Classifications

• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
  • F03D—WIND MOTORS
  • F03D7/00—Controlling wind motors 
  • F03D7/02—Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor
  • F03D7/022—Adjusting aerodynamic properties of the blades
  • F03D7/0236—Adjusting aerodynamic properties of the blades by changing the active surface of the wind engaging parts, e.g. reefing or furling
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
  • F03D—WIND MOTORS
  • F03D9/00—Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
  • F03D9/20—Wind motors characterised by the driven apparatus
  • F03D9/25—Wind motors characterised by the driven apparatus the apparatus being an electrical generator
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
  • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
  • F05B2270/00—Control
  • F05B2270/10—Purpose of the control system
  • F05B2270/103—Purpose of the control system to affect the output of the engine
  • F05B2270/1033—Power (if explicitly mentioned)
• • Y—GENERAL 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
  • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
  • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
  • Y02E10/00—Energy generation through renewable energy sources
  • Y02E10/70—Wind energy
  • Y02E10/72—Wind turbines with rotation axis in wind direction

Definitions

• the present invention relates to wind powered electrical generators, and mountings and control systems therefore.
• the problems associated with wind generated electrical power primarily relate to the need for maintenance and control.
• the propellers that drive the rotating components must be capable of operating in a wide range of wind speeds, and also must be designed or controlled in some manner to keep from exceeding design limits relating to the propeller rpm, maximum generator current output, the load, and the state of charge of the storage batteries (where such batteries are used). Also, the maximum permissible battery bank charging current or load current must be observed in widely varying wind conditions.
• the present invention relates to a wind powered generator mechanical arra ' ngement and control.
• the generator comprises a propeller having a directly coupled rotating field comprising permanent magnets mounted in a rotating housing.
• the stationary armature in turn is sup ⁇ ported on a suitable tower support and is mounted to permit it to rotate about a vertical axis to permit the propeller to be properly oriented with respect to the direction of the wind.
• On the opposite side of the vertical mounting axis from the propeller a suitable control and counterweight arm is mounted providing a balanced support for the generator.
• a vane or tail is mounted for pivotal movement about a vertical axis relative to the counterweight arm, and its angle relative to the counterweight arm and relative to the axis of rotation of the propeller can be varied in response to certain parameters that are being sensed.
• the vane controls the position of the propeller axis relative to the wind and thus may prevent excessive current from being generated; prevent overspeed; prevent overcharging storage batteries, if such are being used, and prevent the unit from providing excessive charging currents.
• the adjusting vane is controlled through a motor which is powered in response to signals indicating the state of selected conditions.
• the unit is designed to eliminate unnecessary short term adjustments of the vane by providing suitable time delay circuits, so that only smooth non-oscillatory operation results.
• the device may be mounted on a suitable high tower, and can have propeller diameters ranging from about two feet to about 50 feet.
• the energy storage can be in batteries, heat storage, hydrogen gas, compressed air or other means of utilizing AC or DC electrical energy such as direct connection to a utility line.
• the voltage range of course can be as desired.
• FIGURE 1 is a fragmentary side view of a typical wind generator tower showing a wind generating apparatus made according to the present invention installed thereon;
• FIGURE 2 is a top plan view of the device of FIGURE 1;
• FIGURE 3 is a sectional view taken as on line 3 — 3 in FIGURE 2;
• FIGURE is a schematic representation of the wind power generating apparatus of the present invention showing schematically certain of the interlocks for controlling the device in an alternating current generating system;
• FIGURE 5 is a schematic representation similar to FIGURE except in a direct current generating system
• FIGURE 6 is a more detailed block diagram of the tail motor control module showing the various functions of such module
• FIGURE 7 is a schematic detail of a switch arrangement for a tail control motor used with the device of the present invention.
• FIGURE 8 is a block diagram of a typical system control module used and represented in FIGURES and 5.
• the tower 15 may be a free standing tower that is supported on the ground, or it can be a stub tower mounted on the top of the building.
• the tower height is selected to achieve the maximum utilization of the wind that is available and can be of any desired construction.
• the bracket 12 is mounted to the top of the tower through a bearing 14A which carries thrust as well as radial loads
• the lower bearing 14 is a radial bearing that guides the tube 13 for free rotation about a generally upright axis.
