US1467227A - Air impeller or propeller - Google Patents

Air impeller or propeller Download PDF

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Publication number
US1467227A
US1467227A US498096A US49809621A US1467227A US 1467227 A US1467227 A US 1467227A US 498096 A US498096 A US 498096A US 49809621 A US49809621 A US 49809621A US 1467227 A US1467227 A US 1467227A
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blades
impeller
oblique
propeller
air
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/325—Rotors specially for elastic fluids for axial flow pumps for axial flow fans
    • F04D29/326—Rotors specially for elastic fluids for axial flow pumps for axial flow fans comprising a rotating shroud

Definitions

  • This invention relates to air impellers or propellers and consists of certain improvements hereinafter expressed, in the type of impeller or propeller adaptable to and capable of:-(a) creating a current of air when caused to rotate in stationary mountings, (b) advancing through the air when mounted and caused to rotate as the propeller of an aeroplane and (0) being
  • the invention consists in providing a conical containing ring around the blades and in some instances providin in such form of impeller a lip upon one-e go of the blades.
  • Figure 1 is an elevation of an impeller or propeller constructed with the improved containing ring.
  • Figure 2 shows a portlon of an impeller constructed with the improved containing ring and improved blades.
  • Figure 3 is a section on tortuous line M--M Figure 1 lookin from right to left and showing a method of mounting.
  • Figure d is a section at YZ Fi re 1
  • Figure 5 is a section at W- Figure 2, showing the improved blade. 7
  • the blades may be formed by cutting suitable slots in a disc C and bending the parts A of the blades obliquely out of the plane of thedisc
  • the outer extremities of the blades A C are suitably attached' to the interior of a conical containing ring E, converging in the direction of the portions A.
  • This ring E may have a cylindrical extension H beyond the portions A of the blades.
  • the disc C is attached at its centre to a flanged sleeve F which is fixed and carried upon a shaft G.
  • the sleeve may be contained within a coneshaped member P thus forming a cone shaped boss which guides the air to the blades.
  • the shaft G may be j ournalled in bearings as shown at K.
  • a modified blade is formed by bending the edges of the portions of the disc C remote from the portions A obliquely out of the plane of the disc to form lips as shown at L in Figures 2 and 5 this bend being in a reverse direction to that of the portions A.
  • What is claimed is 1.
  • blades each consisting of a portion of a disc perpendicular to the axis of said impeller and a ortion oblique to said axis, and on the lea ing side of said perpendicular portion, and a conical ring converging in the direction of said oblique portions secured to the outer extremities of said blades.
  • blades each consisting of a portion of a disc perpendicular to the axis of said impeller and a portion oblique to said axis and on the leadin side of said perpendicular portion, a conica ring converging in the direction of said oblique portions secured to the outer extremities of said blades and a cylindrical extension of said ring.
  • blades each consisting of a portion of a disc perpendicular to the axis of said impeller, a portion oblique to said axis and on the leading side of said perpendicular portion, and an oblique lip remote from and oppositely directed to said oblique portion.
  • blades each consisting of a portion of a disc perpendicular to the axis of said impeller, a portion oblique to said axis and on the leading side of said perpendicular portion, an oblique lipremote from and oppositely directed to said oblique portion, and a conical ring converging in the direction of said oblique portions secured to the outer extremities of said blades.
  • blades each consisting of a portion of a disc perpendicular to the axis of said impeller, a portion oblique to said axis and on the leading side of said perpendicular portion, and an oblique lip remote from and oppositely directed to said oblique portion, a conical ring converging in the direction of said oblique portions secured to the outer extremities of said blades and a cylindrical extension of said ring.

