V39 燃油系统及其附件 标准查询与下载

SAE AS8040A-1996 飞机内燃换热器型加热器

This SAE Aerospace Standard (AS) covers internal combustion heat exchanger type heaters used in the following applications: a) cabin heating (all occupied regions and windshield heating); b) wing and empennage anti-icing; c) engine and accessory heating (when heater is installed as part of the aircraft); d) aircraft de-icing. This document details the minimum safety, performance, design, and testing requirements for internal combustion heaters and certain auxiliary devices that are considered necessary for the utilization of heaters in fixed and rotary wing aircraft. This standard is to be considered currently applicable and necessarily subject to revision from time to time due to advances in the aircraft industry. This standard is based on practical engineering requirements for aircraft heaters currently in use and is applicable to aircraft heaters that shall be developed to meet future requirements. The requirements of this standard are primarily intended to be applicable to civil aircraft whose primary function is transporting passengers or cargo.

Heater, Aircraft Internal Combustion Heat Exchanger Type

NAVY MIL-G-24717 NOTICE 1-1996 无海绵冷却垫圈薄片

MIL-G-24717 (SHI dated 31 March 1989, has been determined to be inact ive for new design.

GASKET, SHEET, REFRIGERATION, NON-ASBESTOS

NAVY MIL-P-17639 F (4)-1996 海军舷侧用的综合服务离心泵

This amendment forms a part of MIL-P-l7639F(SH), dated 18 February 1986,and is approved for use within the Naval Sea Systems Command, Department of the Navy and is available for use by all Departments and Agencies of the Department of Defense.

PUMPS, CENTRIFUGAL, MISCELLANEOUS SERVICE, NAVAL SHIPBOARD USE

ARMY MIL-H-48085 A NOTICE 2-1996 4.2英寸弹药的推进剂夹持器

This notice should be filed in front of MIL-H-48085A(AR) dated 6 March 1981 MIL-H-48085A dated 6 March 1981 with Validation Notice 1, dated 30 January 1987 is inactive for new design and is no longer used, except for replacement purposes.

HOLDER, PROPELLANT FOR 4.2 INCH AMMUNITION

ARMY MIL-C-13609 B REINST NOTICE 3-1996 OGK和AHH 推进剂OIA用铸造溶剂

MIL-C-13609B dated 25 November 1974 and Validation Notice 1, dated 25 April 1988 is hereby reinstated and may be used for acquisition.

CASTING SOLVENT FOR OIA, OGK AND AHH PROPELLANTS

NAVY A-A-50555-1996 全双工自动污水排放离心泵装置[取代: 海军 MIL-P-21251 E CANC 公告 1, 海军 MIL-P-21251 E, 海军 MIL-P-21251 D, 海军 MIL-P-21251 C (1), 海军 MIL-P-21251 C, 海军 MIL-P-21251 B,海军 MIL-P-21251 A]

This commercial item description covers automatic, electric-motor-driven, duplex, centrifugal, wet-pit type, sewage pumps. Capacities for each pump of the duplex unit range from 50 to 1,500 gallons per minute (gpm) (3.15 to 94.62 litershec); total dynamic heads range from 10 to 90 feet (3 048 to 27 432 mm). This commercial item description covers pumps intended for use in pumping raw sewage that carries solids fiom a sump tank or tank into a sewer at a higher level.

PUMPING UNITS, SEWAGE, DUPLEX, CENTIRFUGAL, AUTOMATIC WET-PIT TYPE [Superseded: NAVY MIL-P-21251 E CANC NOTICE 1, NAVY MIL-P-21251 E, NAVY MIL-P-21251 D, NAVY MIL-P-21251 C (1), NAVY MIL-P-21251 C, NAVY MIL-P-21251 B, NAVY MIL-P-21251 A]

SAE ARP1953A-1996 确保清洁燃料系统组件的验收测试程序和标准

To describe general guidelines for achieving selected levels of cleanliness in gas turbine engine fuel system components and to describe laboratory type methods for measuring and reporting the contamination level of the wetted portion of fuel system components. As in SAE J1227 (covering hydraulic components) this practice includes guidelines for levels of acceptance but does not attempt to set those levels. To provide standards and procedures for processing and verification to insure an acceptable level of product cleanliness in gas turbine engine fuel system components.

ACCEPTANCE TEST PROCEDURES AND STANDARDS TO INSURE CLEAN FUEL SYSTEM COMPONENTS

SAE AIR1664A-1996 飞机折叠式油罐的一般设计和安装建议

This SAE Aerospace Information Report (AIR) includes general information about the various types and styles of flexible tanks and the tank-mounted fittings that adapt the tank to the surrounding structure and fluid-system plumbing. Recommendations are given relative to the dimensional layout of the tank when these recommendations serve to avoid tank fabrication problems and tank/structure interface problems. As a part of these recommendations, critical dimensions of plumbing adapter fittings are discussed and recommendations made. Tank manufacturing tolerances are given. Recommendations are made relative to cavity design and preparation to facilitate a reliable installation. The special installation requirements of non-self-sealing, self-sealing, and crash-resistant tanks are discussed. This document is not intended to replace the information or requirements of the military and commercial procurement specifications listed in section 2. No attempt has been made, except in a very general way, to include physical property data such as weight and thickness of the composite materials available in the industry. Such materials are too numerous and vary to much between manufacturers. Whenever specific data or advice is required, it is necessary that the tank manufacturers be consulted. The purpose of this document is to supply aircraft fluid-system designers with baseline information pertinent to the application of flexible, removable tanks for power plant fluids without regard to the fluid in the tank.