• the generator assembly is shown partly in section in FIGURE 2, and as shown has a rotating field made up of permanent magnets 21.
• the rotating field magnets 21 are attached to and mounted on the interior of a cylindrical housing 20.
• the housing 20 has end plates 22 and 23, which in turn are rotatably mounted through suitable bearings 24 with respect to an armature shaft 25.
• the armature shaft 25 in turn is fixedly mounted into a hub 26.
• the hub 26 forms part of the bracket 12, at the upper end thereof, and the bracket 12 is suitably fixed to the rotating vertical tube 13.
• the armature shaft 25 supports a fixed or ⁇ on-rotating armature 27 that is held within the rotating housing 20.
• the armature is suitably wound in a known manner for providing the desired type of power (three phase etc.). Preferably, three " phase power will be generated.
• the number of field magnets and the positioning of the magnets will be arranged to provide the desired frequency and phase relationship of the output power. Because the armature is non-rotating relative to bracket 12 and tube 13, the lead wires from the armature windings can pass through a suitable passageway in the shaft 25, and then down through the bracket 12
• This slip ring assembly 30 can be of a conventional design because the only rotation is relatively infrequent and slow speed movement of the generator assembly about its upright axis due to changes in the wind or the angle of the blade with respect to the wind.
• a propeller 28 is mounted to a suitable hub on the end plate 23 opposite from the bracket hub 26.
• the propeller size and shape may be selected to suit the existing conditions.
• the wind acting on propeller 28 causes rotation of the housing 20 and field magnets 21.
• the bracket 12 also supports a counterweight balance arm indicated at 31.
• the axis of the balance arm is centered on the axis of the shaft 25 and extends outwardly from the bracket 12 on the opposite side of the vertical pivot axis of tube 13 from the generator assembly.
• the counterbalance arm 31, as shown perhaps best in FIGURE 3 has a cross section that forms a track.
• a slot indicated at 32 is provided in the lower wall thereof.
• a carriage 33 is mounted inside the track or arm 31.
• the carriage is mounted on suitable wheels 34 or on slide bearings.
• the carriage has an attached carriage arm 35 which extends through the slot 32 to the exterior of the arm 31.
• the arm 35 as shown in FIGURE 3 extends laterally from the counterbalance arm 31.
• the carriage arm 35 has a portion extending along side the counterbalance arm 31 and an upright pin 36 is mounted to the other end of arm 35.
• the movement of the carriage 33 along the counterbalance arm 31 is controlled through the use of a threaded rod 37 which is rotatably mounted in a suitable bearing adjacent the sleeve 26, and is threadably mounted through a threaded interior opening in the carriage 33.
• the opposite end of the threaded rod or screw 37 is drivably connected to the output shaft of a three phase, fractional horsepower motor indicated generally at 40 that in turn is suitably mounted to the outer end of the counterbalance arm 31.
• the three phase motor 40 is driven in selected direction (by reversing two leads) to cause the carriage to move longitudinally along the counterbalance arm at desired time.
• a suitable weight may be placed at the other end of the counterbalance arm (which could include the weight of the motor 40, plus additional weights that are necessary), to counterbalance the weight of the generator assembly about the axis of the pivot tube 13.
• the propeller 28 is a fixed pitch propeller, and is not a variable pitch propeller. Variable pitch propellers are relatively hard to control and require a good deal of mechanism. Complex mechanism always leads to more maintenance and thus elimination of the need for variable pitch simplifies the structure and tends to reduce required maintenance.
• the relative position of the rotational axis of the propeller is controlled.
• the rotational axis coincides with the longitudinal axis of the counterbalance 31.
• the relative wind position is controlled by a vane or tall assembly indicated generally at 50A.
• the tail assembly including a frame 50 is pivotally mounted as at 51 about an upright axis to a bracket 52 attached to the mounting bracket 12.
• the tail assembly 50A as shown is a lightweight frame that extends outwardly from this pivot.
• a tail plate or vane 53 is mounted at the other end of the tail frame 50, and of course has a large enough surface area so that as the wind blows it will tend to cause the tail frame 50 to align with the direction of the wind. For example, as shown in FIGURE 2 the wind is indicated by the arrow 54.
• the position of the tail frame 50 about the pivot 51 and therefore relative to the counterbalance arm 31 is controlled by the carriage 33 and motor 40.
• the pin 36 on arm 35 as shown has a link 55 pivotally mounted thereto, and the link is also pivotally mounted as at 56 to a bracket 57 mounted on the tail frame 50.
• the driving of the carriage along the arm which forms a track for the carriage will usually be done under power generated by the generator 11.
• suitable limit switches are utilized and these are shown schematically at 60 and 61 in the drawings.
• the limit switches are placed inside the arm 31 in a position to be contacted by the carriage 33 when the carriage has reached its desired extent of travel along the counterbalance arm.
