FR3049573B1 - Commande d'aeronef comprenant une pedale amelioree - Google Patents
Commande d'aeronef comprenant une pedale amelioree Download PDFInfo
- Publication number
- FR3049573B1 FR3049573B1 FR1652981A FR1652981A FR3049573B1 FR 3049573 B1 FR3049573 B1 FR 3049573B1 FR 1652981 A FR1652981 A FR 1652981A FR 1652981 A FR1652981 A FR 1652981A FR 3049573 B1 FR3049573 B1 FR 3049573B1
- Authority
- FR
- France
- Prior art keywords
- pedal
- rotation
- aircraft control
- axis
- support
- 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
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
- B64C13/02—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
-
- 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
- B64C27/56—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D13/08—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned the air being heated or cooled
-
- 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
-
- 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
- G05G1/48—Non-slip pedal treads; Pedal extensions or attachments characterised by mechanical features only
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Pulmonology (AREA)
- Mechanical Control Devices (AREA)
Abstract
L'invention a pour objet une commande d'aéronef de type palonnier qui comprend une pédale (32), un support (34), un premier arbre de rotation (36) reliant la pédale (32) au support (34) avec un premier axe de rotation (A36), une première liaison pivotante (38) configurée pour permettre à la pédale (32) de pivoter autour du premier axe de rotation (A36) par rapport au support (34), une bielle (40), un deuxième arbre de rotation (42) distinct du premier arbre de rotation (36) et reliant la pédale (32) à la bielle (40) avec un deuxième axe de rotation (A42), et une deuxième liaison pivotante (44) configurée pour permettre à la pédale (32) et/ou à la bielle (40) de pivoter autour du deuxième axe de rotation (A42).
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1652981A FR3049573B1 (fr) | 2016-04-05 | 2016-04-05 | Commande d'aeronef comprenant une pedale amelioree |
US15/471,450 US10669012B2 (en) | 2016-04-05 | 2017-03-28 | Aircraft control comprising an improved pedal |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1652981 | 2016-04-05 | ||
FR1652981A FR3049573B1 (fr) | 2016-04-05 | 2016-04-05 | Commande d'aeronef comprenant une pedale amelioree |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3049573A1 FR3049573A1 (fr) | 2017-10-06 |
FR3049573B1 true FR3049573B1 (fr) | 2019-05-10 |
Family
ID=56119591
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1652981A Active FR3049573B1 (fr) | 2016-04-05 | 2016-04-05 | Commande d'aeronef comprenant une pedale amelioree |
Country Status (2)
Country | Link |
---|---|
US (1) | US10669012B2 (fr) |
FR (1) | FR3049573B1 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3045006B1 (fr) * | 2015-12-11 | 2018-01-12 | Airbus Operations | Palonnier curviligne pour aeronef et aeronef comprenant un tel palonnier curviligne. |
FR3081438A1 (fr) * | 2018-05-22 | 2019-11-29 | Airbus Operations | Module a pedale monobloc et amovible pour palonnier d'aeronef. |
US11396362B2 (en) | 2019-11-01 | 2022-07-26 | Woodward, Inc. | Rudder and brake pedal assembly |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2048448A (en) * | 1933-06-28 | 1936-07-21 | Bendix Aviat Corp | Pedal construction |
US2424523A (en) * | 1943-03-06 | 1947-07-22 | Budd Co | Aircraft operating mechanism |
US7726611B2 (en) * | 2006-06-30 | 2010-06-01 | Honeywell International Inc. | Active rudder pedal mechanism with foreign object strike tolerance and articulating brake |
US9764830B2 (en) * | 2012-02-10 | 2017-09-19 | Bell Helicopter Textron Inc. | Pilot control system with adjustable pedals |
CN103605400B (zh) * | 2013-11-27 | 2015-09-16 | 连云港杰瑞电子有限公司 | 一种脚踏控制器 |
-
2016
- 2016-04-05 FR FR1652981A patent/FR3049573B1/fr active Active
-
2017
- 2017-03-28 US US15/471,450 patent/US10669012B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3049573A1 (fr) | 2017-10-06 |
US10669012B2 (en) | 2020-06-02 |
US20170283037A1 (en) | 2017-10-05 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20171006 |
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PLFP | Fee payment |
Year of fee payment: 3 |
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Year of fee payment: 4 |
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PLFP | Fee payment |
Year of fee payment: 5 |
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PLFP | Fee payment |
Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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PLFP | Fee payment |
Year of fee payment: 9 |