Helicopter has undercarriage with skids connected by cross-bars (which are attached to fuselage by mountings whose angular rigidity varies with sinking of undercarriage as it contacts ground

Helicopter has undercarriage with skids connected by cross-bars (which are attached to fuselage by mountings whose angular rigidity varies with sinking of undercarriage as it contacts ground

The helicopter has an undercarriage (20) with skids (24, 25) which are connected by cross-bars (26, 27). These are attached to the fuselage (22) by mountings (30, 31) whose angular rigidity varies with the sinking of the undercarriage as it contacts the ground (23). L'invention concerne un gira...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: BIETENHADER CLAUDE
Format: Patent
Sprache:eng ; fre
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:The helicopter has an undercarriage (20) with skids (24, 25) which are connected by cross-bars (26, 27). These are attached to the fuselage (22) by mountings (30, 31) whose angular rigidity varies with the sinking of the undercarriage as it contacts the ground (23). L'invention concerne un giravion (21) comportant un fuselage (22) et un atterrisseur (20) à patins (24, 25) reliés par au moins une traverse (26, 27), ainsi que des moyens de liaison servant à relier la traverse au fuselage et présentant une rigidité angulaire qui varie avec l'enfoncement (E) de l'atterrisseur résultant d'un contact avec le sol (23).