FR2356210A1 - MULTIPLE PARAMETER DISPLAY SYSTEM, USEFUL IN PARTICULAR FOR CONTROL OF AIRCRAFT ENGINES - Google Patents

MULTIPLE PARAMETER DISPLAY SYSTEM, USEFUL IN PARTICULAR FOR CONTROL OF AIRCRAFT ENGINES

Info

Publication number
FR2356210A1
FR2356210A1 FR7719336A FR7719336A FR2356210A1 FR 2356210 A1 FR2356210 A1 FR 2356210A1 FR 7719336 A FR7719336 A FR 7719336A FR 7719336 A FR7719336 A FR 7719336A FR 2356210 A1 FR2356210 A1 FR 2356210A1
Authority
FR
France
Prior art keywords
control
display system
engines
useful
aircraft engines
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.)
Withdrawn
Application number
FR7719336A
Other languages
French (fr)
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.)
Smiths Group PLC
Original Assignee
Smiths Group PLC
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 Smiths Group PLC filed Critical Smiths Group PLC
Publication of FR2356210A1 publication Critical patent/FR2356210A1/en
Withdrawn legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G07CHECKING-DEVICES
    • G07CTIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
    • G07C3/00Registering or indicating the condition or the working of machines or other apparatus, other than vehicles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00Arrangements or adaptations of instruments
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01DMEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D1/00Measuring arrangements giving results other than momentary value of variable, of general application
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01DMEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D7/00Indicating measured values

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Testing And Monitoring For Control Systems (AREA)
  • Arrangements For Transmission Of Measured Signals (AREA)

Abstract

Système d'affichage analogique et numérique de plusieurs paramètres. Il comprend des détecteurs 1 qui produisent des signaux selon les valeurs de certains parametres de moteurs M1 à M4, par exemple des quatre moteurs d'un aéronef. Ces signaux sont transmis par un dispositif 2 et un étage tampon 3 à un multiplexeur commun 4, puis à un calculateur 5 qui compare ces signaux à des informations placées dans une mémoire 6 et qui transmet le résultat de ces comparaisons à un dispositif 7 d'affichage. Ce dispositif comporte un organe 8 à aiguille produisant un affichage analogique, et des organes 9 et 10 produisant un affichage numérique. Domaine d'application : contrôle des moteurs d'aéronefs.Analog and digital display system of several parameters. It comprises detectors 1 which produce signals according to the values of certain parameters of engines M1 to M4, for example of the four engines of an aircraft. These signals are transmitted by a device 2 and a buffer stage 3 to a common multiplexer 4, then to a computer 5 which compares these signals with information placed in a memory 6 and which transmits the result of these comparisons to a device 7 of display. This device comprises a needle member 8 producing an analog display, and members 9 and 10 producing a digital display. Field of application: control of aircraft engines.

FR7719336A 1976-06-24 1977-06-23 MULTIPLE PARAMETER DISPLAY SYSTEM, USEFUL IN PARTICULAR FOR CONTROL OF AIRCRAFT ENGINES Withdrawn FR2356210A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2641776A GB1578535A (en) 1976-06-24 1976-06-24 Display systems for displaying measurements

Publications (1)

Publication Number Publication Date
FR2356210A1 true FR2356210A1 (en) 1978-01-20

Family

ID=10243334

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7719336A Withdrawn FR2356210A1 (en) 1976-06-24 1977-06-23 MULTIPLE PARAMETER DISPLAY SYSTEM, USEFUL IN PARTICULAR FOR CONTROL OF AIRCRAFT ENGINES

Country Status (2)

Country Link
FR (1) FR2356210A1 (en)
GB (1) GB1578535A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2663117A1 (en) * 1990-06-07 1991-12-13 Notion Progres Sarl Device acting as a tachometer and revolution counter, making it possible to continuously visualise the harmony between gear and speed
FR2674327A1 (en) * 1991-03-19 1992-09-25 Jaeger Improved indicator device with pointer
EP2006202A1 (en) * 2007-06-20 2008-12-24 Eurocopter Method and device for testing and regulating a turboshaft engine of a rotorcraft
FR2946020A1 (en) * 2009-06-02 2010-12-03 Airbus France DEVICE FOR CONFIRMING THE PUSH OF ENGINES OF AN AIRCRAFT.

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT1160818B (en) * 1983-03-22 1987-03-11 Rockwell Rimoldi Spa INSTRUMENT FOR THE PROCESSING OF DATA HAND AND DETECTED WITH AUTOMATIC EXECUTION OF THE CHECK CARD FOR AVERAGE (X) AND EXCURSION (W)
DE3315386A1 (en) * 1983-04-28 1984-10-31 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Display device for the pictorial representation of measurement values
SE451446B (en) * 1983-09-20 1987-10-12 Volvo Penta Ab BATAR TRIM INDICATOR WITH OUTBOARD PROPELLER DRIVE
DE3524886A1 (en) * 1985-07-12 1987-01-22 Vdo Schindling MEASURING CIRCUIT ARRANGEMENT FOR AN ELECTRICAL PROCESSOR
DE4011840A1 (en) * 1989-04-19 1990-10-25 Volkswagen Ag Display unit for several physical parameters - uses graphical, numeral and colour variation indication to enable easy monitoring of values w.r.t. acceptable ranges
US9950805B2 (en) * 2015-10-26 2018-04-24 The Boeing Company Aircraft engine fan speed display improvements for enhanced monitoring and thrust setting ability

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2663117A1 (en) * 1990-06-07 1991-12-13 Notion Progres Sarl Device acting as a tachometer and revolution counter, making it possible to continuously visualise the harmony between gear and speed
FR2674327A1 (en) * 1991-03-19 1992-09-25 Jaeger Improved indicator device with pointer
EP2006202A1 (en) * 2007-06-20 2008-12-24 Eurocopter Method and device for testing and regulating a turboshaft engine of a rotorcraft
FR2917715A1 (en) * 2007-06-20 2008-12-26 Eurocopter France METHOD AND DEVICE FOR MONITORING AND CONTROLLING A GYRANE TURBOMOTOR
US8050842B2 (en) 2007-06-20 2011-11-01 Eurocopter Method and apparatus for controlling and regulating a rotorcraft turbine engine
FR2946020A1 (en) * 2009-06-02 2010-12-03 Airbus France DEVICE FOR CONFIRMING THE PUSH OF ENGINES OF AN AIRCRAFT.

Also Published As

Publication number Publication date
GB1578535A (en) 1980-11-05

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Legal Events

Date Code Title Description
ST Notification of lapse