SAE ARP277B-2013 機首螺旋槳配件

PROPELLER ATTACHMENT - NOSE MOUNTED (Stabilized Type)

HB 20126-2012 發(fā)動機葉片坐標測量要求

本標準規(guī)定了應(yīng)用坐標測量機實施航空發(fā)動機葉片測量的方法、流程以及誤差評定要求。本標準適用于航空發(fā)動機葉片的坐標測量,其他葉片可參照執(zhí)行。

Requirements of measurement for aero-engine blades and vanes using CMM

HB 20120-2012 渦輪綜合試驗器試驗安全技術(shù)要求

本標準規(guī)定了渦輪綜合試驗器試驗的一般安全、過程安全、設(shè)備維護維修安全、應(yīng)急預(yù)案等要求。本標準適用于航空發(fā)動機渦輪部件試驗器。

Technical requirements for safety in synthetic turbine test facility

HB 6864-2011 銷釘快卸鎖

本標準規(guī)定了銷釘快卸鎖(以下簡稱鎖)的結(jié)構(gòu)和尺寸。本標準適用于飛機、直升機的機身和發(fā)動機艙口蓋及其他部件。

Pin quick-operating latch

HB 20046-2011 圓弧端齒檢驗

本標準規(guī)定了圓弧端齒檢驗原理和檢驗要求。 本標準適用于航空發(fā)動機圓弧端齒的檢驗。

Verification for curvic coupling

HB 6865-2011 滾花銷釘快卸鎖

本標準規(guī)定了滾花銷釘快卸鎖(以下簡稱鎖)的結(jié)構(gòu)和尺寸。本標準適用于飛機、直升機的機身和發(fā)電機艙口蓋及其他部件。

Embossed pin quick-operating latch

SAE ARP1827B-2009 航空器燃氣渦輪發(fā)動機精細燃料過濾器元件性能測定方法

This SAE Aerospace Recommended Practices (ARP) delineates two complementary filter element performance ratings: (1) dirt capacity, and (2) filtration efficiency, and correpsonding test procedures. It is intended for the noncleanable (disposable), fine fuel filter elements used in aviation gas turbine engine systems. Variation in filter element testing methods and requirements make comparison of results difficult. In order to minimize these problems, this document describes standard filtration ratings and test procedures. Both manufacturer and customer will have a common means to specify, control, and evaluate filter elements

Measuring Aircraft Gas Turbine Engine Fine Fuel Filter Element Performance

DIN EN 3658:2008 航空航天系列.發(fā)動機用管彎曲半徑.設(shè)計標準

This standard provides details of bend radii used in the manufacture of rigid tubes. It also provides details of the minimum length of straight permissible between such radii during manufacture. This standard applies to rigid tubes conforming to EN 3717 and produced only in ASD materials.

Aerospace series - Tube bend radii, for engine application - Design standard; German and English version EN 3658:2008

NF L43-112*NF EN 3658:2008 航空航天系列.發(fā)動機用管彎曲半徑.設(shè)計標準

Aerospace series - Tube bend radii, for engine application - Design standard.

SAE AS17107A-2007 1型標準輕型航空發(fā)電機和電動發(fā)電機主用的環(huán)形球軸承

(R) BEARING, BALL, ANNULAR, PRIMARILY FOR AIRCRAFT GENERATORS AND MOTOR-GENERATORS, STANDARD LIGHT, TYPE I

(R) BEARING, BALL, ANNULAR, PRIMARILY FOR AIRCRAFT GENERATORS AND MOTOR-GENERATORS, STANDARD LIGHT, TYPE I

SAE AS5877A-2007 航空器壓力加注嘴用詳細規(guī)范

This SAE Aerospace Standard (AS) prescribes requirements for the various types of nozzles that are used for refueling of aircraft fitted with pressure fuel servicing systems. It is to be used as a replacement for MIL-N-5877, MS29520 and for all commercial applications. Classification: The nozzles specified herein shall be classified in accordance with Table 1. Type I nozzles are primarily used by the US military services; Type II nozzles are primarily used in commercial service. Field of Application: This specification is for all nozzles that are utilized either in commercial or military applications where the aircraft system utilizes pressure fuel-servicing systems. The nozzle shall be compatible with and mate with the international aircraft adapter fitting in accordance to ISO 45 Aircraft Pressure Refueling Connections. Nozzle Configuration: The nozzle shall conform to the design interface envelope of Figure 1 of this document. The inlet configuration outside of the envelope is at the manufacturer's option and may be designed to have an angled, straight or variable configuration to meet individual requirements. The envelope restrictions are mandatory to assure that aircraft fuel system manufacturers and nozzle manufacturers have a common interface with which to work. This will assure compatibility between the available nozzles and the aircraft refueling system adapters. The nozzle may be configured to include various features and be available in various inlet configurations including, but not necessarily limited to those shown in Table 2.