• a sealing strip can be used along the slot 32 in arm 31.
• the sealing strip may fit tightly around the arm 35, and yields to permit the arm to move.
• the seal would have resilient lips that would close together to keep foreign material out of the track.
• FIGURE 4 a system schematic diagram is displayed for an alternating current supplementary system.
• the rotating housing 20 is illustrated, and also the magnets 21 are illustrated in the rotating housing only schematically.
• the armature 27 is shown in place, and the counterbalance arm 31 and related elements are also shown for orientatipn purposes.
• the armature 27 is wired to provide a three phase generator, and includes a first phase winding 62, a second phase winding 63, and a third phase winding 64 shown schematically.
• the electrical output is provided along the lines 62A, 63A and 64A, respectively.
• the line 62A extends to the tail control motor 40, and energizes one winding indicated at 40A of this three phase motor in the form of the invention shown.
• the generator is connected in a standard delta connection, while the motor is a Y connection motor.
• the lines 62A, 63A and 64A are connected to tail control circuits 65 and also to the load control circuits 66. Systems controls indicated at 67 are also connected to the tail controls.
• the tail control circuits are shown only as a block diagram in FIGURE 4, but include suitable relays and other controls to provide power from lines 63A and 64A to properly connect the lines to additional lines 69B and 69C, which in turn are connected to windings 40B and 40C, respectively.
• the limit switch and reversing connection are not shown in
• a vibration sensor shown generally at 72 can be provided on the counterbalance arm 31, and is connected by suitable lines 73 to the tail control circuits. This vibration sensor would be utilized to close down the system if it starts to shake apart, or to adjust the tail motor to minimize vibrations.
• a current transforer indicated generally at 74 is provided on line 64A, and a current transformer 75 is provided on line 62A. These current transformers are utilized to sense the amount of current being generated by the generator and used for controls.
• the lines 62A, 63A and 64A may have suitable fuses shown at 76 therein as well.
• the tail control circuit has inputs such as condition responsive sensors indicated generally at 78, in FIGURE 4.
• the tail control circuits include various components to sense the conditions that are provided by the current transformers and the input condition sensors 78.
• the generator may be dynamically braked by placing a large resistor into the output circuit of the generator.
• a large resistor 80 is provided and it is controlled from the tail control circuit through suitable relays as will be more fully explained.
• a spring loaded, normally applied mechanical brake illustrated schematically at 82 is provided.
• the brake can take a desired form, such as a band or block which engages the rotating housing, and the brake can be controlled by a solenoid 83 which may normally be energized to hold the brake released.
• Automatic controls and sensors may open contacts 118A to deenergize the brake solenoid when conditions sensed indicate a shut down is desired, but as shown a manual switch may also be used.
• the system control circuitry includes sensors to provide for connection to auxiliary loads if excessive current or voltage is being generated. Further, a tail motor control feedback signal may be provided
• a first auxiliary load 85 or a second auxiliary load 86 may be used to store or utilize electrical energy being generated.
• display monitors can be provided to indicate conditions. These may include lights or meters to show frequency, current, voltage and the like.
• the . output of the generator acting through the utility interface module 65 can provide power directly to a three phase utility line as indicated generally at 88, or if desired to a single phase utility line indicated generally at 89.
• the interface connections are identical to existing equipment, which will tie in auxiliary generators from a power plant when needed.
• the components used for sensing current and the like also are of conventional design.
• the relays for sensing load conditions and connecting the auxiliary loads to the system also are conventional.
• the controls operate with logic level signals with very low current consumption and may drive suitable amplifiers to carry out switching.
• FIGURE 5 a system diagram is provided for the wind generator of the present invention used with a direct current load such as a battery bank that has to be charged.
• the generator components are substantially the same as shown in FIGURE 4, except that a rectification circuit indicated generally at 90 is provided at the output lines 62A, 63A and 64A, and the DC output is provided along lines 90A and 90B.
• the lines 90A and 90B are connected to a battery bank 92 (or a DC load of some type).
• the current in line 90A may be sensed with a current sensor 91, and the current signal provides a control signal to the tail control circuit.
• the current sensor 91 of course is a DC current sensor.
• the battery voltage can be sensed across lines 93, which are connected to lines 90A and 90B.
• the battery voltage signal can be provided to the tail control circuit as well.
• the other components are the same and are numbered alike in FIGURES 4 and 5.
