GB767907A - Improved variable pitch air-driven bladed rotor unit - Google Patents

Improved variable pitch air-driven bladed rotor unit

Info

Publication number
GB767907A
GB767907A GB8393/55A GB839355A GB767907A GB 767907 A GB767907 A GB 767907A GB 8393/55 A GB8393/55 A GB 8393/55A GB 839355 A GB839355 A GB 839355A GB 767907 A GB767907 A GB 767907A
Authority
GB
United Kingdom
Prior art keywords
pins
blade
rotor
flyweights
retainer
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
Application number
GB8393/55A
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.)
Motors Liquidation Co
Original Assignee
Motors Liquidation Co
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 Motors Liquidation Co filed Critical Motors Liquidation Co
Publication of GB767907A publication Critical patent/GB767907A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30Blade pitch-changing mechanisms
    • B64C11/32Blade pitch-changing mechanisms mechanical
    • B64C11/34Blade pitch-changing mechanisms mechanical automatic
    • B64C11/343Blade pitch-changing mechanisms mechanical automatic actuated by the centrifugal force or the aerodynamic drag acting on the blades
    • 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
    • F05B2220/00Application
    • F05B2220/30Application in turbines
    • F05B2220/31Application in turbines in ram-air turbines ("RATS")
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Emergency Lowering Means (AREA)

Abstract

767,907. Wind-motors. GENERAL MOTORS CORPORATION. March 23, 1955 [April 1, 1954; April 1, 1954], No. 8393/55. Class 110 (3). A wind motor comprising flyweights, responsive to centrifugal force due to the rotation of the rotor, rotatable about the longitudinal axis of each blade so as to move upon rotation of the rotor in a direction similar to that of the blade toward a high pitch position has resilient means interconnecting each blade and associated flyweight which biases the blade toward the high pitch position and resilient means connected with the flyweights to oppose their movement under the action of centrifugal force. The rotor of a wind motor comprises a hub 20 in which are pivotably mounted the aerofoil section blades 31 by ball bearings 30. A retainer 50 is attached to the root of each blade by a nut 40 and relative movement between the blade and retainer is prevented by tangs 57. One end of a torsion spring 55 located in a groove 51 of the retainer is passed through wall 58 and the other end is attached to a flyweight 65, Fig. 4. Each flyweight is mounted by a ball bearing 62 in the retainer 50 and carries a pair of pins 66, 67. The pins 66 abut against the output shaft 25 and the pins 67 project into the cut-away portion of the wall 52, Fig. 6, of the retainer 50. The pins 67 are also engaged by a pair of links 70 which are pivotally connected to a collar 73 slidable on the shaft 25. The collar 73 is urged to the left by a spring 74. When the rotor is stationary, the pins 67 engage the shoulder 53, Fig. 6, and the pins 66 engage the shaft 25 and the blades are set to a high pitch stop position of approximately 75 degrees. When the rotor starts to rotate, the forces on the blades rotate the retainers 50 until the shoulders 54, Fig. 4, engage the pins 67. In this position the opposed forces of the governor spring 74 and the centrifugal twisting moments on the blades are in equilibrium with the centrifugal force on the flyweights and the aerodynamic twisting moment on the blades. The flyweights then govern the speed of the rotor. A pin 80 coacts with surfaces 82, 83 to limit the movement of the blade. In a modification the torsion spring 55 is replaced by a coiled tension spring and the flyweights in the form of a major segment of a cylinder having an arm which engages the shaft 25. This arm enables the pin 66 to be dispensed with. The governor spring 74 may be replaced by a pair of coaxial springs.
GB8393/55A 1954-04-01 1955-03-23 Improved variable pitch air-driven bladed rotor unit Expired GB767907A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US767907XA 1954-04-01 1954-04-01

Publications (1)

Publication Number Publication Date
GB767907A true GB767907A (en) 1957-02-06

Family

ID=22134202

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8393/55A Expired GB767907A (en) 1954-04-01 1955-03-23 Improved variable pitch air-driven bladed rotor unit

Country Status (1)

Country Link
GB (1) GB767907A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3013613A (en) * 1958-08-25 1961-12-19 Gen Motors Corp Air driven turbine
US4411596A (en) * 1980-03-25 1983-10-25 Sundstrand Corporation Ram air turbine control system
WO1986004385A1 (en) * 1985-01-24 1986-07-31 Sundstrand Corporation Ram air turbine
WO1987003332A1 (en) * 1985-11-22 1987-06-04 Sundstrand Corporation Ram air turbine control system
US4701104A (en) * 1986-06-18 1987-10-20 Sundstrand Corporation Ram air turbine
CN110182355A (en) * 2019-04-29 2019-08-30 中国航空工业集团公司金城南京机电液压工程研究中心 One kind being used for flight safety Emergency power source system feather centrifugal governor device

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3013613A (en) * 1958-08-25 1961-12-19 Gen Motors Corp Air driven turbine
US4411596A (en) * 1980-03-25 1983-10-25 Sundstrand Corporation Ram air turbine control system
WO1986004385A1 (en) * 1985-01-24 1986-07-31 Sundstrand Corporation Ram air turbine
WO1987003332A1 (en) * 1985-11-22 1987-06-04 Sundstrand Corporation Ram air turbine control system
US4743163A (en) * 1985-11-22 1988-05-10 Sundstrand Corporation Ram air turbine control system
US4701104A (en) * 1986-06-18 1987-10-20 Sundstrand Corporation Ram air turbine
CN110182355A (en) * 2019-04-29 2019-08-30 中国航空工业集团公司金城南京机电液压工程研究中心 One kind being used for flight safety Emergency power source system feather centrifugal governor device

Similar Documents

Publication Publication Date Title
US2485543A (en) Power plant
US4743163A (en) Ram air turbine control system
US4411596A (en) Ram air turbine control system
GB767907A (en) Improved variable pitch air-driven bladed rotor unit
US3215370A (en) Rotating wing aircraft
US2876847A (en) Air driven propeller and governor therefor
US2997109A (en) Air driven turbine
US3013613A (en) Air driven turbine
FR2300233A1 (en) Windmill with variable pitch blades - pitch of blade is automatically reduced as wind force increases
US1537401A (en) Controlling or regulating device for propellers
FR2295259A1 (en) Wind driven turbine with fixed pitch blades - and speed control by varying angle of inclination of rotor axis
GB735111A (en) Improvements in or relating to high speed windmill motors
US2857006A (en) Air driven propeller and governor therefor
CA2073406C (en) Pitch control mechanism
ATE31905T1 (en) AUTOMATIC PROPELLER BLADE ANGLE ADJUSTMENT DEVICE.
US2600531A (en) Rotary wing aircraft
SU1801A1 (en) Two-blade propeller for aircraft station wireless
SU1000586A1 (en) Wind engine
US2962258A (en) Slotted vane turbine governor
GB722978A (en) Improvements in wind-power plant with a centrifugal governor
GB876954A (en) Constant speed and feathering propeller
US2987926A (en) Mechanical governors
US2029674A (en) Windmill
GB816485A (en) Improvements in or relating to ram air turbine
ES8406336A1 (en) Aircraft lift rotors