FR3045006B1 - Palonnier curviligne pour aeronef et aeronef comprenant un tel palonnier curviligne. - Google Patents

Palonnier curviligne pour aeronef et aeronef comprenant un tel palonnier curviligne. Download PDF

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Publication number
FR3045006B1
FR3045006B1 FR1562207A FR1562207A FR3045006B1 FR 3045006 B1 FR3045006 B1 FR 3045006B1 FR 1562207 A FR1562207 A FR 1562207A FR 1562207 A FR1562207 A FR 1562207A FR 3045006 B1 FR3045006 B1 FR 3045006B1
Authority
FR
France
Prior art keywords
palonnier
curviligne
aircraft
pedals
rails
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
FR1562207A
Other languages
English (en)
Other versions
FR3045006A1 (fr
Inventor
Bernard Guering
Laurent Saint-Marc
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 Operations SAS
Original Assignee
Airbus Operations 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 Operations SAS filed Critical Airbus Operations SAS
Priority to FR1562207A priority Critical patent/FR3045006B1/fr
Priority to US15/370,037 priority patent/US10399667B2/en
Priority to CN201611129142.3A priority patent/CN107031821B/zh
Publication of FR3045006A1 publication Critical patent/FR3045006A1/fr
Application granted granted Critical
Publication of FR3045006B1 publication Critical patent/FR3045006B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • B64C13/02—Initiating means
    • B64C13/04—Initiating means actuated personally
    • B64C13/044—Initiating means actuated personally operated by feet, e.g. pedals
    • 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
    • B64C13/02—Initiating means
    • B64C13/04—Initiating means actuated personally
    • B64C13/06—Initiating means actuated personally adjustable to suit individual persons
    • 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
    • B64C13/02—Initiating means
    • B64C13/04—Initiating means actuated personally
    • B64C13/12—Dual control apparatus
    • 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
    • B64C13/42—Transmitting means with power amplification using fluid pressure having duplication or stand-by provisions
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
    • G05G1/00—Controlling members, e.g. knobs or handles; Assemblies or arrangements thereof; Indicating position of controlling members
    • G05G1/30—Controlling members actuated by foot
    • G05G1/36—Mounting units comprising an assembly of two or more pedals, e.g. for facilitating mounting
    • 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
    • B64C13/02—Initiating means
    • B64C13/04—Initiating means actuated personally
    • B64C13/08—Trimming zero positions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42—Arrangement or adaptation of brakes
    • B64C25/44—Actuating mechanisms
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
    • G05G1/00—Controlling members, e.g. knobs or handles; Assemblies or arrangements thereof; Indicating position of controlling members
    • G05G1/30—Controlling members actuated by foot
    • G05G1/40—Controlling members actuated by foot adjustable
    • G05G1/405—Controlling members actuated by foot adjustable infinitely adjustable

Abstract

- Le palonnier (1) comprend un ensemble d'actionnement comprenant deux ensembles d'actionnement (6A, 6B) munis chacun de deux pédales (12AD, 12AG, 12BD, 12BG), chaque ensemble d'actionnement (6A, 6B) comportant un châssis (14) pourvu de deux rails (15, 16) agencés de part et d'autre dudit châssis (14) et présentant une forme de courbe concave, et associé à chacun desdits rails (15, 16), un chariot mobile (17), chacun desdits chariots mobiles (17) portant l'une desdites pédales (12AD, 12AG, 12BD, 12BG), chacun desdits chariots mobiles (17) étant configuré pour pouvoir être déplacé sur le rail (15, 16) associé, pour une commande de direction, sous une action exercée par au moins un pied d'un pilote sur au moins l'une desdites pédales (1 2AD, 12AG, 1 2BD, 12BG).
FR1562207A 2015-12-11 2015-12-11 Palonnier curviligne pour aeronef et aeronef comprenant un tel palonnier curviligne. Active FR3045006B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1562207A FR3045006B1 (fr) 2015-12-11 2015-12-11 Palonnier curviligne pour aeronef et aeronef comprenant un tel palonnier curviligne.
US15/370,037 US10399667B2 (en) 2015-12-11 2016-12-06 Curvilinear rudder bar for an aircraft and aircraft comprising such a curvilinear rudder bar
CN201611129142.3A CN107031821B (zh) 2015-12-11 2016-12-09 用于航空器的曲线型方向舵脚蹬和包括该曲线型方向舵脚蹬的航空器

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1562207A FR3045006B1 (fr) 2015-12-11 2015-12-11 Palonnier curviligne pour aeronef et aeronef comprenant un tel palonnier curviligne.
FR1562207 2015-12-11

Publications (2)

Publication Number Publication Date
FR3045006A1 FR3045006A1 (fr) 2017-06-16
FR3045006B1 true FR3045006B1 (fr) 2018-01-12

Family

ID=55411578

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1562207A Active FR3045006B1 (fr) 2015-12-11 2015-12-11 Palonnier curviligne pour aeronef et aeronef comprenant un tel palonnier curviligne.