Description

Sept. 4, 1923. 1,467.22?
G. M. CAPELL AIR IMPELLER OR PROPELLER Filed Sept. 2. 1921 ATTY.
Patented Sept. 4, 1923.
GEORGE MIARIE CAPELL, DECEASED, LATE 0F PASSENHAM, NEAR STONY STRATFORD, ENGLAND; BY ROBERT ALFRED BLAKE, TRUSTEE AND LEGAL REPRESENTATIVE.
AIR IMPELLER OR PROPELLER.
Application filed September 2, 1921. Serial No. 498,096.
To all whom it may concern:
Be it known that GEORGE MARIE CAPELL, deceased, subject of the King of Great Britain, late residing at Passenham, near Stony Stratford, in the county of Bucks, England, has invented new and useful Improvements in and Relating to Air Impellers or Propellers, of which the following is a specification,
This invention relates to air impellers or propellers and consists of certain improvements hereinafter expressed, in the type of impeller or propeller adaptable to and capable of:-(a) creating a current of air when caused to rotate in stationary mountings, (b) advancing through the air when mounted and caused to rotate as the propeller of an aeroplane and (0) being The invention consists in providing a conical containing ring around the blades and in some instances providin in such form of impeller a lip upon one-e go of the blades.
Figure 1 is an elevation of an impeller or propeller constructed with the improved containing ring. Figure 2 shows a portlon of an impeller constructed with the improved containing ring and improved blades. Figure 3 is a section on tortuous line M--M Figure 1 lookin from right to left and showing a method of mounting. Figure d is a section at YZ Fi re 1, and Figure 5 is a section at W- Figure 2, showing the improved blade. 7
As previously proposed the blades may be formed by cutting suitable slots in a disc C and bending the parts A of the blades obliquely out of the plane of thedisc According to the present invention the outer extremities of the blades A C are suitably attached' to the interior of a conical containing ring E, converging in the direction of the portions A. This ring E may have a cylindrical extension H beyond the portions A of the blades. The disc C is attached at its centre to a flanged sleeve F which is fixed and carried upon a shaft G. The sleeve may be contained within a coneshaped member P thus forming a cone shaped boss which guides the air to the blades.
The shaft G may be j ournalled in bearings as shown at K.
A modified blade is formed by bending the edges of the portions of the disc C remote from the portions A obliquely out of the plane of the disc to form lips as shown at L in Figures 2 and 5 this bend being in a reverse direction to that of the portions A. What is claimed is 1. In an air impeller, blades each consisting of a portion of a disc perpendicular to the axis of said impeller and a ortion oblique to said axis, and on the lea ing side of said perpendicular portion, and a conical ring converging in the direction of said oblique portions secured to the outer extremities of said blades.
2. In an air impeller, blades each consisting of a portion of a disc perpendicular to the axis of said impeller and a portion oblique to said axis and on the leadin side of said perpendicular portion, a conica ring converging in the direction of said oblique portions secured to the outer extremities of said blades and a cylindrical extension of said ring.
3. In an air impeller, blades each consisting of a portion of a disc perpendicular to the axis of said impeller, a portion oblique to said axis and on the leading side of said perpendicular portion, and an oblique lip remote from and oppositely directed to said oblique portion.
4. In an air impeller, blades each consisting of a portion of a disc perpendicular to the axis of said impeller, a portion oblique to said axis and on the leading side of said perpendicular portion, an oblique lipremote from and oppositely directed to said oblique portion, and a conical ring converging in the direction of said oblique portions secured to the outer extremities of said blades.
meme? 5. In an air impeller, blades each consisting of a portion of a disc perpendicular to the axis of said impeller, a portion oblique to said axis and on the leading side of said perpendicular portion, and an oblique lip remote from and oppositely directed to said oblique portion, a conical ring converging in the direction of said oblique portions secured to the outer extremities of said blades and a cylindrical extension of said ring. 10
In testimony whereof I have signed my name to this specification.
ROBERT ALFRED BLAKE.
Trustee and legal representative of George Marie Capell, deceased.
US498096A 1921-09-02 1921-09-02 Air impeller or propeller Expired - Lifetime US1467227A (en)