• FIGURE 6 the schematic diagram of the tail motor control circuitry is shown.
• the inputs include inputs that relate to both AC and DC systems, but only the appropriate sensor would be used with each system.
• logic level signals can be provided with relatively little current flow through sensors.
• the battery voltage sensor 95 used with a DC system for example can be combined with a'time delay 95A and comparator 95B.
• the comparator compares the actual sensed voltage of the battery with respect to a reference from a stabilized power supply 94.
• the comparator provides a logic level "one" signal along line 96 when the battery voltage is lower than desired. This signal is provided to a first input of a NOR gate 97. If the battery voltage is higher than the reference, a logic level high signal is provided along a line 98, to one input of a multiple input OR gate 99.
• the power supply may be a battery, if desired.
• the control components are generally mounted on the ground and the necessary signals are carried across slip rings in assembly 30.
• a generator current sensor 102 utilizes the current ' sensed by one of the current transformers shown in FIGURE 4, for example, and incorporates a rectifier 102A and comparator 102B.
• the sensed current may also be reduced in voltage through a transformer before rectification.
• the AC current is rectified, and then compared with a reference from the power supply 94 and if the generator current is above a desired level, a logic level "one" or high signal is provided along a line 103 to a second input of the OR gate 99.
• the circuit also may have a time delay as may all of the sensors to prevent chatter or oscillation from instantaneous current or voltage surges.
• An rpm sensor 104 such as a standard frequency sensing tachometer circuit is used to sense the alternating current output frequency of the generator.
• the sensor includes a comparator so that if the frequency of the signal from the tachometer is higher than the desired rpm, a high logic level signal would be provided along the line 105 to another input of the OR gate 99.
• Vibration sensor 72 is designed to provide a suitable signal if the amplitude of vibration is greater than a desired level. This "excessive vibration" output is provided along a line 106 to energize a relay 106 A through a suitable relay driver. The relay 106A controls contacts 106B. An "overspeed" fail-safe alternating current relay indicated generally at 110 can also be utilizied to provide an input control signal.
• the output frequency of the generator may be sensed from lines 63A and
• a suitable capacitor 110A connected to the diode bridge HOB also connected to line 63A and 64A.
• Suitable resistors HOC and HOD are connected across the diode bridge and lines 63A and 64A. If the generator overspeeds, the diode bridge provides an output that energizes a relay 112 which operates contacts 112A, 112B and 112C to initiate dynamic braking and suitable alarm circuits if desired, and also to disable the motor 40 as will be explained.
• Closing contacts 112A will energize a relay 113 which controls contacts 113A shown in FIGURE 4 and 5 to close the contacts and to thereby connect the dynamic brake resistor 80 into the load to slow down the generator unit.
• the contacts 106B also energizes relay 113 to connect the dynamic brake resistor to the generator output if the vibration becomes excessive.
• the relay 113 may be connected through a series resistor and capacitor as shown to ground.
• Power supply 94 or a separate power supply or battery may provide a voltage (indicated by plus signs on lines) for energizing the relays.
• Relay 113 for example, is connected to a line 113B carrying power to relay 113. When either contacts 106B or 112A close, the relay circuit is grounded and relay 113 energized. This also energizes a relay 111 which locks on relay 113 by closing contacts 111A. Normal reset is necessary to drop out the relay 111.
• a relay 118 is manually operated by a switch 118B to open contacts 118A leading to the brake solenoid and to thereby deenergize the brake solenoid.
• the contacts 118A are normally closed and whenever the control power is on the manual brake solenoid is energized to release the brake.
• the manual brake is thus a fail ⁇ safe device.
• battery current is sensed with sensor 91 (such as a meter relay).
• sensor 91 such as a meter relay
• the sensor 91 is also connected to a time delay and to a comparator 124.
• OMPI batteries are being charged an indicator light 122 will light. If the charging rate is greater than desired, the comparator provides a high logic level signal along a line 125 to a further input of the OR gate 99. If the batteries are discharging a level logic level "one" signal may be provided on line 123 to one input of NOR gate 97.
• a discharge indicator lamp 126 can also be provided for connection to the output of the current sensor to indicate discharging condition for the batteries.
• NOR gate 97 When either of the inputs to the NOR gate 97 for example are "ones", either because of a low battery voltage, or because of a battery current sensor being low, the output along a line 131 will be low and this is fed into one input of a second NOR gate 132.
• the NOR gate will provide a high output signal only when both of its inputs are low.
• the output of NOR gate 132 When both inputs are low the output of NOR gate 132 will act to energize a relay 134 through line 113B and a relay drive circuit 134D.
