GB1398498A - Digital synchronizing and phasing system - Google Patents

Digital synchronizing and phasing system

Info

Publication number
GB1398498A
GB1398498A GB1426873A GB1426873A GB1398498A GB 1398498 A GB1398498 A GB 1398498A GB 1426873 A GB1426873 A GB 1426873A GB 1426873 A GB1426873 A GB 1426873A GB 1398498 A GB1398498 A GB 1398498A
Authority
GB
United Kingdom
Prior art keywords
governor
winding
flop
flip
magnetic
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
GB1426873A
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.)
Woodward Inc
Original Assignee
Woodward Governor 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 Woodward Governor Co filed Critical Woodward Governor Co
Publication of GB1398498A publication Critical patent/GB1398498A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D25/00Controlling two or more co-operating engines
    • F02D25/02Controlling two or more co-operating engines to synchronise speed
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/46Arrangements of, or constructional features peculiar to, multiple propellers
    • B64C11/50Phase synchronisation between multiple propellers
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02PCONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P5/00Arrangements specially adapted for regulating or controlling the speed or torque of two or more electric motors
    • H02P5/46Arrangements specially adapted for regulating or controlling the speed or torque of two or more electric motors for speed regulation of two or more dynamo-electric motors in relation to one another
    • H02P5/50Arrangements specially adapted for regulating or controlling the speed or torque of two or more electric motors for speed regulation of two or more dynamo-electric motors in relation to one another by comparing electrical values representing the speeds

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Velocity Or Acceleration (AREA)
  • High-Pressure Fuel Injection Pump Control (AREA)
  • Control Of Eletrric Generators (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)

Abstract

1398498 Automatic speed control; centrifugal governors WOODWARD GOVERNOR CO 23 March 1973 [14 June 1972] 14268/73 Headings G3B and G3R The speed of a prime mover is measured and represented as the frequency of an electrical signal which is compared with a reference frequency signal by feeding the two signals to respective inputs of a bi-stable device. The bi-stable output controls the energization of a magnetic biasing coil in a governor so as to adjust the prime mover speed to a value corresponding to the reference frequency. As shown in Fig. 1, a reference signal is provided by the shaft 23 of a master aircraft engine 21 connected to a transducer 61 supplying pulses through a Schmitt trigger circuit 75 to a differentiator 77 which supplies trigger pulses to the set input of flip-flop 79. The reset input receives similar pulses from a transducer 62 associated with a slave engine 22. The resulting rectangular signal at the set output of flip-flop 79 switches a transistor 59 into saturation for intervals whose duration determines the mean current in a winding 57a which magnetically controls the setting of a governor in the fuel supply system for the slave engine 22. In another arrangement, Fig. 5 (not shown), the winding 57a is connected across a transistor bridge and is energized alternately in opposite senses by the set and reset outputs of the flip-flop. Fig. 7 (not shown) illustrates an arrangement for manually setting a required phase relationship between the two engine shafts using an operational amplifier receiving an adjustable reference current to control the current in the magnetic winding. The phase setting may be automatically regulated by including a further operational amplifier with an integrating characteristic, Fig. 8 (not shown). A further arrangement Fig. 10 (not shown), concerns the synchronization of two engines each controlled by a governor with a magnetic biasing winding. The windings are energized by complementary signals derived respectively from the set and reset outputs of a flip-flop. The construction of the magnetic speed governor is shown in Fig. 2. Flyweights 43, 44 may be permanent magnets or magnetic material such as soft iron, and their rotation about pivots 52, 53 is controlled by a spring 49 and by the energization of a winding 57a. The position taken up by the weights determines the relative positions of a valve plunger 47 and sleeve 46 which hydraulically control a fuel servosystem for the prime mover.
GB1426873A 1972-06-14 1973-03-23 Digital synchronizing and phasing system Expired GB1398498A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US26279272A 1972-06-14 1972-06-14

Publications (1)

Publication Number Publication Date
GB1398498A true GB1398498A (en) 1975-06-25

Family

ID=22999067

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1426873A Expired GB1398498A (en) 1972-06-14 1973-03-23 Digital synchronizing and phasing system

Country Status (4)

Country Link
US (1) US3785147A (en)
JP (1) JPS5318675B2 (en)
CA (1) CA994892A (en)
GB (1) GB1398498A (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2726268B2 (en) * 1977-06-10 1980-08-28 Verkaufsgesellschaft Fuer Teererzeugnisse (Vft) Mbh, 4300 Essen Process for the manufacture of a high carbon product from waste soot
US4259376A (en) * 1977-09-16 1981-03-31 Nathan Feldstein Catalytic promoters in electroless plating catalysts applied as an emulsion
US4245955A (en) * 1978-12-14 1981-01-20 The Cessna Aircraft Company Phase and speed control system
JPS5793664A (en) * 1980-11-29 1982-06-10 Fuji Heavy Ind Ltd Phase setting system for internal combustion engine having plural power sources
FR2649797B1 (en) * 1989-07-11 1991-10-31 Valeo Equip Electr Moteur CIRCUIT FOR DETECTING THE ALTERNATOR-PHASE POLYPHASE CONTROL SIGNAL OF A MOTOR VEHICLE BATTERY CHARGE REGULATOR AND THE USE THEREOF
JPH0413033U (en) * 1990-05-11 1992-02-03
JP3922105B2 (en) * 2002-02-06 2007-05-30 株式会社デンソー Engine composite rotating electric machine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3097488A (en) * 1961-11-03 1963-07-16 Gen Electric Turbine control system
US3367110A (en) * 1966-02-01 1968-02-06 Woodward Governor Co Digital synchronizing and phase matching system
US3408549A (en) * 1966-06-24 1968-10-29 Xerox Corp Motor synchronizing system utilizing reversible counter and logic means
US3546553A (en) * 1968-09-06 1970-12-08 Nasa System for maintaining a motor at a predetermined speed utilizing digital feedback means
BE757455A (en) * 1969-10-16 1971-03-16 Westinghouse Electric Corp ANTI-RIGGING SYSTEM FOR
US3689175A (en) * 1970-08-11 1972-09-05 Piqua Aircraft Co Inc Apparatus for controlling the speed and phase of engines

Also Published As

Publication number Publication date
US3785147A (en) 1974-01-15
JPS4943084A (en) 1974-04-23
JPS5318675B2 (en) 1978-06-16
CA994892A (en) 1976-08-10

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLE Entries relating assignments, transmissions, licences in the register of patents
PCNP Patent ceased through non-payment of renewal fee