FR2874205B1 - Procede et dispositif de suspension active d'un aeronef a voilure tournante - Google Patents

Procede et dispositif de suspension active d'un aeronef a voilure tournante

Info

Publication number
FR2874205B1
FR2874205B1 FR0408843A FR0408843A FR2874205B1 FR 2874205 B1 FR2874205 B1 FR 2874205B1 FR 0408843 A FR0408843 A FR 0408843A FR 0408843 A FR0408843 A FR 0408843A FR 2874205 B1 FR2874205 B1 FR 2874205B1
Authority
FR
France
Prior art keywords
wing aircraft
rotary wing
active suspension
suspension
active
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.)
Expired - Fee Related
Application number
FR0408843A
Other languages
English (en)
Other versions
FR2874205A1 (fr
Inventor
Brice Makinadjian
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
Eurocopter France SA
Eurocopter SA
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 Eurocopter France SA, Eurocopter SA filed Critical Eurocopter France SA
Priority to FR0408843A priority Critical patent/FR2874205B1/fr
Priority to US11/188,725 priority patent/US7720582B2/en
Publication of FR2874205A1 publication Critical patent/FR2874205A1/fr
Application granted granted Critical
Publication of FR2874205B1 publication Critical patent/FR2874205B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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 
    • B64C25/58—Arrangements or adaptations of shock-absorbers or springs
    • B64C25/60—Oleo legs
    • 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 
    • B64C2025/325—Alighting gear characterised by elements which contact the ground or similar surface  specially adapted for helicopters
FR0408843A 2004-08-12 2004-08-12 Procede et dispositif de suspension active d'un aeronef a voilure tournante Expired - Fee Related FR2874205B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0408843A FR2874205B1 (fr) 2004-08-12 2004-08-12 Procede et dispositif de suspension active d'un aeronef a voilure tournante
US11/188,725 US7720582B2 (en) 2004-08-12 2005-07-26 Active suspension method and apparatus for a rotary wing aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0408843A FR2874205B1 (fr) 2004-08-12 2004-08-12 Procede et dispositif de suspension active d'un aeronef a voilure tournante

Publications (2)

Publication Number Publication Date
FR2874205A1 FR2874205A1 (fr) 2006-02-17
FR2874205B1 true FR2874205B1 (fr) 2006-09-15

Family

ID=34948264

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0408843A Expired - Fee Related FR2874205B1 (fr) 2004-08-12 2004-08-12 Procede et dispositif de suspension active d'un aeronef a voilure tournante

Country Status (2)

Country Link
US (1) US7720582B2 (fr)
FR (1) FR2874205B1 (fr)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0608744D0 (en) * 2006-05-03 2006-06-14 Airbus Uk Ltd Landing Gear Ground Test
US8285447B2 (en) * 2007-03-20 2012-10-09 Enpulz, L.L.C. Look ahead vehicle suspension system
US8428819B2 (en) * 2007-08-31 2013-04-23 GM Global Technology Operations LLC Suspension system with optimized damper response for wide range of events
FR2922190B1 (fr) * 2007-10-11 2010-04-09 Eurocopter France Verin de retraction, atterrisseur de giravion muni d'un tel verin de retraction
US9708057B2 (en) * 2014-02-24 2017-07-18 The Boeing Company Active landing gear damper
US9303709B2 (en) 2014-08-11 2016-04-05 Ggodrich Corporation Shock damper
CN105480431B (zh) * 2014-10-11 2017-10-31 中国航空工业集团公司西安飞机设计研究所 一种避免起落架离地状态过度振动的方法
CA2929760C (fr) * 2015-05-12 2022-01-11 Quanta Associates, L.P. Crochet de barre de ventre d'aeronef en vol stationnaire
US10507920B2 (en) * 2015-05-18 2019-12-17 Sikorsky Aircraft Corp. Systems and methods for lifting body vibration control
WO2016210265A1 (fr) 2015-06-25 2016-12-29 Sikorsky Aircraft Corporation Ensemble train d'atterrissage adaptatif pour aéronef à voilure tournante
US11066172B2 (en) 2015-10-15 2021-07-20 The Boeing Company Controlled energy absorption of seats for impact
GB2569175A (en) * 2017-12-08 2019-06-12 Airbus Operations Ltd Aircraft with active support
PL73389Y1 (pl) * 2018-02-08 2024-03-11 Vita Inclinata Tech Inc Urządzenie do stabilizacji zawieszonego ładunku
US11209836B1 (en) 2018-02-08 2021-12-28 Vita Inclinata Technologies, Inc. Long line loiter apparatus, system, and method
US11142316B2 (en) 2018-02-08 2021-10-12 Vita Inclinata Technologies, Inc. Control of drone-load system method, system, and apparatus
US11945697B2 (en) 2018-02-08 2024-04-02 Vita Inclinata Ip Holdings Llc Multiple remote control for suspended load control equipment apparatus, system, and method
US11142433B2 (en) 2018-02-08 2021-10-12 Vita Inclinata Technologies, Inc. Bidirectional thrust apparatus, system, and method
US10940061B2 (en) 2018-02-08 2021-03-09 Vita Inclinata Technologies, Inc. Modular suspended load control apparatuses, systems, and methods
US10946979B2 (en) 2018-04-13 2021-03-16 The Boeing Company Apparatus for controlling vehicle impact absorption systems and related methods
WO2020176665A1 (fr) 2019-02-26 2020-09-03 Vita Inclinata Technologies, Inc. Appareil de déploiement de câble, système et procédés pour équipement de contrôle de charge suspendue
US11618566B1 (en) 2019-04-12 2023-04-04 Vita Inclinata Technologies, Inc. State information and telemetry for suspended load control equipment apparatus, system, and method
US11834305B1 (en) 2019-04-12 2023-12-05 Vita Inclinata Ip Holdings Llc Apparatus, system, and method to control torque or lateral thrust applied to a load suspended on a suspension cable
EP3725671B1 (fr) * 2019-04-15 2023-09-27 Safran Landing Systems UK Ltd Aéronef ayant un train d'atterrissage à stabilisateur
CA3148446A1 (fr) 2019-07-21 2021-01-28 Vita Inclinata Technologies, Inc. Appareil, systeme et procede de treuil et d'equipement deployable
US11620597B1 (en) 2022-04-29 2023-04-04 Vita Inclinata Technologies, Inc. Machine learning real property object detection and analysis apparatus, system, and method

