DE2753775A1 - Fahr- und aufhaengegestellsystem fuer ein flugzeug - Google Patents

Fahr- und aufhaengegestellsystem fuer ein flugzeug

Info

Publication number
DE2753775A1
DE2753775A1 DE19772753775 DE2753775A DE2753775A1 DE 2753775 A1 DE2753775 A1 DE 2753775A1 DE 19772753775 DE19772753775 DE 19772753775 DE 2753775 A DE2753775 A DE 2753775A DE 2753775 A1 DE2753775 A1 DE 2753775A1
Authority
DE
Germany
Prior art keywords
damping
helicopter
roll
fuselage
vertical
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
DE19772753775
Other languages
German (de)
English (en)
Other versions
DE2753775C2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html
Inventor
Irwin Jeffrey Kenigsberg
Steven Arlen Klusman
Charles Frederick Niebanck
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.)
RTX Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of DE2753775A1 publication Critical patent/DE2753775A1/de
Application granted granted Critical
Publication of DE2753775C2 publication Critical patent/DE2753775C2/de
Granted legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vehicle Body Suspensions (AREA)
  • Vibration Prevention Devices (AREA)
  • Compositions Of Oxide Ceramics (AREA)
  • Vibration Dampers (AREA)
DE19772753775 1976-12-03 1977-12-02 Fahr- und aufhaengegestellsystem fuer ein flugzeug Granted DE2753775A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/747,458 US4142698A (en) 1976-12-03 1976-12-03 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

Publications (2)

Publication Number Publication Date
DE2753775A1 true DE2753775A1 (de) 1978-06-08
DE2753775C2 DE2753775C2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1988-02-04

Family

ID=25005143

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19772753775 Granted DE2753775A1 (de) 1976-12-03 1977-12-02 Fahr- und aufhaengegestellsystem fuer ein flugzeug

Country Status (17)

Country Link
US (1) US4142698A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
JP (1) JPS6047157B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
AU (1) AU510507B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
BE (1) BE861445A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
BR (1) BR7707993A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
CA (1) CA1077454A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
CH (1) CH625173A5 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DE (1) DE2753775A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DK (1) DK536377A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
EG (1) EG14200A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
FR (1) FR2372726A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
GB (1) GB1573688A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
IL (1) IL53517A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
IT (1) IT1088386B (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
NL (1) NL186625C (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
NO (1) NO143736C (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
PL (1) PL120174B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112977806A (zh) * 2021-03-04 2021-06-18 南京航空航天大学 一种自适应行走起落架及其控制方法

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4270711A (en) * 1979-01-29 1981-06-02 Textron, Inc. Helicopter landing gear with crosstube pivot
FR2874205B1 (fr) * 2004-08-12 2006-09-15 Eurocopter France Procede et dispositif de suspension active d'un aeronef a voilure tournante
FR2959207B1 (fr) * 2010-04-26 2012-04-20 Eurocopter France Systeme a absortion d'energie pour un atterisseur, et aeronef muni dudit systeme a absorption d'energie
EP2607232B1 (en) * 2011-12-21 2014-10-29 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Landing gear vibration absorber for a helicopter and method of operating said landing gear vibration absorber
GB2524762B (en) * 2014-04-01 2020-06-17 Airbus Operations Ltd Drive system for aircraft landing gear
CA2929760C (en) * 2015-05-12 2022-01-11 Quanta Associates, L.P. Hovering aircraft belly bar clasp
US10507920B2 (en) * 2015-05-18 2019-12-17 Sikorsky Aircraft Corp. Systems and methods for lifting body vibration control
FR3069228B1 (fr) 2017-07-18 2020-07-31 Airbus Helicopters Giravion muni d'au moins un train d'atterrisage ayant au moins une roue inclinee et procede
WO2019067873A1 (en) * 2017-09-29 2019-04-04 Georgia Tech Research Corporation CABLE-DRIVEN FOUR-BAR LINK LEG MECHANISM
CN111959749B (zh) * 2020-07-16 2022-04-19 南京航空航天大学 具备地形自适应起降和行走能力的直升机四足起落架
US12060148B2 (en) 2022-08-16 2024-08-13 Honeywell International Inc. Ground resonance detection and warning system and method
US12415633B2 (en) * 2022-12-21 2025-09-16 Wing Aviation Llc Multistage suspension for UAV landing gear
US11987346B1 (en) * 2022-12-27 2024-05-21 Wing Aviation Llc UAV landing gear with shared suspension
US20250223031A1 (en) * 2024-01-08 2025-07-10 Lockheed Martin Corporation Thrust control for ground navigation of aerial vehicles

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3807668A (en) * 1971-02-04 1974-04-30 Us Federal Aviation Admin Anti-roll hydraulic analog damping device