• the relay 134 operates reversing contacts 134A and 134B shown in FIGURE 7 to control direction of rotation of the tail control motor to increase the interceptance of the unit with the wind when the relay 134 is energized.
• the driver 134D includes a pulse stretcher circuit (a three second latch for example) and a transistor that conducts to ground when the base receives the pulse from gate 132.
• the relay 133 which controls contacts 133A and 133B (see FIGURE 7) is controlled by a relay driver 133D.
• the pulse from the pulse stretcher circuit of driver 134D is connected through a diode to the base of the transistor in the driver circuit 133D.
• the pulse relay 134 also actuates relay 133, closing contacts 133A and 133B and the motor 40 is energized.
• the screw is then driven to drive the carriage 33 away from the generator housing, which swings the vane 53 toward the arm 31 to increase the interceptance of the propeller into the wind.
• timer 136 If the output of OR gate 99 has been "high" during a selected preceding time period. The time period of timer 136 may be adjusted to suit the desired operation. The timer is made to smooth out instantaneous pulses that may occur, so that a signal to initiate the tail control motor to drive in direction to increase wind interceptance will not be provided until it is determined that no signal from OR gate 99 had existed for a desired length of time. The input of the timer 136 is on the output line 137 of the
• OR gate 99 Thus, if the OR gate 99 provides an output, the timer will be energized and the inhibit signal will not permit a increasing wind interceptance until no signal has been present for a desired length of time.
• the relay driver 133D is energized by the pulses from OR gate 99 to decrease wind interceptance.
• the driver 133D includes a pulse stretcher circuit and transistor as well.
• the decrease relay 133 will be powered from any one of the high signal inputs to OR gate 99.
• relay 133 will be energized directly through line 113B and contacts 112C when an overspeed occurs which energizes relays 112. Thus for safety the wind interceptance will be decreased to effectively shut the generator down.
• FIGURE 7 the schematic representation of the reversing circuit and the contacts used for controlling a tail control motor are illus ⁇ trated.
• the tail control motor 40 has its windings connected across a reversing set of contacts controlled by relay 134. These contacts are shown at 134A (normally closed), and 134B (normally open). With relay 134 energized, the rotation of the tail control motor 40 is to increase wind interception.
• the limit switches are also shown in circuit schematically in FIGURE 7 and are numbered the same as the other figures.
• the relay 133 controls the actual power contacts indicated at 133A and 133B in FIGURE 7 as well. These contacts are in lines 64A and 63A which connect to lines 69B and 69C.
• the third phase line of the tail control motor is always connected to one phase lead (62A) of the generator.
• the system control circuitry is used to detect load from power lines 68 (in the AC form) and on lines 93A in the DC system and to connect the power lines to auxiliary loads, as well as to determine if the generator is operating at maximum output in relation to the wind. Because these controls are conventional they are shown schematically.
• a battery voltage sensor signal (in the DC system) for example, from sensor 95 is fed through a suitable time delay to a comparator 95D.
• generator current sensor 102 may provide a time delayed, rectified signal to a comparator 102D. These signals may be properly weighted in relation to one or more reference voltages provided to the comparators. There may be several reference inputs with different outputs to indicate different levels of generator output or battery voltage. The outputs of the comparators 102D and 95D are provided to a logic circuit 150.
• An electric ammeter or wind velocity sensor 151 also is used and provides outputs in digital form to the logic circuit 150.
• the ammeter is mounted on or adjacent the tower for the generator.
• the logic is programmed to evaluate the wind velocity signal in relation to battery voltage and generator output, and if the battery voltage is low and the generator output is not at a desired level for a given wind velocity a signal comprising a system feedback signal on line 84 may be used to initiate a drive signal for the tail control motor.
• Such signal line may be connected to one input of an AND gate 160 which has a second input, an inverting input, connected to line 135 through a line 135A. If the signal on line 135 is low the connected input of AND gate 160 will be high. With a high signal on line 84 the AND gate output will be provided to driver 134D to increase the wind interceptance, unless other signals from OR gate 99 inhibited AND gate 160.
• the output of logic circuit 150 on a line 152 may be used to energize a relay drive circuit 153 and energize a relay 154 to close contacts 154A and connect auxiliary load 85 to the output lines 68 (or 90A and 90B). After a suitable time delay or from another signal suitable relays 155 may be energized to close contacts 155A to connect auxiliary load 86 into the circuit.
• the relay drive 153 may also be energized by load sensors 158.