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1279981A (en) * 1969-05-07 1972-06-28 Terence Walshaw An improvement in or relating to hydraulic dampers
US3716208A (en) * 1970-06-11 1973-02-13 Textron Inc Energy absorbing landing gear
US4142698A (en) * 1976-12-03 1979-03-06 United Technologies Corporation Improved aircraft suspension system with mechanism operable to establish system vertical stiffness and damping and mechanism operationally independent thereof to establish system roll stiffness and damping
US4519559A (en) * 1979-12-26 1985-05-28 Hughes Helicopters, Inc. Landing gear energy distribution and righting system
DE3414258A1 (de) * 1984-04-14 1985-10-24 Robert Bosch Gmbh, 7000 Stuttgart Vorrichtung zum steuern der federhaerte eines fahrzeugs i
US5231583A (en) * 1990-06-08 1993-07-27 Monroe Auto Equipment Company Method and apparatus for dynamic leveling of a vehicle using an active suspension system
US5276622A (en) * 1991-10-25 1994-01-04 Lord Corporation System for reducing suspension end-stop collisions
JPH10278529A (ja) * 1997-04-08 1998-10-20 Unisia Jecs Corp 車両懸架装置
US6120009A (en) * 1998-04-16 2000-09-19 The Boeing Company Shock strut with managed damping and force characteristics
US6885917B2 (en) * 2002-11-07 2005-04-26 The Boeing Company Enhanced flight control systems and methods for a jet powered tri-mode aircraft

Also Published As

Publication number Publication date
US20070032931A1 (en) 2007-02-08
US7720582B2 (en) 2010-05-18
FR2874205A1 (fr) 2006-02-17

Similar Documents

Publication Publication Date Title
FR2874205B1 (fr) Procede et dispositif de suspension active d'un aeronef a voilure tournante
FR2884605B1 (fr) Procede et dispositif de surveillance d'une structure d'un avion
FR2894368B1 (fr) Dispositif et procede de construction automatisee de trajectoire d'urgence pour aeronefs
FR2904461B1 (fr) Procede et dispositif d'affichage d'un plan de vol d'un aeronef
FR2890867B1 (fr) Dispositif et procede d'assistance respiratoire
FR2894045B1 (fr) Procede de controle de parametres de decollage ou d'atterrissage et dispositif associe
FR2861871B1 (fr) Procede de suivi du deroulement du plan de vol d'un aeronef cooperatif
FI20030647A (fi) Menetelmä ja laite ihmisen painon hallintaan
FR2863070B1 (fr) Procede et dispositif d'interface homme - machine
FR2861051B1 (fr) Procede de guidage d'un aeronef en phase d'approche et balise sol correspondante
FR2909462B1 (fr) Procede et dispositif de controle actif du tangage d'un avion.
FR2870604B1 (fr) Procede et dispositif de securisation d'un vol a basse altitude d'un aeronef
FR2911689B1 (fr) Procede et dispositif de controle de la vitesse d'un aeronef
FR2909463B1 (fr) Procede et dispositif de controle actif du roulis d'un avion
FR2861325B1 (fr) Procede et dispositif d'usinage de panneaux
FR2861206B1 (fr) Procede et dispositif d'adaptation automatique d'affichage
FR2902080B1 (fr) Dispositif et procede de suveillance d'un aeronef
FR2858252B1 (fr) Dispositif et procede d'enduction
FR2883088B1 (fr) Dispositif et procede de suivi d'aeronefs
IL173996A (en) Method for photographing on board of a flying rotating body and system for carrying out said method
FR2873094B1 (fr) Procede et dispositif d'amelioration de la manoeuvrabilite d'un aeronef lors des phases d'approche avant l'atterrissage puis d'arrondi
FR2922641B1 (fr) Procede et dispositif de recalage de la position d'un aeronef.
FR2875900B1 (fr) Procede et dispositif de mesure de l'orientation du train d'atterrissage avant d'un avion
FR2855895B1 (fr) Procede et dispositif de lutte contre le vol d'un appareil de radiocommunication
FR2872904B1 (fr) Procede et dispositif de controle de l'integrite d'un recipient

Legal Events

Date Code Title Description
CD Change of name or company name

Owner name: AIRBUS HELICOPTERS, FR

Effective date: 20140602

PLFP Fee payment

Year of fee payment: 13

PLFP Fee payment

Year of fee payment: 14

PLFP Fee payment

Year of fee payment: 15

PLFP Fee payment

Year of fee payment: 16

PLFP Fee payment

Year of fee payment: 17

ST Notification of lapse

Effective date: 20220405