AIRCRAFT FLEXIBLE TANKS GENERAL DESIGN AND INSTALLATION RECOMMENDATIONS

ARMY MIL-I-14961 REINST NOTICE 3-1996 M1A1.M2A1.M3A1.M181及M182型推进剂增量(用推进剂M8制作)

MIL-I- 1496 1 dated 17 February 1969, with Amendment 4, dated 12 October 1992 and . Validation Notice 1, dated 22 April 1988 is hereby reinstated and may be used for acquisition.

INCREMENTS, PROPELLANT M1A1, M2A1, M3A1, M181 AND M182 (MADE FROM PROPELLANT, M8)

HB 7169-1995 飞机燃油系统地面模拟试验要求

本标准规定了飞机燃油系统在研制过程中，须进行的地面模拟试验项目及其验收规则。给出了试验条件，阐明了各项试验的目的、内容、要求和试验设备、测试参数。 　　本规范规定的试验项目及验收规则，适用于军用飞机燃油系统的地面模拟试验。

Aircraft fuel system ground simulation test requirements

HB 7252-1995 民用飞机整体燃油箱通用规范

本规范规定了民用飞机整体燃油箱（以下简称整体油箱）作为贮存燃油功能的设计、性能和试验要求，不包括整体油箱作为机翼或其它结构的一部分所规定的结构强度和外形等方面的要求。 　　本规范适用于民用飞机整体油箱的设计、制造和试验。其它类型飞机可参照使用。

General specifications for integral fuel tanks of civil aircraft

HB 7170-1995 飞机燃油系统飞行试验要求

Aircraft fuel system flight test requirements

HB 7168-1995 数字式油量测量系统通用规范

本规范规定了以计算机为中心，采用线性电容式油量传感器的数字式油量测量系统（以下简称系统）的设计、性能、试验和交付的一般要求。 　　本规范适用于数字式油量测量系统的设计、试验和交付。

General specification for digital oil quantity measuring system

NAVY MIL-T-24797-1995 光纤转速计的一般规格 (海军舰载使用)(十进制)

This specification covers fiber optic tachometers capable of measuring rotational speed for use in Navy shipboard applications.

TACHOMETERS, FIBER OPTIC, (NAVAL SHIPBOARD USE), (METRIC), GENERAL SPECIFICATION FOR

NAVY MIL-G-24696 B-1995 无海绵垫圈薄片

This specification establishes the requirements of non-asbestos sheet gasket material for non-propulsion and propulsion steam and water applications and for all petroleum based hydraulic oil applications.

GASKET, SHEET, NON-ASBESTOS

HB 7116-1994 燃油电动插板开关通用规范

本标准规定了航空燃油系统所用的燃油电动插板开关（以下简称开关）的一般技术要求、试验方法和检验规则。 　　本标准适用于开关的新品研制及老产品的改进、改型。

General specification for fuel electric plug-in switch

NAVY MIL-PRF-24951 B-1995 再生燃油

This specification covers Fuel Oil, Reclaimed (Stock Number NSN 9140-01-068-6903) which is produced as a product of Navy reclamation operations (product use is described in 6.1).

FUEL OIL RECLAIMED

SAE ARP4028-1994 飞机/发动机燃油泵双相(缓动流)入口性能测试和评价

This procedure is intended to apply to all engine or airframe mounted fuel pumps and controls when required by the applicable specification. The procedure recommends a recirculation system similar to ARP492 to control the fuel properties affecting the fluid and its ability to "release" fuel vapors and dissolved air and have these "re-entrained or dissolved" during the fluid recovery process back to the tank and the original starting conditions. This SAE Aerospace Recommended Practice (ARP) defines procedures for testing aircraft/engine fuel pumps for the purpose of: a. determining two phase ("slugging flow") inlet performance capability; b. determining the pump's resistance to deterioration during an endurance test with the operating conditions defined by the applicable specification which includes two phase ("slugging flow") operation; and c. determining the effects that contaminated fuel operation may have had on two phase ("slugging flow") inlet performance. The procedure recommended herein is intended to produce useful, reproducible, steady state results. This test is not intended to establish maximum starting altitude or rate of climb performance of the pump. This procedure defines recommended test setups, test procedures, and data requirements for testing engine or airframe mounted fuel pumps or controls with pumps for the purpose of determining "slugging flow" inlet performance capability

Aircraft/Engine Fuel Pump Two Phase (Slugging Flow) Inlet Performance Test and Evaluation

NAVY MIL-F-24385 F (1)-1994 淡水和海水薄膜形成泡沫液体浓缩灭火剂(用以代替:NAVY MIL-F-0024385 E)

This amendment forms a part of MIL-F-24385F(SH), dated 07 January 1992 and is approved for use by all Departments and Agencies of the Department of Defense.

FIRE EXTINGUISHING AGENT, AQUEOUS FILM FORMING FOAM (AFFF) LIQUID CONCENTRATE, FOR FRESH AND SEAWATER [Use In Lieu Of: NAVY MIL-F-0024385 E]

HB 6778-1993 飞机燃油系统附件压降试验方法

本标准规定了HB 6507中所包含的飞机燃油系统附件的压降试验方法。 　　本标准适用于飞机燃油系统附件，也适用于其他液体输送装置的压降试验。

Aircraft fuel system accessories pressure drop test method