 2018-01-03 Rolls-Royce plc Fluidfoil
US20180127086A1 (en) * 2016-11-10 2018-05-10 Coretronic Intelligent Robotics Corporation Aerial Vehicle and Propeller Thereof

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2899128A (en) * 1959-08-11 Vaghi
US4830315A (en) * 1986-04-30 1989-05-16 United Technologies Corporation Airfoil-shaped body
US4789117A (en) * 1986-12-29 1988-12-06 United Technologies Corporation Bodies with reduced base drag
US4813633A (en) * 1986-12-29 1989-03-21 United Technologies Corporation Airfoil trailing edge
DE9013099U1 (en) * 1990-09-14 1991-11-07 Moser, Josef, 8058 Pretzen, De
US8083487B2 (en) * 2007-07-09 2011-12-27 General Electric Company Rotary airfoils and method for fabricating same
US20090013532A1 (en) * 2007-07-09 2009-01-15 Trevor Howard Wood Airfoils for use in rotary machines and method for fabricating same
EP2014870B1 (en) * 2007-07-09 2016-10-05 General Electric Company Airfoil for use in rotary machines
US8419372B2 (en) 2007-07-09 2013-04-16 General Electric Company Airfoil having reduced wake
US8721280B2 (en) * 2008-01-07 2014-05-13 Daikin Industries, Ltd. Propeller fan
US20100266428A1 (en) * 2008-01-07 2010-10-21 Suguru Nakagawa Propeller fan
EP2169216A3 (en) * 2008-09-26 2012-01-11 General Electric Company Wind turbine blade
US8016568B2 (en) * 2008-09-26 2011-09-13 General Electric Company Wind turbine blade
CN101684773A (en) * 2008-09-26 2010-03-31 通用电气公司 Wind turbine blade
US20100080709A1 (en) * 2008-09-26 2010-04-01 General Electric Company Wind turbine blade
EP2169216A2 (en) * 2008-09-26 2010-03-31 General Electric Company Wind turbine blade
US8939729B2 (en) * 2010-11-05 2015-01-27 Delta Electronics, Inc. Fan structure
TWI464328B (en) * 2010-11-05 2014-12-11 Delta Electronics Inc Fan structure
US20120114498A1 (en) * 2010-11-05 2012-05-10 Hsieh Chi-Hao Fan structure
EP2711558A3 (en) * 2012-09-24 2017-12-13 Samsung Electronics Co., Ltd Propeller fan
EP2759471A3 (en) * 2013-01-25 2018-01-03 Rolls-Royce plc Fluidfoil
US10113431B2 (en) 2013-01-25 2018-10-30 Rolls-Royce Plc Fluidfoil
US20140301860A1 (en) * 2013-04-09 2014-10-09 MTU Aero Engines AG Airfoil having a profiled trailing edge for a fluid flow machine, blade, and integrally blade rotor
US9657576B2 (en) * 2013-04-09 2017-05-23 MTU Aero Engines AG Airfoil having a profiled trailing edge for a fluid flow machine, blade, and integrally blade rotor
US20180127086A1 (en) * 2016-11-10 2018-05-10 Coretronic Intelligent Robotics Corporation Aerial Vehicle and Propeller Thereof

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