• the adding of auxiliary loads by logic 150 may be programmed as a result of a determination that the wind veolocity sensed is great enough to provide more output than needed by the existing loads.
• Suitable meters 161 such as ammeters, volt meters or frequency meters (AC only) also are connected to the generator output lines in the system control circuit.
• the circuits used may all have time delays built in to smooth out operation.
• the power supply 94, or any battery used for power to the controls may be monitored and if failure occurs the alarm circuit will be activated and also contacts such as contacts 112C may be separately closed to decrease interception to a minimum and prevent uncontrolled operation.
• Multiple generators may be used as sequential add on units to operate in parallel as load is added.
• the controls disclosed inherently regulate the output of each generator to prevent damage from overspeed, over load and the like, and the control of wind interceptance by motor 40 provides a control to equalize the output from each of a plurality of generator assemblies.
• FIGURES 9 and 10 a modified arrangement for the drive used to change the angle of the vane assembly relative to the mounting frame is shown.
• the frame member 31 is made as previously described, except it can be a closed tube with no slot in the bottom.
• the frame 50 for the vane assembly is pivotally mounted to the bracket 26 as previously shown.
• the rotating housing 20 and the propeller 28 are previously described as well.
• the frame 31 has a pin 200 rotatably mounted about an upright axis at the outer end thereof.
• the pin 200 in turn has a bracket 201 which is mounted onto the outer housing of the motor 40.
• the bracket 201 and pin 200 permit the motor 40 to pivot about a vertical axis relative to frame 31, while supporting the motor adequately for operation.
• the output shaft 202 of the motor 40 is drivably connected to the outer end of a threaded rod 205, which is mounted in a suitable bearing 203 and is thereby guided into a tube 204.
• the tube and threaded rod take the place of the link 55 in the previous form of the invention.
• the end of tube 204 adjacent frame 50 is closed (sealed) and has a connector 207 pivotally mounted to frame 50.
• the tube 204 is sealed at its outer end by bearing 203.
• the threaded rod 205 is threaded through a block 206 fixedly mounted at a suitable location inside the tube 204.
• the rod Upon rotation of the shaft 202 when the motor 40 is driven, the rod will be threaded relative to the block and the length of the overall link assembly, including the tube 204 and the exposed end of the rod 205 can be changed to cause the angle of the tail frame 50 to change about its pivotal mounting relative to frame 50 and the generator assembly.
• OMPI in the inside for adjusting the angle of the tail provides a long life with minimum maintenance. With a sealed bearing closing up the tube (the opposite end of the tube is also closed), very little chance of any foreign material causing problems exists.
• Pivoting of the tail vane is controlled by operating a mechanism that changes the angle of the pivoting tail vane about its axis of pivot relative to the fixed frame member.
• the threaded rod can be permanently lubricated inside of the tube so that there is no need for external lubrication fittings or the like.
• limit switches 60 and 61 are relocated as shown schematically in FIGURE 9 to sense the actual position of the vane.
• the limit switches serve the same function as previously described.
• the basic generator and counterbalance arm with the swinging vane may be strictly manually operated by a mechanical linkage from the ground.
• Carriage 33 can be spring loaded toward the generator to tend to decrease wind interception, and a cable and pulley arrangement may be operable to manually pull the carriage away from the generator along the balance arm to permit increase of wind interception.
• the cable control may be operated from the ground through a winch or lever arrangement.
• the manual control would be analogous to the water pumping windmill controls used in the past.
• a swivel in the control cable may be used to accommodate ' rotation of the generator about its upright axis.
• the motor 40, the dynamic and mechanical brakes and other relays used may all be manually controlled from the ground by paralleling in manual switches to operate relays, such as relays 133 and 134, or by direct manual switches. Where necessary, the switches would be connected across slip rings to the ground operator's station.
• the motor 40 may be a DC motor if desired.
• the automatic controls disclosed permit extended unattended operation.
• the alarm circuits may be optional, and also the conditions may be monitored from a remote location.
• the alarm signals may actuate an emergency radio transmitter, or the alarm signals may be carried on transmission lines.
• Adding auxiliary load control also may be optional, as is the possibility of connecting more than one generator in parallel for increasing potential maximum output from one location. It should be noted that one generator may act as a lead unit with others picking up load sequentially as needed, or a plurality of generators may operate simultaneously, to satisfy the load demands. Load equalization is achieved by changing the wind interceptance.
• the comparators illustrated are preferably operational ampli ⁇ bombs. Integrators may be used to amplify various sensor signals prior to input to the respective comparator amplifiers.

