SAE ARP 1311C-2009 起落装置结构和机理

标准号：SAE ARP 1311C-2009
中文标准名称：起落装置结构和机理
英文标准名称：Landing Gear Structures and Mechanisms
标准类型：V42
发布日期：2009/2/4 12:00:00
实施日期：1999/12/31 12:00:00
中国标准分类号：V42
国际标准分类号：49.045
引用标准：ASME B46.1-1995;MIL-PRF-5606-2006;MIL-PRF-83282-1997;MIL-PRF-87257-2004;SAE AIR 1494-1978;SAE AIR 1594-1981;SAE AIR 1752;SAE AIR 4566-1992;SAE AIR 4894-1995;SAE AIR 5358-2004;SAE AIR 5451-2005;SAE AIR 5479-2002;SAE AIR 5883-2006;SAE AMS-P-83461-1998;SAE A
适用范围：This SAE Aerospace Recommended Practice (ARP) applies to landing gear structures and mechanisms (excluding wheels, tires, and brakes and other landing gear systems) for all types and models of civil and military aircraft. All axles, wheel forks, links, arms, mechanical and gas/oil shock struts, downlock and uplock assemblies, braces, trunnion beams, and truck beams etc., that sustain loads originating at the ground, and that are not integral parts of the airframe structure, should be designed and validated in accordance with this document. Hydraulic actuators (retraction, main and nose gear steering, positioning, damping, etc.) should also be included in this coverage. System level, non-structural components such as retraction/extension valves, controllers, secondary structure and mechanisms in the airframe (e.g., manual release mechanisms, slaved doors) as well as equipment that is located in the cockpit are not addressed in this ARP. This document establishes minimum recommended design requirements and validation for landing gear structure and mechanisms. In addition, recommended guidelines regarding priorities in landing gear structural design particularly in the early design stages is provided.