US1757667A - Device for regulating wind wheels - Google Patents

Device for regulating wind wheels Download PDF

Info

Publication number
US1757667A
US1757667A US278305A US27830528A US1757667A US 1757667 A US1757667 A US 1757667A US 278305 A US278305 A US 278305A US 27830528 A US27830528 A US 27830528A US 1757667 A US1757667 A US 1757667A
Authority
US
United States
Prior art keywords
vanes
hub
arms
wind
rack
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
US278305A
Inventor
Hesse Erich
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Application granted granted Critical
Publication of US1757667A publication Critical patent/US1757667A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D7/00Controlling wind motors 
    • F03D7/02Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor
    • F03D7/022Adjusting aerodynamic properties of the blades
    • F03D7/0224Adjusting blade pitch
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/70Adjusting of angle of incidence or attack of rotating blades
    • F05B2260/74Adjusting of angle of incidence or attack of rotating blades by turning around an axis perpendicular the rotor centre line
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/70Adjusting of angle of incidence or attack of rotating blades
    • F05B2260/75Adjusting of angle of incidence or attack of rotating blades the adjusting mechanism not using auxiliary power sources, e.g. servos
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/70Adjusting of angle of incidence or attack of rotating blades
    • F05B2260/77Adjusting of angle of incidence or attack of rotating blades the adjusting mechanism driven or triggered by centrifugal forces
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/70Adjusting of angle of incidence or attack of rotating blades
    • F05B2260/79Bearing, support or actuation arrangements therefor
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction

Definitions

  • This invention relates to a device for regulating the number of revolutions, as well as the performance, of wind-wheels by'turning and at the same time shifting the vanes upon their arms with the aid of curved guide members, the difierence between the centrifugal force arising in the vanes and a uniform-counter-force being used as the re-ad ustmg power.
  • igure 2 is a section located at right angles with respect to Fig. 1.
  • r f o l On the'drawin 1 denotes the hollow main shaft of thewintgwheel, and 2 a hub secured 7 3 are two hollow arms holding the vanes i'which areturnable, as well as 'shiftable, upon these arms.
  • crossed rods 7 couple each vane with a rod'8located axially 'inthearm 3 in such a manner that the vane 7 can turn upon the arm.
  • thedriving'gear for each va e can be arra d symm r al y th re
  • the counter-force draws' the vanes radially inwards so that their. inner endscontact with the outer ends of'the hub, as
  • a device for regulating wind wheelsto obtaina. uniform; rotational speed, comprisin .in combination withthe-ma-in shaft, the
  • ' 31A device for regulating wind-wheels to Obtain a uniform rotational speed comprislnga hub a pair of arms pro ecting from said hub a'rodaxially'provided 1n mounted on eachcarm-and secured-to the outer end ofthe rod; a rod slidably mounted in axial relation to the hub and-havinga gear rack at the inner endiandcounter-force means each arm and havlng a gear rack at the inner end a vane crease of the force of air .to maintain the wind-wheel-at a uniform speed.
  • a device for regulatingwind wheelsto obtain a uniform rotational" speed comprisinga hub a pair of arms proj ecting from said hub ;a rod axially provided in each arm and having'a gear rack at theinner end; vane mounted'oneach arm andisecured to the outer end-of the, rod; a rod slidably mounted' in axial relation, to thehub and havin'gza gear rack at the inner endand'counter-force means at the Iouter'endf; a plurality of" gear wheels in the hub meshing with the gear racks of the rods andpins and cooperating slot means on the arms andvanes adapted toturn the vanes at the increase or decrease of therfor'ce ofv the air when thejcentrifugal force of-the vanes, and the counterforce become unequal to. maintain thej wind wheel' at a. predeteri mined uni'form speed.