Landscapes

• Engineering & Computer Science (AREA)
• Life Sciences & Earth Sciences (AREA)
• Sustainable Development (AREA)
• Sustainable Energy (AREA)
• Chemical & Material Sciences (AREA)
• Combustion & Propulsion (AREA)
• Mechanical Engineering (AREA)
• General Engineering & Computer Science (AREA)
• Power Engineering (AREA)
• Physics & Mathematics (AREA)
• Fluid Mechanics (AREA)
• Wind Motors (AREA)

Applications Claiming Priority (1)

Publications (2)

Family

ID=22154576

Family Applications (1)

Country Status (5)

Citations (1)

Family Cites Families (5)

• 1980
  • 1980-10-03 EP EP19810901189 patent/EP0061448A4/de not_active Withdrawn
  • 1980-10-03 GB GB8215666A patent/GB2098669A/en not_active Withdrawn
  • 1980-10-03 WO PCT/US1980/001303 patent/WO1982001221A1/en not_active Application Discontinuation
  • 1980-10-03 DE DE803050593A patent/DE3050593A1/de not_active Withdrawn
  • 1980-10-03 AU AU70739/81A patent/AU7073981A/en not_active Abandoned

Patent Citations (1)

Non-Patent Citations (1)

Also Published As

Similar Documents

Legal Events