49.040 有关航空航天制造用镀涂和有关工艺 标准查询与下载

SAE AMS2432D-2013 计算机控制喷丸加工

This specification establishes the requirements for computer monitored shot peening of parts surfaces by impingement of media, including metallic, glass, or ceramic shot. Computer monitored peening is intended to provide a method of process observation, traceability, and response for all process in put settings, in real time, during the entire peening process to ensure with objective evidence, the desired process outputs. Shot peening in accordance with AMS 2432 meets or exceeds the requirements of AMS 2430.

Shot Peening, Computer Monitored

BS EN 4687:2012 航空航天系列. 涂料和清漆. 军用非铬系列非腐蚀抑制双组分冷硬化底漆

Aerospace series. Paints and varnishes. Chromate free non corrosion inhibiting two components cold curing primer for military application

BS EN 4595:2013 航空航天系列. 涂料和清漆. 双组分冷固化聚氨酯罩面漆. 亚音速耐腐蚀性

Aerospace series. Paints and varnishes. Two component cold curing polyurethane finish. Subsonic erosion resistance

BS EN 4594:2013 航空航天系列.涂料和清漆.双组分冷固化聚氨酯罩面漆.超音速耐腐蚀性

Aerospace series. Paints and varnishes. Two component cold curing polyurethane finish. Supersonic erosion resistance

SAE AMS2515G-2013 聚四氟乙烯(PTFE)树脂覆膜低构造370至400℃(698至752℉)熔断器

This specification establishes the engineering requirements for producing thin coatings of polytetrafluoroethylene (PTFE) resin on parts and the properties of such coatings. Primarily to provide dry lubrication, high heat stability, and corrosion protection on parts which operate at not higher than 275 °C (527 °F) for limited periods or not higher than 245 °C (473 °C) for extended periods. This coating may also be used as a release film for molds.

Polytetrafluoroethylene (PTFE) Resin Coating, Low Build, 370 to 400°C (698 to 752°F) Fusion

SAE AMS2526D-2013 冲击应用薄润滑油膜二氧化钼涂层

This specification covers requirements for acoating consisting of finely-powdered molybdenum disulfide in a heat-resistant inorganic binder applied to parts.

Molybdenum Disulfide Coating, Thin Lubricating Film, Impingement Applied

EN 4594:2013 航空航天系列.油漆和清漆两个组件冷固化聚氨酯完成.超音速耐腐蚀性

This standard specifies the requirements for a two component polyurethane, topcoat, with a medium degree of resistance to erosion by the effects of rain, available in a range of colours and levels of gloss, to be applied over a primer for aerospace applications on areas where rain erosion at supersonic speeds may be a problem e.g. leading edges and air intakes.The properties specified in this standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 Procedure A and EN 23270 and painted with primer to EN 2435. The ability of the material to be used for a specific application (e.g. alternative substrate, alternative prim

Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Supersonic erosion resistance

EN 4595:2013 航空航天系列.油漆和清漆两个组件冷固化聚氨酯完成.亚音速耐腐蚀性

This European Standard specifies the requirements for a two component polyurethane, topcoat, with a medium degree of resistance to erosion by the effects of rain, available in a range of colours and levels of gloss, to be applied over a primer for aerospace applications on areas where rain erosion at subsonic speeds may be a problem e.g. leading edges and air intakes.The properties specified in this standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 Procedure A and EN 23270 and painted with primer to EN 2435. The ability of the material to be used for a specific application (e.g. alternative substrate, alternati

Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Subsonic erosion resistance

HB 1809-2012 套环

本标准规定了套环的结构型式、基本参数、技术要求、试验方法、检验规则、标志、包装、运输和贮存。本标准适用于航空工业起重钢索、可调起重钢索用的套环。

Ringer

HB 1810-2012 钢索夹子

本标准规定了钢索夹子的结构型式、基本参数、技术要求、检验规则、标志、包装、运输和贮存。本标准适用于航空工业可调起重钢索用的钢索夹子。

Wire rope clip

HB 1807-2012 起重钢索

本标准规定了压接头起重钢索的结构型式、基本参数、技术要求、试验方法、检验规则、标志、包装、运输和贮存。本标准适用于航空工业用压接头起重钢索。

Hoisting rope

HB 1808-2012 可调起重钢索

本标准规定了可调起重钢索的结构型式、基本参数、技术要求、试验方法、检验规则、标志、包装、运输和贮存。本标准适用于航空工业用可调起重钢索。

Adjustable hoisting rope

SAE AMS2425F-2012 电镀、热控制用黄金

This specification covers the requirements for gold deposited on metal surfaces and the properties of the deposit. This process has been used typically for passive thermal control applications where high reflectance and low absorptance of solar radiation are required, but usage is not limited to such applications.

Plating, Gold For Thermal Control

SAE AMS2406M-2012 电镀铬固体沉淀

This specification covers the engineering requirements for electrodeposited hard chromium plate and processing requirements. This plating has been used typically on parts for increasing abrasion resistance, increasing tool and die life, maintaining accuracy of gages, and reconditioning worn or undersized parts, but usage is not limited to such applications.

Plating, Chromium Hard Deposit

SAE MA4872A-2012 商用飞机除漆.材料和加工评定

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This document details the technical requirements to be used in the evaluation of materials and processes developed for use in stripping organic finishes from fixed wing commercial aircraft. The requirements herein are intended to ensure that the materials and processes used are not detrimental to the commercial aircraft when used as specified. These requirements are not intended to judge performance of the stripping method.

Paint Stripping of Commercial Aircraft - Evaluation of Materials and Process

NF L16-015:2012 航空航天系列. 涂料和清漆. 冷固化中间涂层.

Aerospace series - Paints and varnishes - Cold curing intermediate coat.

SAE AMS2451/9B-2012 低氢脆性锌-镍电镀刷

This specification covers the engineering requirements and processes for brush plating of zinc-nickel by electrodeposition. This process has been used typically to improve corrosion resistance of steel parts operating under 500 °F (260 °C) asplated or under 250 °F (121 °C) when chromate treated, to repair zinc-nickel deposits and to repair damaged or worn parts, but usage is not limited to such applications.

Plating, Brush, Zinc-Nickel Low Hydrogen Embrittlement

NF L17-306:2012 航空航天系列. 涂料和清漆. 用于军事应用方面的腐蚀抑制双组分冷固化底漆.

Aerospace series - Paints and varnishes - Corrosion inhibiting two components cold curing primer for military application.

NF L17-305:2012 航空航天系列 涂料和清漆 军用非铬系列非腐蚀抑制双组分冷硬化底漆

Aerospace series - Paints and varnishes - Chromate free non corrosion inhibiting two components cold curing primer for military application.

NF L17-307:2012 航空航天系列 涂料和清漆 双组份冷硬化聚氨酯罩面漆 军用高柔软性和耐化学剂

Aerospace series - Paints and varnishes - Two components cold curing polyurethane finish - High flexibility and chemical agent resistance for military application.