SLIDER-CRANK RETRACTABLE AIRCRAFT LANDING GEAR MECHANISM

Description

Link 1 turns about fixed axis A of the aircraft frame member. Connecting rod 2 with wheel a is connected by turning pair E to link 1 and it has roller d which slides along fixed guide b. Link 2 is connected by turning pair B to piston rod 3 of the retracting cylinder. When piston rod 3 moves into the retracting cylinder, link 1 is turned clockwise, and the landing gear is retracted as shown by the dash lines.
$1661$SC,AL$

Linked items

Documents:

Lever mechanisms [Streambook]

Permanent links

DMG-Lib		https://www.dmg-lib.org/dmglib/handler?image=17420023
Europeana		http://www.europeana.eu/portal/record/2020801/dmglib_handler_image_17420023.html

Data provider

Ilmenau TU

http://www.tu-ilmenau.de

thinkMOTION

DMG-Lib goes Europeana
The thinkMOTION project is providing content for Europeana. The digitised content is part of the Digital Mechanism and Gear Library (DMG-Lib).
Parteneri
GERMANY
Ilmenau University of Technology
Rheinisch-Westfälische Technische Hochschule Aachen
SPAIN
University of the Basque Country
ROMANIA
Politehnica University of Timisoara
FRANCE
French Institute for Advanced Mechanics
ITALY
University of Cassino

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Gesellschaft zur Förderung der Digitalen Mechanismen und Getriebebibliothek e. V.
Max-Planck-Ring 12 (Haus F), Raum 4020
98693 Ilmenau
Telefon: +49 (0)3677 691 263
Fax: +49 (0)3677 691 259

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SLIDER-CRANK RETRACTABLE AIRCRAFT LANDING GEAR MECHANISM

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