CA3060742A1 - Systemes et methodes d`actionnement de conversion pour un aeronef a rotors basculants - Google Patents

Systemes et methodes d`actionnement de conversion pour un aeronef a rotors basculants Download PDF

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Publication number
CA3060742A1
CA3060742A1 CA3060742A CA3060742A CA3060742A1 CA 3060742 A1 CA3060742 A1 CA 3060742A1 CA 3060742 A CA3060742 A CA 3060742A CA 3060742 A CA3060742 A CA 3060742A CA 3060742 A1 CA3060742 A1 CA 3060742A1
Authority
CA
Canada
Prior art keywords
rod
spindle
downstop
aircraft
actuator
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.)
Granted
Application number
CA3060742A
Other languages
English (en)
Other versions
CA3060742C (fr
Inventor
Guy Bernard
Randy Aloysius
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.)
Bell Textron Rhode Island Inc
Original Assignee
Bell Textron Inc
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 Bell Textron Inc filed Critical Bell Textron Inc
Priority to CA3060742A priority Critical patent/CA3060742C/fr
Publication of CA3060742A1 publication Critical patent/CA3060742A1/fr
Application granted granted Critical
Publication of CA3060742C publication Critical patent/CA3060742C/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H25/00—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
    • F16H25/18—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
    • F16H25/20—Screw mechanisms
    • F16H2025/2043—Screw mechanisms driving an oscillating lever, e.g. lever with perpendicular pivoting axis
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H25/00—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
    • F16H25/18—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
    • F16H25/20—Screw mechanisms
    • F16H2025/2062—Arrangements for driving the actuator
    • F16H2025/2071—Disconnecting drive source from the actuator, e.g. using clutches for release of drive connection during manual control
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H25/00—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
    • F16H25/18—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
    • F16H25/20—Screw mechanisms
    • F16H2025/2062—Arrangements for driving the actuator
    • F16H2025/2075—Coaxial drive motors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H25/00—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
    • F16H25/18—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
    • F16H25/20—Screw mechanisms
    • F16H25/2003—Screw mechanisms with arrangements for taking up backlash
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H25/00—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
    • F16H25/18—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
    • F16H25/20—Screw mechanisms
    • F16H25/2015—Means specially adapted for stopping actuators in the end position; Position sensing means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H25/00—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
    • F16H25/18—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
    • F16H25/20—Screw mechanisms
    • F16H25/22—Screw mechanisms with balls, rollers, or similar members between the co-operating parts; Elements essential to the use of such members
    • F16H25/2204—Screw mechanisms with balls, rollers, or similar members between the co-operating parts; Elements essential to the use of such members with balls

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)

Abstract

Une méthode de déplacement de rotors dun aéronef entre un mode de vol et un mode daéronef comprend la rotation dun axe raccordé en relation dentraînement aux rotors autour dun axe pour déplacer les rotors entre le mode de vol et le mode daéronef jusquà ce quun composant mobile avec laxe entre en contact avec une butée de laéronef et applique une charge contre la butée. La méthode comprend le maintien du composant contre la butée pour maintenir la charge appliquée contre la butée. Il est également décrit un aéronef.
CA3060742A 2019-10-29 2019-10-29 Systemes et methodes d`actionnement de conversion pour un aeronef a rotors basculants Active CA3060742C (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA3060742A CA3060742C (fr) 2019-10-29 2019-10-29 Systemes et methodes d`actionnement de conversion pour un aeronef a rotors basculants

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA3060742A CA3060742C (fr) 2019-10-29 2019-10-29 Systemes et methodes d`actionnement de conversion pour un aeronef a rotors basculants

Publications (2)

Publication Number Publication Date
CA3060742A1 true CA3060742A1 (fr) 2021-04-29
CA3060742C CA3060742C (fr) 2023-03-28

Family

ID=75683099

Family Applications (1)

Application Number Title Priority Date Filing Date
CA3060742A Active CA3060742C (fr) 2019-10-29 2019-10-29 Systemes et methodes d`actionnement de conversion pour un aeronef a rotors basculants

Country Status (1)

Country Link
CA (1) CA3060742C (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2023033662A1 (fr) * 2021-09-06 2023-03-09 Rebielak Janusz Avion à décollage et atterrissage verticaux
WO2024076966A1 (fr) * 2022-10-06 2024-04-11 Archer Aviation, Inc. Trajet de charge redondant pour actionneur d'inclinaison de levage motorisé

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2023033662A1 (fr) * 2021-09-06 2023-03-09 Rebielak Janusz Avion à décollage et atterrissage verticaux
WO2024076966A1 (fr) * 2022-10-06 2024-04-11 Archer Aviation, Inc. Trajet de charge redondant pour actionneur d'inclinaison de levage motorisé

Also Published As

Publication number Publication date
CA3060742C (fr) 2023-03-28

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