Description

May 6, 1930. E. HESSE DEYICE FOR REGULATING WIND WHEELS Filed May is, 1928 4 n 1 ll-MM. z
Patented May 6, 1930 i ire STA res PATENT foFF lcE Enron HESSE, or InsrEn Und eE n ANY DEVICE FonnneULA'rInG wnvn WHEELS a i Application filed May is, 1928, Serial No.
This invention relates to a device for regulating the number of revolutions, as well as the performance, of wind-wheels by'turning and at the same time shifting the vanes upon their arms with the aid of curved guide members, the difierence between the centrifugal force arising in the vanes and a uniform-counter-force being used as the re-ad ustmg power. "The present lmproved devlce 1s d1s tinguished from the known devices for regui counteracting the centrifugal force arising in the vanes is transmitted to themechanism by means of a rack extending through the hol low'main shaft ofthe wind-wheel and being coupled, by the intermediary ofsuitable gearings, with a system of rods located in every vane and extendingin, and parallel to, the
axis passing through the centre of'gravity of the respective vane. Owing to this arrangement and combination of the parts the curved guide members taking part in effecting theturning of the vanes on said axis are loaded only with the slight re-a'djusting power required for producing that turning.
I am aware of the fact that it has already been proposed, with regulating devices for wind-mill vanes, to couple their shutter or shutters by means of rods and levers with cog-wheels carried by the vanes-holding rim and meshing with a cylindrical rack which is longitudinally movable and located in the hollow wind-wheel shaft. This arrangement and combination of parts has not,'however, a uniform ratio of transmission on account of the lever connection. Maintaining the ratio of transmission with turnable propeller vanes is known, the respective arrangement-being such that the shifting of a rack with, steep thread is used to shift another steep thread carrying the vane which is prevented" from shifting. The shifting of the rack is efi'ected inthis case either manually or by means of a utilized in, thatQknown device.
thereto I V and reverselv.
th like, the respective 278,305, anainer any May 21, 192?.
motor. The centrifugal force arising in the vaneswlnle they are rotating is, thus, not
The' invention is illustrated diagrammatically and by wayof example on theaccomjpanying drawing on which Figure 1 is an axialrsection through a two-vane wind-wheel,
one of the vanes being partly broken-away,
and igure 2 is a section located at right angles with respect to Fig. 1. r f o l On the'drawin 1 denotes the hollow main shaft of thewintgwheel, and 2 a hub secured 7 3 are two hollow arms holding the vanes i'which areturnable, as well as 'shiftable, upon these arms. The vanesare; of course, flat, and pins 6 projecting inwardly from the lar'ge faces of the-wings engage curved Slotsl5 provided in the arms 3 whereby the arms are turned when they are shifted,
'5 and 6 from the'centrifugal force arising when the vanes are rotating, crossed rods 7 couple each vane with a rod'8located axially 'inthearm 3 in such a manner that the vane 7 can turn upon the arm.
The, inner end of the rod Sis connected with two'parallel rods 10 by means of'a crosspiece 9; the inner halves of the rods 10 are transformed into racks located within the hollow hub 2, and these racks mesh with cogwheels 11, firmly connected with an axle 12 supported in the sides of aflat casing 13 connected with the correspondingly shaped hub.
There are two wheels 11, corresponding to the two racks'1'O, and both mesh with pinions lt firmly connected with an axle 15 also supported'in; said flat casing. A cog-wheel 16 located between said pinions and 'also secured to the ax1e;15 meshes with a rack rod 17 located in the bore of the hollow main shaft 1. This rack is subjected to a pull exerted in the direction of the'arrow either'bythe'tem sion of a spring/or by a weight or ;by an electromagnet, or, a-solenoid respectively, or
pull constituting a uniform ,countenforce.
