发明名称 Compact shock absorber for aircraft landing gear and landing gear comprising such a shock absorber
摘要 <p>The absorber has a rod (2) mounted on a main cylinder (1), and pneumatic chambers (12, 22) filled with gas. Laminating units (14, 24) are arranged such that the gas is compressed and hydraulic fluid is laminated when the absorber is pushed. The chambers are contained in auxiliary cylinders (10, 20). Pistons (11, 21) separate the pneumatic chambers from fluid chambers (13, 23) that are in fluid communication with the main cylinder. The units are integrated to the main cylinder and are placed at an inlet of fluidic connection e.g. rigid tube, between the main and auxiliary cylinders.</p>
申请公布号 EP1921341(A1) 申请公布日期 2008.05.14
申请号 EP20070291310 申请日期 2007.10.31
申请人 MESSIER-DOWTY S.A. 发明人 LAHARGOU, ANDRE;BRUNE, MARC
分类号 F16F9/48;B64C25/60 主分类号 F16F9/48
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