FR3054619B1 - INTEGRATED DISTRIBUTOR STABILIZER SERVO CONTROL FOR FLIGHT CONTROLS OF AN AIRCRAFT - Google Patents

INTEGRATED DISTRIBUTOR STABILIZER SERVO CONTROL FOR FLIGHT CONTROLS OF AN AIRCRAFT Download PDF

Info

Publication number
FR3054619B1
FR3054619B1 FR1601147A FR1601147A FR3054619B1 FR 3054619 B1 FR3054619 B1 FR 3054619B1 FR 1601147 A FR1601147 A FR 1601147A FR 1601147 A FR1601147 A FR 1601147A FR 3054619 B1 FR3054619 B1 FR 3054619B1
Authority
FR
France
Prior art keywords
aircraft
servo control
flight controls
integrated distributor
stabilizer
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.)
Active
Application number
FR1601147A
Other languages
French (fr)
Other versions
FR3054619A1 (en
Inventor
Thibaut MARGER
Arnaud GROLL
Clement COIC
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.)
Airbus Helicopters SAS
Original Assignee
Airbus Helicopters SAS
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 Airbus Helicopters SAS filed Critical Airbus Helicopters SAS
Priority to FR1601147A priority Critical patent/FR3054619B1/en
Publication of FR3054619A1 publication Critical patent/FR3054619A1/en
Application granted granted Critical
Publication of FR3054619B1 publication Critical patent/FR3054619B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/40—Transmitting means with power amplification using fluid pressure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24—Transmitting means
    • B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/36—Transmitting means without power amplification or where power amplification is irrelevant fluid
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/58—Transmitting means, e.g. interrelated with initiating means or means acting on blades
    • B64C27/64—Transmitting means, e.g. interrelated with initiating means or means acting on blades using fluid pressure, e.g. having fluid power amplification
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B13/00—Details of servomotor systems ; Valves for servomotor systems
    • F15B13/02—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors
    • F15B13/04—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor
    • F15B13/0401—Valve members; Fluid interconnections therefor
    • F15B13/0402—Valve members; Fluid interconnections therefor for linearly sliding valves, e.g. spool valves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B13/00—Details of servomotor systems ; Valves for servomotor systems
    • F15B13/02—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors
    • F15B13/04—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor
    • F15B13/042—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor operated by fluid pressure
    • F15B13/0422—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor operated by fluid pressure with manually-operated pilot valves, e.g. joysticks
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B13/00—Details of servomotor systems ; Valves for servomotor systems
    • F15B13/02—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors
    • F15B13/04—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor
    • F15B13/042—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor operated by fluid pressure
    • F15B13/043—Fluid distribution or supply devices characterised by their adaptation to the control of servomotors for use with a single servomotor operated by fluid pressure with electrically-controlled pilot valves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B9/00—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member
    • F15B9/02—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type
    • F15B9/08—Servomotors with follow-up action, e.g. obtained by feed-back control, i.e. in which the position of the actuated member conforms with that of the controlling member with servomotors of the reciprocatable or oscillatable type controlled by valves affecting the fluid feed or the fluid outlet of the servomotor

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Transmission Devices (AREA)
FR1601147A 2016-07-26 2016-07-26 INTEGRATED DISTRIBUTOR STABILIZER SERVO CONTROL FOR FLIGHT CONTROLS OF AN AIRCRAFT Active FR3054619B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1601147A FR3054619B1 (en) 2016-07-26 2016-07-26 INTEGRATED DISTRIBUTOR STABILIZER SERVO CONTROL FOR FLIGHT CONTROLS OF AN AIRCRAFT

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1601147 2016-07-26
FR1601147A FR3054619B1 (en) 2016-07-26 2016-07-26 INTEGRATED DISTRIBUTOR STABILIZER SERVO CONTROL FOR FLIGHT CONTROLS OF AN AIRCRAFT

Publications (2)

Publication Number Publication Date
FR3054619A1 FR3054619A1 (en) 2018-02-02
FR3054619B1 true FR3054619B1 (en) 2018-11-23

Family

ID=57209506

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1601147A Active FR3054619B1 (en) 2016-07-26 2016-07-26 INTEGRATED DISTRIBUTOR STABILIZER SERVO CONTROL FOR FLIGHT CONTROLS OF AN AIRCRAFT

Country Status (1)

Country Link
FR (1) FR3054619B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4306810A1 (en) * 2022-07-13 2024-01-17 Microtecnica S.r.l. Main control valve with integrated hydraulic scas

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3529514A (en) * 1969-03-25 1970-09-22 United Aircraft Corp Redundant servomechanism with bypass provisions
DE2855636C2 (en) * 1978-12-22 1985-08-08 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Servo control valve
DE2931533C2 (en) * 1979-08-03 1984-09-13 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Servo control system
FR3005632B1 (en) * 2013-05-17 2015-05-29 Eurocopter France DOUBLE HYDRAULIC DISTRIBUTOR OF A SERVO CONTROL FOR MANEUVERING OF THE BLADES OF A ROTOR OF GIRAVION

Also Published As

Publication number Publication date
FR3054619A1 (en) 2018-02-02

Similar Documents

Publication Publication Date Title
FR3016607B1 (en) ACTUATOR FOR CONTROLLING A HORIZONTAL STABILIZATION PLAN OF AN AIRCRAFT
FR3039643B1 (en) HUMAN-MACHINE INTERFACE FOR THE FLIGHT MANAGEMENT OF AN AIRCRAFT
FR3028836B1 (en) ACTUATOR FLIGHT CONTROL ACTUATOR OF AN AIRCRAFT
EP3398853A4 (en) Biomimetic and zoosemiotic unmanned aircraft guided by automatic pilot for precision and/or pursuit flights
IL267729A (en) Potent and short promoter for expression of heterologous genes
IL260842B1 (en) Regulation of gene expression via aptamer-mediated control of self-cleaving ribozymes
EP3492378A4 (en) Unmanned flying body and flight control method for unmanned flying body
GB2542365B (en) A method of controlling a vehicle take-off from rest
ZA202006491B (en) Flight control and navigation integrated machine
GB201900044D0 (en) Actuator assembly for moving an aircraft wing tip device
FR3033767B1 (en) DEVICE FOR CONTROLLING FLIGHT OF AN AIRCRAFT
PL3891068T3 (en) Landing guidance system for a drone
MA53107A (en) AIRCRAFT WING
GB201809534D0 (en) Vertical stabilizer for an aircraft
IL263229A (en) Altitude control along segmented track
EP3976467C0 (en) Aircraft wing control
MA50841A (en) PROCESS FOR ASSEMBLING PORTIONS OF AN AERONAUTICAL WING
FR3042660B1 (en) ELECTROMECHANICAL ACTUATOR FOR ELECTRICAL FLIGHT CONTROL OF AN AIRCRAFT
IT201700121411A1 (en) METHOD FOR THE CONTROL OF AIRCRAFT TRAFFIC
FI20165511A (en) Boom arrangement and method for controlling the tilt position of the boom arrangement
FR3050303B1 (en) SECURING THE SEQUENCING OF THE FLIGHT PLAN OF AN AIRCRAFT
GB2569851B (en) Control of diverse types of crew interface for flight control
SG11201605183VA (en) Precision guidance method and system for aircraft approaching and landing
FR3054619B1 (en) INTEGRATED DISTRIBUTOR STABILIZER SERVO CONTROL FOR FLIGHT CONTROLS OF AN AIRCRAFT
FI20150071A (en) A method of replacing a control signal of an actuator of a remote controlled flying device by another signal

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20180202

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 8