"Owingto the provision of two racks 10 locatedbne at the left and: the other at the right of the rod'-8, thedriving'gear for each va e can be arra d symm r al y th re In order to relieve ,the parts H around the axis of the shaft 1',. of course-with it and the hub 2, as well as with the casing 13, with a speed that lies belowa certain predetermined limit, or a certain maximum speed respectively; the counter-force draws' the vanes radially inwards so that their. inner endscontact with the outer ends of'the hub, as
in the figures. If,liowever,that limit or maximumr speedc is surpassed, the centrifugal force becomes greater thanthe counter-force, in consequence whereof the vanes: move outwards along therarms 3:.whereby the curved slots 5 of theselatter act upon the pins.6 andcause thereby a corresponding turning of'the vanes upon the arms, the direction of this, turning being such that the pressure which;the wind has exerted upon the vanes is nowless than. before. Theresultof this is that the rotational speed becomes less, and the centrifugal force becomes smaller, also in -proportion: to. the counter-force, and the vanes. are.- nowdrawn inwards upon their arms bythe counter-force. until the forces balance one] another and equilibriumhas, therefore, been re-established. I
Itis obvious that the ultimate efiectof the device consists ina uniform number of revolut-ions and uniform performance. Equiliuhoflthe-wheel, and hollowa-rms projecting from. the: hub, Y vanfesglocat'ed libriumiexists only at a certain definite number of revolutions, irrespectlve of the .posi- Ition: ofthe. vanes upon their. arms.-
All operating partsof the regulation device are housed in the chamber formed by the hub. and. the. casing, I and' are, therefore. securely protected, V
1:. A device for regulating wind wheelsto obtaina. uniform; rotational speed, comprisin .in combination withthe-ma-in shaft, the
hiiblo'f the wheel, andhollow'arm'sprojecting radially forth fromthe hub, vanes located V .uponsaid, arms "and: being adapted to be shifted and simultaneously. therewithtobe turned thereon rods: located. in said hollow arms in theraxisvp'a's'sing throughthe point of gravity of each vane, arack at theinner end ofcieach o f tsaid arodgai gearing meshing; with ed andsimultaneously therewith to be turned thereon, rods located in said hollow arms in the axis passing through the point of gravity of each vane, two parallel racks at the end of each of said rods, gearings meshing with the racks ofeach of said rods, and a common central rack meshing with all said-gear-iiigs and sub ected" to the actlon'of a counter-force.
' 31A device for regulating wind-wheels to Obtain a uniform rotational speed comprislnga hub a pair of arms pro ecting from said hub a'rodaxially'provided 1n mounted on eachcarm-and secured-to the outer end ofthe rod; a rod slidably mounted in axial relation to the hub and-havinga gear rack at the inner endiandcounter-force means each arm and havlng a gear rack at the inner end a vane crease of the force of air .to maintain the wind-wheel-at a uniform speed.
4;. A device for regulatingwind wheelsto obtain a uniform rotational" speed 'compris inga hub a pair of arms proj ecting from said hub ;a rod axially provided in each arm and having'a gear rack at theinner end; vane mounted'oneach arm andisecured to the outer end-of the, rod; a rod slidably mounted' in axial relation, to thehub and havin'gza gear rack at the inner endand'counter-force means at the Iouter'endf; a plurality of" gear wheels in the hub meshing with the gear racks of the rods andpins and cooperating slot means on the arms andvanes adapted toturn the vanes at the increase or decrease of therfor'ce ofv the air when thejcentrifugal force of-the vanes, and the counterforce become unequal to. maintain thej wind wheel' at a. predeteri mined uni'form speed.
= In. testimony whereof I haveaffixed my signature.
' ERIGH', H ssE;
said rack, and a=commonccentral racklmesh mg: with all. Sflldi gearings Sub eCted to the act-ion -ofa 'c'ounter-force.-
2. A device for regulating w111d-.wheels;-to
obtain: a iuniform rotational speed, comprisiiig in combination.withthe main ishaft,-.the
US278305A 1927-05-21 1928-05-16 Device for regulating wind wheels Expired - Lifetime US1757667A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE290988X 1927-05-21

