DE609362C - Cantilever suspension unit for aircraft - Google Patents

Cantilever suspension unit for aircraft

Info

Publication number
DE609362C
DE609362C DEE45606D DEE0045606D DE609362C DE 609362 C DE609362 C DE 609362C DE E45606 D DEE45606 D DE E45606D DE E0045606 D DEE0045606 D DE E0045606D DE 609362 C DE609362 C DE 609362C
Authority
DE
Germany
Prior art keywords
aircraft
suspension unit
cantilever suspension
cantilever
suspension element
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
DEE45606D
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.)
Mahle GmbH
Original Assignee
Elektronmetall GmbH
Publication date
Priority to DEE45606D priority Critical patent/DE609362C/en
Application granted granted Critical
Publication of DE609362C publication Critical patent/DE609362C/en
Expired legal-status Critical Current

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 
    • B64C25/50—Steerable undercarriages; Shimmy-damping

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Vibration Dampers (AREA)
  • Axle Suspensions And Sidecars For Cycles (AREA)

Description

*) Von dem Patentsucher ist als der Erfinder angegeben worden:*) The patent seeker stated as the inventor:

Carl König in Stuttgart.Carl König in Stuttgart.

Hierzu 1 Blatt Zeichnungen1 sheet of drawings

BERLIN. GEDRUCKT IN DEK REICHSDMJCKEKEIBERLIN. PRINTED IN DEK REICHSDMJCKEKEI

Claims (1)

Patentanspruch:Claim: Frei tragendes Federungsaggregat für Flugzeuge, bei welchem ein mit dem Flugzeug verbundener lind in der Arbeitsstellung starrer Einzelträger einen zur Aufnahme der Radachse dienenden schwenkbaren Hebel trägt, an den das Federungselement angelenkt ist, dadurch gekennzeichnet, daß das Federungselement (1, 2) im Innern des Hoblträgers (4) ohne Führungsteile für die die Stoßkräfte übertragende Druckstrebe (2) beweglich angebracht ist.Cantilever suspension unit for aircraft, in which one with the aircraft connected lind in the working position rigid single carrier one to the Receiving the wheel axle serving pivotable lever carries, to which the suspension element is articulated, thereby characterized in that the suspension element (1, 2) inside the plow carrier (4) Movable without guide parts for the pressure strut (2) transmitting the impact forces is appropriate.
DEE45606D Cantilever suspension unit for aircraft Expired DE609362C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DEE45606D DE609362C (en) Cantilever suspension unit for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEE45606D DE609362C (en) Cantilever suspension unit for aircraft

Publications (1)

Publication Number Publication Date
DE609362C true DE609362C (en) 1935-02-13

Family

ID=7080037

Family Applications (1)

Application Number Title Priority Date Filing Date
DEE45606D Expired DE609362C (en) Cantilever suspension unit for aircraft

Country Status (1)

Country Link
DE (1) DE609362C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE746423C (en) * 1941-03-04 1944-12-23 Brake device for aircraft landing gears

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE746423C (en) * 1941-03-04 1944-12-23 Brake device for aircraft landing gears

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