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DE460965C - Undercarriage for aircraft - Google Patents

Undercarriage for aircraft

Info

Publication number
DE460965C
DE460965C DED47406D DED0047406D DE460965C DE 460965 C DE460965 C DE 460965C DE D47406 D DED47406 D DE D47406D DE D0047406 D DED0047406 D DE D0047406D DE 460965 C DE460965 C DE 460965C
Authority
DE
Germany
Prior art keywords
aircraft
wheels
fuselage
undercarriage
shafts
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
Application number
DED47406D
Other languages
German (de)
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.)
Daimler Benz AG
Original Assignee
Daimler Benz AG
Publication date
Priority to DED47406D priority Critical patent/DE460965C/en
Application granted granted Critical
Publication of DE460965C publication Critical patent/DE460965C/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C35/00—Flying-boats; Seaplanes
    • B64C35/008—Amphibious sea planes

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Dampers (AREA)

Description

Fahrgestell für Flugzeuge. Die Erfindung bezieht sich auf ein Fahrgestell für Flugzeuge, bei welchem die Stützorgane, Laufräder u. dgl. um eine quer zum Rumpf liegende Welle verschwenkbar sind, zu dem Zweck, die Räder für das Niedergehen des Flugzeugs auf dem Wasser hochzuziehen.Undercarriage for aircraft. The invention relates to a chassis for aircraft in which the supporting elements, running wheels and the like are arranged at right angles to the fuselage horizontal shaft are pivotable for the purpose of the wheels for the fall of the Airplane pulling up on the water.

Die Erfindung besteht in der Hauptsache darin, daß die Schwenkwellen mit Zapfen in feststehende, schraubengangartige Führungen eingreifen und sich gegen Pufferfedern oder Gummipuffer stützen, welche die auf die Räder einwirkenden Stöße infolge hierbei eintretender Längsverschiebung der Schwenkwelle aufnehmen und die Rückführung der aufgezogenen Stützorgane in die Fahrtstellung bewirken. Zweckmäßig werden die Wellen in an sich bekannten, seitlich am Rumpf befestigten Auslegern gelagert.The invention consists mainly in that the pivot shafts engage with pins in fixed, helical guides and against Buffer springs or rubber buffers support the impacts on the wheels record as a result of this occurring longitudinal displacement of the pivot shaft and the Bring back the raised support members in the driving position. Appropriate the waves are in known, laterally attached to the fuselage brackets stored.

Gegenüber den bekannten Ausführungen zeichnet sich die Erfindung hauptsächlich durch ihre Einfachheit und Zweckmäßigkeit aus.Compared to the known designs, the invention is mainly characterized characterized by their simplicity and practicality.

Auf der Zeichnung ist ein Ausführungsbeispiel der Erfindung in einer Abbildung dargestellt. Die Schwenkwelle für die Laufräder e ist in zwei Teile c2 zerlegt. Die Wellenteile stützen sich auf Pufferfedern f2 und greifen in schräge Führungen i ein. Zum Verdrehen der Wellen c2 um ihre Achse und zum Hochziehen der Laufräder ist an geeigneter Stelle, beispielsweise innerhalb des Rumpfes a, ein Hebel g2 aufgesetzt.In the drawing, an embodiment of the invention is in a Figure shown. The pivot shaft for the wheels e is in two parts c2 disassembled. The shaft parts are supported on buffer springs f2 and grip obliquely Guided tours i a. To rotate the shafts c2 about their axis and to pull up the Impellers is at a suitable location, for example within the fuselage a Lever g2 put on.

Claims (2)

PATENTANSPRÜCHE: I. Fahrgestell für Flugzeuge, bei welchem die Stützorgane, Laufräder u. dgl. um eine quer zum Rumpf liegende Welle verschwenkbar sind, zu dem Zweck, die Räder für das Niedergehen des Flugzeugs auf dem Wasser hochzuziehen, dadurch gekennzeichnet, daß die Schwenkwellen mit Zapfen in feststehende, schraubengangartige Führungen eingreifen und sich gegen Pufferfedern oder Gummipuffer stützen, welche die auf die Räder einwirkenden Stöße infolge hierbei eintretender Längsverschiebung der Schwenkwelle aufnehmen und die Rückführung der aufgezogenen Stützorgane in die Fahrtstellung bewirken. PATENT CLAIMS: I. Undercarriage for aircraft, in which the supporting elements, Impellers and the like can be pivoted about a shaft lying transversely to the fuselage, to which Purpose of pulling the wheels up for the plane to descend on the water, characterized in that the pivot shafts with pins in fixed, helical Engage guides and support themselves against buffer springs or rubber buffers, which the impacts acting on the wheels as a result of the longitudinal displacement occurring here record the pivot shaft and the return of the drawn support members in the Cause driving position. 2. Fahrgestell für Flugzeuge nach Anspruch I, dadurch gekennzeichnet, daß die Wellen in an sich bekannten, seitlich am Rumpf befestigten Auslegern gelagert sind. 2. Chassis for aircraft according to claim I, characterized in that the shafts are mounted in known, laterally attached to the fuselage arms.
DED47406D Undercarriage for aircraft Expired DE460965C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DED47406D DE460965C (en) Undercarriage for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DED47406D DE460965C (en) Undercarriage for aircraft

Publications (1)

Publication Number Publication Date
DE460965C true DE460965C (en) 1928-06-04

Family

ID=7050406

Family Applications (1)

Application Number Title Priority Date Filing Date
DED47406D Expired DE460965C (en) Undercarriage for aircraft

Country Status (1)

Country Link
DE (1) DE460965C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3128971A (en) * 1964-04-14 Aircraft landing gear

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3128971A (en) * 1964-04-14 Aircraft landing gear

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