LINK-GEAR RETRACTABLE AIRCRAFT LANDING GEAR MECHANISM

Premi per ingrandire

Description

Link 1 with wheel a turns about fixed axis A of the aircraft frame member. Connecting rod 4 is connected by turning pair E to link 1 and its end d slides along fixed guide b. Link 4 is actuated by piston rod 2 of cylinder 3 and is connected by turning pair B to the rod. Cylinder 3 turns about fixed axis Cof the aircraft frame. When piston rod 2 moves into cylinder 3, link 1 is turned clockwise, and the landing gear is retracted as shown by the dash lines.
$1415$LG,AL$

Linked items

Documents:

Lever mechanisms [Streambook]

Permanent links

DMG-Lib		https://www.dmg-lib.org/dmglib/handler?image=17166023
Europeana		http://www.europeana.eu/portal/record/2020801/dmglib_handler_image_17166023.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).
Partner
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

Nuove fonti bibliografiche

Eventi

16th Int. Symposium on Advances in Robot Kinematics
July 01-05, 2018
Bologna, Italy

contatto

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