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Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2615301A (en) * 1946-11-09 1952-10-28 United Aircraft Corp Centrifugal diffuser
US2800967A (en) * 1955-05-09 1957-07-30 Fogel Jacob Fan rotor
US2831630A (en) * 1955-01-21 1958-04-22 Perry John Fan
US3746465A (en) * 1971-08-11 1973-07-17 Lummus Industries Centrifugal fan for handling material
US4362469A (en) * 1979-09-04 1982-12-07 Stichting Energieonderzoek Centrum Nederland Device for deriving energy from a flow of fluid
US4364712A (en) * 1980-07-10 1982-12-21 Canadian Fram Cross flow cooling fan
US4664598A (en) * 1984-10-05 1987-05-12 Reliance Electric Company Unitized quick-assembly fan
US4692098A (en) * 1981-08-31 1987-09-08 General Motors Corporation Airfoil for high efficiency/high lift fan
US4697988A (en) * 1986-02-04 1987-10-06 Her Majesty The Queen In Right Of Canada, As Represented By The Minister Of Energy & Natural Resources Reinforced delta-wing blade for wind turbine
US4871298A (en) * 1987-07-09 1989-10-03 Ecia - Equipments Et Composants Pour L'industrie Automoblie Falciform blade for a propeller and its application in particular in motorized fans for automobiles
US6370695B2 (en) 1998-01-16 2002-04-16 Depuy Orthopaedics, Inc. Head gear apparatus
US20040068208A1 (en) * 1998-09-25 2004-04-08 Cimino William Wayne Surgical system console
WO2004083631A2 (en) 2003-03-18 2004-09-30 Renewable Devices Swift Turbines Limited Wind turbine
US6990691B2 (en) 2003-07-18 2006-01-31 Depuy Products, Inc. Head gear apparatus

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2615301A (en) * 1946-11-09 1952-10-28 United Aircraft Corp Centrifugal diffuser
US2831630A (en) * 1955-01-21 1958-04-22 Perry John Fan
US2800967A (en) * 1955-05-09 1957-07-30 Fogel Jacob Fan rotor
US3746465A (en) * 1971-08-11 1973-07-17 Lummus Industries Centrifugal fan for handling material
US4362469A (en) * 1979-09-04 1982-12-07 Stichting Energieonderzoek Centrum Nederland Device for deriving energy from a flow of fluid
US4364712A (en) * 1980-07-10 1982-12-21 Canadian Fram Cross flow cooling fan
US4692098A (en) * 1981-08-31 1987-09-08 General Motors Corporation Airfoil for high efficiency/high lift fan
US4664598A (en) * 1984-10-05 1987-05-12 Reliance Electric Company Unitized quick-assembly fan
US4697988A (en) * 1986-02-04 1987-10-06 Her Majesty The Queen In Right Of Canada, As Represented By The Minister Of Energy & Natural Resources Reinforced delta-wing blade for wind turbine
US4871298A (en) * 1987-07-09 1989-10-03 Ecia - Equipments Et Composants Pour L'industrie Automoblie Falciform blade for a propeller and its application in particular in motorized fans for automobiles
US6513168B2 (en) 1998-01-16 2003-02-04 Depuy Orthopaedics, Inc. Head gear apparatus
US6393617B1 (en) 1998-01-16 2002-05-28 Depuy Orthopaedics, Inc. Head gear apparatus
US6370695B2 (en) 1998-01-16 2002-04-16 Depuy Orthopaedics, Inc. Head gear apparatus
US6711748B2 (en) 1998-01-16 2004-03-30 Depuy Orthopaedics, Inc. Head gear apparatus having movably mounted fan
US20040068208A1 (en) * 1998-09-25 2004-04-08 Cimino William Wayne Surgical system console
US7550864B2 (en) * 2003-03-18 2009-06-23 Renewable Devices Swift Turbines Limited Wind turbine
WO2004083631A3 (en) * 2003-03-18 2005-01-27 Renewable Devices Ltd Wind turbine
US20060244264A1 (en) * 2003-03-18 2006-11-02 Renewable Devices Swift Turbines Limited Wind turbine
WO2004083631A2 (en) 2003-03-18 2004-09-30 Renewable Devices Swift Turbines Limited Wind turbine
AP2032A (en) * 2003-03-18 2009-08-25 Renewable Devices Swift Turbines Ltd Wind turbine
CN1788155B (en) * 2003-03-18 2010-11-17 可换部件轻便涡轮有限公司 Rotor of wind turbine and the wind turbine
AU2004221591B2 (en) * 2003-03-18 2011-01-27 Renewable Devices Swift Turbines Limited Wind turbine
US6990691B2 (en) 2003-07-18 2006-01-31 Depuy Products, Inc. Head gear apparatus
US7200873B2 (en) 2003-07-18 2007-04-10 Depuy Products, Inc. Head gear apparatus having improved air flow arrangement
US7937779B2 (en) 2003-07-18 2011-05-10 Depuy Products Head gear apparatus having improved air flow arrangement

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