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Publication numberUS1861065 A
Publication typeGrant
Publication dateMay 31, 1932
Filing dateJun 19, 1931
Priority dateAug 18, 1930
Publication numberUS 1861065 A, US 1861065A, US-A-1861065, US1861065 A, US1861065A
InventorsPhilippe Poot
Original AssigneePhilippe Poot
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Screw-propeller for flying machines and other aerodynamics apparatus
US 1861065 A
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Description  (OCR text may contain errors)

P. FOOT I May 31 1932.

SCREW PROPELLER FOR FLYING MACHINES AND OTHER AERODYNMIICS APPARATUS Filed June 19. 1931 Patented May 31, 1932 UNITED STATES PATENT OFFICE PHILIPPE PO01, OF SAVENTHEM, BELGIUM.

Application filed June 19, 1931, Serial No.

I have made foreign applications as fol-' lows: in Belgium, on August 18th, 1930, No. 37 2,767; in Germany, on April 20th, 1931.

My present invention relates to screw-pro- 5 pellers for flying machines and other aerodynamics apparatus and it has for its object to provide an improved screw-propeller of this type, that is one in which the wings are undulated or waved in. the plane parallel to the axis of the propeller as well as at right angles to said axis.

A further object of my invention is to provide a screw-propeller of the type described, in which the axes of the wave troughs for the inner waves or undulations coincide with a circumference the center of which is located on the hub member of the propeller on the extension of the base line of the Wave troughs, whilst for the outer wave troughs the axes of 29 the troughs coincide with a circumference the centre of which is located on the extension of the front edge line of the propeller wing.

Other objects and advantages of my invention will appear from the following disclosure taken in connection with the accompanying drawings showing by way of example one preferred embodiment of my invention and in which:

Fig. 1 is a front elevation of a screw-propeller having two alined wings.

Fig. 2 is a diagrammatica'l cross section thereof, showing the different pitches of the screw threads.

Referring more particularly to the drawings, my improved screw-propeller is constructed with two or more combined pitches. Each wing of the screw-propeller is limited on the side turned towards the wind by a straight line 1 el, whilst the rear edge 2-3 thereof is undulated or waved in the plane parallel to the axis 11 as well as at right angles thereto. The peaks or crests are designated by the numeral 2 and the troughs by the numeral 3. The wave troughs 3 are made of conical shape and the apexes thereof are turned towards the straight edge 1-4, that is towards the wind. The axes of these wave troughs correspond: for the inner waves or undulations to a circumference 6 the centre 9 of which is located on the cen- 545,509, and in Belgium August 18, 1930.

tral portion or hub member 7 of the screw propeller on the extension of the base line 8, and for the outer Wave troughs to a circun1- ference 5 the centre 10 of which'is located a on the extension of the. front wing edge a. Owing to this particular arrangement the vacuum in front of the propeller Wing will be highly increased, whereby an increase of the action of the pressure existing at the rear of the wing will be obtained.

Referring more particularly to Fig. 2 of the drawings, the section line l2, representwill be saved and on the other hand the energy driving the screw wings forwardly will be reduced.

Minor details of the construction described and shown may be changed or modified as desired without departing from the scope of my invention.

I claim:

In a screw-propeller for flying machines and other aerodynamics apparatus having a plurality of wings, the combination with each wing body, of undulations or waves formed in said body parallel to the axis of the screw-propeller as well as at right angles thereto, the axes of the inner wave troughs coinciding with a circumferencethe centre of which is located on the central portion or hub member of the screw-propeller on the extension of the base line of said troughs, Whilst the axes of the outer wave troughs coincide with a circumference the centre of which is located on the extension of the front straight edge line of the wing body, substantially as set forth.

PHILIPPE POOT.

Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US2899128 *Feb 12, 1957Aug 11, 1959 Vaghi
US2962101 *Feb 12, 1958Nov 29, 1960Vaghi JosephWater screw propeller
US4089618 *Feb 5, 1976May 16, 1978Rotron IncorporatedFan with noise reduction
US4108573 *Jan 26, 1977Aug 22, 1978Westinghouse Electric Corp.Vibratory tuning of rotatable blades for elastic fluid machines
US4872484 *Dec 12, 1988Oct 10, 1989John HickeySystem for controlling the flow of a fluid medium relative to an object
US4886421 *Jan 4, 1988Dec 12, 1989Wind Feather, United Science Asc.Wind turbine air foil
US4974633 *Dec 19, 1989Dec 4, 1990Hickey John JSystem for controlling the flow of a fluid medium relative to an object
US5075564 *Feb 23, 1990Dec 24, 1991Hickey John JCombined solar and wind powered generator with spiral surface pattern
US5254876 *May 28, 1992Oct 19, 1993Hickey John JCombined solar and wind powered generator with spiral blades
US5463257 *Feb 28, 1995Oct 31, 1995Yea; Ton A.For generating electricity
US7976283 *Nov 10, 2010Jul 12, 2011General Electric CompanyNoise reducer for rotor blade in wind turbine
US8267657Dec 16, 2010Sep 18, 2012General Electric CompanyNoise reducer for rotor blade in wind turbine
US8414261May 31, 2011Apr 9, 2013General Electric CompanyNoise reducer for rotor blade in wind turbine
US8430638Dec 19, 2011Apr 30, 2013General Electric CompanyNoise reducer for rotor blade in wind turbine
US8523515Nov 15, 2010Sep 3, 2013General Electric CompanyNoise reducer for rotor blade in wind turbine
DE102006044330B4 *Sep 19, 2006Nov 11, 2010Karl SternFlügelrotor
DE102006044332B3 *Sep 19, 2006Jan 3, 2008Karl SternRotor vane especially for underwater power station, has vibrator sheath arranged externally on vane and lying in the plane of the blade
Classifications
U.S. Classification416/235
International ClassificationB64C11/16, B64C11/00
Cooperative ClassificationB64C11/16
European ClassificationB64C11/16