EP 1613531 A1 20060111 - LANDING GEAR
Title (en)
LANDING GEAR
Title (de)
FAHRWERK
Title (fr)
Train d'atterrissage
Publication
Application
Priority
- GB 2004001525 W 20040407
- GB 0308003 A 20030407
- EP 03252216 A 20030408
- EP 04726206 A 20040407
Abstract (en)
[origin: WO2004089742A1] An aircraft landing gear (1, 21) is arranged such that in its deployed position it is configured to reduce, during the approach on landing, the noise generated by the interaction of the landing gear (1, 21) and the air flowing past the landing gear. Various means are described to reduce the amount of turbulent air flow generated in the region of the landing gear (1, 21), including inverting and fairing the nose-gear shock-absorbing leg (3, 4), providing faired twin in-line oleos (2a, 2b,) and providing fairings (11) that produce shielding air curtains (24).
IPC 1-7
IPC 8 full level
B64C 7/00 (2006.01); B64C 25/16 (2006.01)
CPC (source: EP)
B64C 25/001 (2013.01); B64C 25/16 (2013.01); B64C 2025/003 (2013.01)
Citation (search report)
See references of WO 2004089742A1
Designated contracting state (EPC)
DE ES FR GB
DOCDB simple family (publication)
WO 2004089742 A1 20041021; EP 1613531 A1 20060111; EP 2239196 A2 20101013; EP 2239196 A3 20101201
DOCDB simple family (application)
GB 2004001525 W 20040407; EP 04726206 A 20040407; EP 10170885 A 20040407