Detailed Specification for Aircraft Pressure Refueling Nozzle

SAE AS5838-2006 非螺紋柔性固定空腔、載流、自粘合對焊接插座金屬箍

FEMALE FERRULE, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, SWAGED FSC 4730.Table is about DIMENSIONS AND WEIGHTS.

FEMALE FERRULE, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, SWAGED FSC 4730

SAE AS5837-2006 非螺紋柔性固定空腔、載流、自粘合對焊接插頭金屬箍

MALE FERRULE, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, BUTT WELDED FSC 4730.Table is about DIMENSIONS AND WEIGHTS.

MALE FERRULE, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, BUTT WELDED FSC 4730

SAE AS5839-2006 非螺紋柔性固定空腔、載流、自粘合對焊接插座金屬箍

FEMALE FERRULE, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, BUTT WELDED FSC 4730.Table is about DIMENSIONS AND WEIGHTS.

FEMALE FERRULE, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, BUTT WELDED FSC 4730

SAE AS5835-2006 非螺紋柔性固定空腔、載流、自粘聯(lián)軸器體

COUPLING BODY, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING FSC 4730.Table is about DIMENSIONS AND WEIGHTS /6/.

COUPLING BODY, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING FSC 4730

SAE AS5834-2006 非螺紋柔性固定空腔、載流、自粘套管

SLEEVE, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING FSC 4730.Table is about DIMENSIONS AND WEIGHTS.

SLEEVE, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING FSC 4730

SAE AS5833-2006 非螺紋柔性固定空腔、載流、自粘插型鍛頭金屬箍

MALE FERRULE, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, SWAGED FSC 4730.Table is about BASIC NO. AS5833 /12/ SIZE CODE, NOM TUBE SIZE REF and LB/EA NOM REF ALUM.

MALE FERRULE, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, SWAGED FSC 4730

SAE AS5832-2006 非螺紋撓性固定空腔、載流、自粘合組合聯(lián)軸器部件

ASSEMBLED COUPLING COMPONENTS, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING FSC 4730.Table is about ASSEMBLED COUPLING COMPONENTS WEIGHTS.

ASSEMBLED COUPLING COMPONENTS, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING FSC 4730

SAE AS5831-2006 非螺紋固定空腔、載流、自粘合撓性組合聯(lián)軸器外殼尺寸

ASSEMBLED COUPLING, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, ENVELOPE DIMENSIONS.Table is about DIMENSIONS.

ASSEMBLED COUPLING, THREADLESS-FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF BONDING, ENVELOPE DIMENSIONS

SAE AS5830-2006 非螺紋撓性固定空腔、載流、自粘合組合聯(lián)軸器采購規(guī)范

This aerospace specification defines the requirements for a threadless, flexible, conductive, self-bonding coupling assembly which, when installed on fixed cavity ferrules, provides a flexible, current carrying connection for joining tubing and components in aircraft fuel, vent and other systems. The assembled coupling is designed to provide interchangeability of parts and components between qualified manufacturers for the service life of the aircraft system. The assembled coupling is for use from -65 to +200 °F at nominal operating pressures (125 psig for -08 through -64 and 30 psig for -72 through -88). This aerospace specification is a departure from prior qualification practices for assembled couplings. Prior practice sought to validate this type of assembled coupling design by conducting a sequence of tests on sets of coupling assemblies. There were multiple test sequences and each was conducted on a different set of coupling assemblies. Each of these test sequences challenged a particular design feature of the coupling assembly. No single coupling assembly was expected to survive all of the required tests. FAR 23.954, FAR 25.954 and FAR 25.981 certification requirements have identified the need for high-current capable flexible fluid couplings. The coupling assembly does not require inspection and maintenance to remain current capable for the life of the aircraft. It is important to simulate the in-service wear and damage experienced by the assembled coupling if it is to remain capable of carrying current for the life of the aircraft. The test procedures in this specification simulate a worst case wear and damage condition for the assembled couplings. Interchangeability of vendor parts must be qualified by design, test and/or analysis.

Coupling Assembly, Threadless, Flexible, Fixed Cavity, Current Carrying, Self-Bonding, Procurement Specification FSC 4730