Publications (1)

Publication Number Publication Date
US1757667A true US1757667A (en) 1930-05-06

Family

ID=6065281

Family Applications (1)

Application Number Title Priority Date Filing Date
US278305A Expired - Lifetime US1757667A (en) 1927-05-21 1928-05-16 Device for regulating wind wheels

Country Status (3)

Country Link
US (1) US1757667A (en)
GB (1) GB290988A (en)
NL (1) NL22407C (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4137010A (en) * 1977-07-25 1979-01-30 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Constant lift rotor for a heavier than air craft
US4335996A (en) * 1980-12-01 1982-06-22 Ross Joel M Windmill construction
US4374631A (en) * 1981-05-21 1983-02-22 Fayette Manufacturing Corporation Windmill speed limiting system utilizing hysteresis
WO1984004362A1 (en) * 1983-04-27 1984-11-08 Gyula Vari Wind driven power source
US4575309A (en) * 1983-05-25 1986-03-11 James Howden & Company Ltd. Wind turbines
US4710101A (en) * 1985-04-26 1987-12-01 James Howden & Company Limited Wind turbine
US20050008488A1 (en) * 2002-01-18 2005-01-13 Brueckner Manfred Karl Sky turbine that may be mounted on top of a city
US20060093483A1 (en) * 2002-01-18 2006-05-04 Brueckner Manfred K Sky turbine that is mounted on a city

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4137010A (en) * 1977-07-25 1979-01-30 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Constant lift rotor for a heavier than air craft
US4335996A (en) * 1980-12-01 1982-06-22 Ross Joel M Windmill construction
US4374631A (en) * 1981-05-21 1983-02-22 Fayette Manufacturing Corporation Windmill speed limiting system utilizing hysteresis
WO1984004362A1 (en) * 1983-04-27 1984-11-08 Gyula Vari Wind driven power source
US4575309A (en) * 1983-05-25 1986-03-11 James Howden & Company Ltd. Wind turbines
US4710101A (en) * 1985-04-26 1987-12-01 James Howden & Company Limited Wind turbine
US20050008488A1 (en) * 2002-01-18 2005-01-13 Brueckner Manfred Karl Sky turbine that may be mounted on top of a city
US20060093483A1 (en) * 2002-01-18 2006-05-04 Brueckner Manfred K Sky turbine that is mounted on a city
US7131812B2 (en) 2002-01-18 2006-11-07 Manfred Karl Brueckner Sky turbine that is mounted on a city

Also Published As

Publication number Publication date
GB290988A (en) 1928-09-13
NL22407C (en)

Similar Documents

Publication Publication Date Title
US1757667A (en) Device for regulating wind wheels
CA2884659C (en) Rotorcraft and planetary gear systems
US9709136B2 (en) Aircraft and planetary gear systems
US4983153A (en) Gear unit, particularly for use in a helicopter
CN103266988B (en) Wind generating set and variable pitch driving system thereof
US3825370A (en) Pitch varying mechanism for variable pitch fan
US2461931A (en) Multistage compressor
US3910721A (en) Pitch varying mechanisms for bladed rotors
US2146367A (en) Propeller
US1973573A (en) Screw propeller
US2117788A (en) Aeroplane propeller
JPS621690A (en) Variable pitch propeller
US2085483A (en) Aircraft propelling device
EP3705753B1 (en) Continuously variable transmission for ram air turbines
JP6078103B2 (en) Variable pitch rotor with remote counterweight
US2382229A (en) Controllable pitch propeller
US2275361A (en) Adjustable pitch propeller
US3794442A (en) Variable pitch rotary blading
US1757292A (en) Cooling fan
US2243046A (en) Selective two pitch airscrew
US2237030A (en) Aeronautical propeller
US2427136A (en) Supercharger
WO2020238280A1 (en) Continuously variable transmission
US2594160A (en) Variable pitch propeller with an axially movable hub
US1969280A (en) Propeller