SAE ARP 1311B-1999

Aircraft Landing Gear

SAE ARP 1311B-1999 发布历史

This SAE Aerospace Recommended Practice (ARP) applies to landing gear structures and mechanisms (excluding wheels, tires, and brakes) for all types and models of civil and military aircraft including all aircraft with vertical landing and crash attenuation requirements. All axles, wheel forks, axle beams, links, arms, mechanical and nitrogen/oil energy absorbers, lock 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 in accordance with this document. Hydraulic actuators (retraction, main and nose gear steering, positioning, and/or damping) should also be included in this coverage.

SAE ARP 1311B-1999由美国机动车工程师协会 US-SAE 发布于 1999-06-01。

SAE ARP 1311B-1999在国际标准分类中归属于: 49.045 结构和结构元件。

SAE ARP 1311B-1999的历代版本如下：

• 1999年06月01日 SAE ARP 1311B-1999

SAE ARP 1311B-1999 于 2009-02-04 变更为 SAE ARP 1311C-2009 起落装置结构和机理。

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标准号

SAE ARP 1311B-1999

发布日期

1999年06月01日

实施日期

废止日期

无

国际标准分类号

49.045

发布单位

US-SAE

代替标准

SAE ARP 1311C-2009

适用范围

This SAE Aerospace Recommended Practice (ARP) applies to landing gear structures and mechanisms (excluding wheels, tires, and brakes) for all types and models of civil and military aircraft including all aircraft with vertical landing and crash attenuation requirements. All axles, wheel forks, axle beams, links, arms, mechanical and nitrogen/oil energy absorbers, lock 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 in accordance with this document. Hydraulic actuators (retraction, main and nose gear steering, positioning, and/or damping) should also be included in this coverage.