Country Status (3)

Country Link
US (1) US10399667B2 (fr)
CN (1) CN107031821B (fr)
FR (1) FR3045006B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11167838B2 (en) 2018-05-22 2021-11-09 Airbus Operations (S.A.S.) Rudder control unit having a single-piece main module mobile on a curved support frame

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3039505B1 (fr) * 2015-07-27 2018-05-04 Airbus Helicopters Palonnier reglable et rotatif pour un aeronef a voilure tournante
FR3081438A1 (fr) * 2018-05-22 2019-11-29 Airbus Operations Module a pedale monobloc et amovible pour palonnier d'aeronef.
FR3081437A1 (fr) * 2018-05-22 2019-11-29 Airbus Operations Palonnier pour aeronef a module principal monobloc et amovible.
CN109229345B (zh) * 2018-09-25 2021-11-02 陕西飞机工业（集团）有限公司 一种防误刹车的飞机脚操纵机构
US11396362B2 (en) 2019-11-01 2022-07-26 Woodward, Inc. Rudder and brake pedal assembly
CN113460288B (zh) * 2021-09-03 2021-12-10 中国商用飞机有限责任公司 用于控制飞行器的主动式方向舵脚蹬组件以及飞行器

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US1333535A (en) * 1918-07-06 1920-03-09 Bopp Charles William Clutch-lever-lock device
US2420528A (en) * 1944-10-24 1947-05-13 Curtiss Wright Corp Rudder pedal assembly
US3359821A (en) * 1965-10-11 1967-12-26 Lockheed Aircraft Corp Connecting mechanism between a control lever and multiple controlled members
US3576302A (en) * 1968-07-10 1971-04-27 Bendix Corp Solid-state position sensor for sensing an adjusted position of a control element
US4484722A (en) * 1982-06-30 1984-11-27 The United States Of America As Represented By The Secretary Of The Air Force Translating rudder pedal system
DE3638820A1 (de) * 1986-09-12 1988-03-24 Messerschmitt Boelkow Blohm Seitenruder-steuerungsanordnung fuer luftfahrzeuge
US5056742A (en) * 1987-11-13 1991-10-15 The Boeing Company Modular rudder pedal and brake control assembly for aircraft
FR2721120B1 (fr) * 1994-06-10 1996-08-23 Guillaume Pierre Vincent Feral Véhicule du type véhicule automobile ou avion susceptible d'être conduit ou piloté par un handicapé des membres inférieurs.
US5878981A (en) * 1997-04-14 1999-03-09 Dewey; Daniel L. Flight console for radio controlled aircraft
US7690604B2 (en) * 2006-11-06 2010-04-06 Honeywell International Inc. Rudder pedal assembly including non-parallel slide rails
US8353484B2 (en) * 2009-11-10 2013-01-15 Textron Innovations, Inc. Cockpit rudder control mechanism for an aircraft
FR2956756B1 (fr) * 2010-02-23 2012-08-24 Airbus Operations Sas Dispositif generateur de couple resistif perfectionne
CN103303462B (zh) * 2012-03-09 2015-08-05 陕西飞机工业（集团）有限公司 一种立轴式脚操纵系统
EP2917102B1 (fr) * 2012-11-09 2016-09-28 Mason Electric Co. Système modulaire de commande de frein et de gouverne de direction au-dessus du plancher
US9261894B2 (en) * 2013-03-08 2016-02-16 Woodward, Inc. Multiple degrees of translational adjustment pedals
CN103587679B (zh) * 2013-11-28 2015-11-18 江西洪都航空工业集团有限责任公司 机械式飞机脚蹬调节机构
US9581226B2 (en) * 2015-05-26 2017-02-28 Woodward Mpc, Inc. Barrel cam rudder pedal system
FR3039505B1 (fr) * 2015-07-27 2018-05-04 Airbus Helicopters Palonnier reglable et rotatif pour un aeronef a voilure tournante
FR3042776B1 (fr) * 2015-10-23 2019-05-17 Airbus Operations Palonnier suspendu pour aeronef et aeronef comprenant un tel palonnier suspendu.
US10017242B2 (en) * 2016-01-29 2018-07-10 The Boeing Company Aircraft rudder pedal lockout assemblies systems and methods
FR3049573B1 (fr) * 2016-04-05 2019-05-10 Airbus Operations Commande d'aeronef comprenant une pedale amelioree

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11167838B2 (en) 2018-05-22 2021-11-09 Airbus Operations (S.A.S.) Rudder control unit having a single-piece main module mobile on a curved support frame

Also Published As

Publication number Publication date
US10399667B2 (en) 2019-09-03
CN107031821A (zh) 2017-08-11
CN107031821B (zh) 2021-11-09
US20170166296A1 (en) 2017-06-15
FR3045006A1 (fr) 2017-06-16

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