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB441432A (en) * 1935-01-21 1936-01-20 G & J Weir Ltd Improvements in or relating to undercarriages for aircraft
US2139192A (en) * 1935-01-28 1938-12-06 Krekel Paul Aircraft undercarriage
US2326210A (en) * 1941-03-14 1943-08-10 Kellett Autogiro Corp Aircraft landing gear
GB745915A (en) * 1953-02-09 1956-03-07 British Messier Ltd Improvements in or relating to shock absorbers for aircraft
US2933270A (en) * 1954-06-04 1960-04-19 Menasco Mfg Company Landing gear for helicopters
US2933271A (en) * 1954-07-09 1960-04-19 Menasco Mfg Company Landing gear for helicopters
US2774553A (en) * 1955-04-04 1956-12-18 United Aircraft Corp Damper by-pass for lag-lead control of helicopter rotor blades
US3042345A (en) * 1957-08-05 1962-07-03 Jr Raymond Prunty Holland Control-augmenting landing gear
US3173632A (en) * 1962-07-30 1965-03-16 Del Mar Eng Lab Landing gear for hovering type aircraft

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3807668A (en) * 1971-02-04 1974-04-30 Us Federal Aviation Admin Anti-roll hydraulic analog damping device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112977806A (zh) * 2021-03-04 2021-06-18 南京航空航天大学 一种自适应行走起落架及其控制方法
CN112977806B (zh) * 2021-03-04 2022-04-22 南京航空航天大学 一种自适应行走起落架及其控制方法

Also Published As

Publication number Publication date
CA1077454A (en) 1980-05-13
DK536377A (da) 1978-06-04
NO143736B (no) 1980-12-29
NL7713354A (nl) 1978-06-06
EG14200A (en) 1983-09-30
US4142698A (en) 1979-03-06
NO143736C (no) 1981-04-08
IT1088386B (it) 1985-06-10
CH625173A5 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1981-09-15
GB1573688A (en) 1980-08-28
AU510507B2 (en) 1980-06-26
IL53517A (en) 1980-05-30
AU3116577A (en) 1979-06-07
DE2753775C2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1988-02-04
NL186625C (nl) 1991-01-16
BE861445A (fr) 1978-03-31
JPS5373799A (en) 1978-06-30
PL202598A1 (pl) 1978-07-31
BR7707993A (pt) 1978-08-15
NL186625B (nl) 1990-08-16
JPS6047157B2 (ja) 1985-10-19
FR2372726B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1983-03-25
PL120174B1 (en) 1982-02-27
NO774119L (no) 1978-06-06
FR2372726A1 (fr) 1978-06-30

Similar Documents

Publication Publication Date Title
DE2753775A1 (de) Fahr- und aufhaengegestellsystem fuer ein flugzeug
DE2923357C2 (de) Sich regelnde Aufhängungen für die Zelle eines Kraftfahrzeugs
DE2853589C2 (de) Hydropneumatischer Teleskopstoßdämpfer
DE68917601T2 (de) Regelungsvorrichtung.
DE602006000781T2 (de) Bughilfsfahrwerk, Befestigungsstruktur und Drehflügelflugzeug
DE2264015B2 (de) Dreieck-Spurketten-Anordnung
DE69107294T2 (de) Mehrachsig gestütztes Fahrwerk.
DE2311233A1 (de) Fahrzeugaufhaengung
DE2105699A1 (de) Radaufhängung an Kraftfahrzeugen
DE2632720C2 (de) Flugzeug- oder Hubschrauberfahrwerk
EP1075407A1 (de) Wankstützeinrichtung für den rahmen des laufwerks eines schienenfahrzeugs
DE4136262A1 (de) Fahrwerk eines kraftfahrzeuges
DE1028435B (de) Ausgleichsfederung fuer Fahrzeuge, insbesondere Kraftfahrzeuge
DE69515328T2 (de) Grossflugzeugfahrwerk mit achtrad-bogie
DE1153270B (de) Abfederungssystem fuer Kraftfahrzeuge
DE2164772A1 (de) Rotoraufhängung
DE1272736B (de) Um eine sich in Flugzeuglaengsrichtung erstreckende Achse einschwenkbares Flugzeugfahrwerk
DE3000606C2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DE2246881C3 (de) Laufwerk für Fahrzeuge, insbesondere Schienenfahrzeuge
DE69409729T2 (de) Hubschrauber
DE1630761A1 (de) Radaufhaengung bzw. Radabfederung der Fahrzeuge,insbesondere fuer Kraftfahrzeuge
EP3892515B1 (de) Hydropneumatische federung für ein fahrzeug
DE623257C (de) Stossdaempfer fuer Land- und Wasserflugzeuge
DE561375C (de) Landungsgestell fuer Flugzeuge
DE720214C (de) Flugzeuglandegestell mit Skiern

Legal Events

Date Code Title Description
8110 Request for examination paragraph 44
8128 New person/name/address of the agent

Representative=s name: MENGES, R., DIPL.-ING., PAT.-ANW., 8000 MUENCHEN

D2 Grant after examination
8364 No opposition during term of opposition