V39 燃油系统及其附件 标准查询与下载
共找到 351 条与 燃油系统及其附件 相关的标准，共 24 页
This specification covers the requirements for two grades and two types of argon.
PROPELLANT PRESSURIZING AGENT, ARGON
- ICS
- 49.140
- CCS
- V39
- 发布
- 2007-02-08
- 实施
The documents listed in this section are specified in sections 3, 4, or 5 of this specification. This section does not include documents cited in other sections of this specification or recommended for additional information or as examples. While every
PROPELLANT, HYDROGEN
- ICS
- 49.140
- CCS
- V39
- 发布
- 2007-02-07
- 实施
MIL-PRF-24755A, dated 31 May 2001, has been reviewed and determined to be valid for use in acquisition.
FANS, VANEAXIAL, HIGH PRESSURE, NAVAL SHIPBOARD
- ICS
- 49.020
- CCS
- V39
- 发布
- 2007-01-23
- 实施
MIL-PRF-19004B, dated 25 May 2001, has been reviewed and determined to be valid for use in acquisition.
Fans, Centrifugal, Ventilation, Naval Shipboard
- ICS
- 49.020
- CCS
- V39
- 发布
- 2007-01-22
- 实施
This list has been prepared for use by or for the Government in the acquisition of products covered by the subject specification and such listing of a product is not intended to and does not connote endorsement of the product by the Department of Defense.
FIRE EXTINGUISHING AGENT, AQUEOUS FILM-FORMING FOAM (AFFF) LIQUID CONCENTRATE, FOR FRESH AND SEA WATER
- ICS
- 49.020
- CCS
- V39
- 发布
- 2007-01-03
- 实施
This SAE Aerospace Standard (AS) defines the requirements for a threaded flexible coupling assembly, which utilizes ferrules or machined tube end fittings to join tubing and components in aircraft fuel and fuel vent or other systems. This coupling assembly is designed for use from -65 to +200 °F and at 125 psig peak working pressure, and the coupling assembly may be used in other fluid systems when requirements are within the limits.
Coupling, Fuel, Flexible, Variable Cavity Threaded Type With Ferrules
- ICS
- 49.050
- CCS
- V39
- 发布
- 2006-08-01
- 实施
Maximum test limits are based upon material bonded to a non-combustible substrate
FIRE PERFORMANCE REQUIREMENTS AND APPROVED SPECIFICATIONS FOR INTERIOR FINISH MATERIALS AND FURNISHINGS (NAVAL SHIPBOARD USE)
- ICS
- 49.020
- CCS
- V39
- 发布
- 2006-06-20
- 实施
本规范规定了飞机燃油系统的设计、性能、安装和试验要求。 本规范适用于以空气发动机作动力的军用飞机燃油系统的设计、制造和试验，也适用于后勤保障、装备维修与改进。直升机可参照使用。
General specification for aircraft fuel system
- ICS
- CCS
- V39
- 发布
- 2006-05-17
- 实施
- 2006-10-01
Refrigeration Oil Description
Refrigeration Oil Description
- ICS
- CCS
- V39
- 发布
- 2006-01-21
- 实施
This SAE Aerospace Recommended Practice contains general criteria for the planning, design, and construction of military and commercial ground based aviation fueling facilities that receive, store, distribute, and dispense liquid aviation turbine fuels at airports. Its purpose is to provide a description of practices that are commonly recognized throughout the industry as proving beneficial in the planning, design, and construction of aviation fuel systems at airports. The purpose of any aviation fueling system is to safely deliver clean, dry, on specification fuel to an aircraft. As is true for any type of system, there are peculiarities inherent to handling aviation fuels that are not readily apparent to anyone who does not design, build, or use these systems regularly. Aviation fueling systems represent a barely measurable percentage of the overall construction industry; there are therefore very few companies or individuals who are aware of these peculiarities. With both the commercial airlines and the military going through a protracted cycle of downsizing and outsourcing, the portion of the industry that pays for and is ultimately responsible for these systems is losing many of its most experienced personnel. The purpose of this guide is to provide key individuals who are responsible for aviation fuel facilities an overview of general practices which have proven beneficial in planning, design, and construction.
Aviation Fuel Facilities
- ICS
- 49.050
- CCS
- V39
- 发布
- 2006-01-01
- 实施
The documents listed in this section are specified in sections 3, 4, or 5 of this specification. This section does not include documents cited in other sections of this specification or recommended for additional information or as examples. While every
PROPELLANT, HIGH DENSITY SYNTHETIC HYDROCARBON TYPE, GRADE JP-10
- ICS
- 49.140
- CCS
- V39
- 发布
- 2006
- 实施
The documents listed in this section are specified in sections 3, 4, or 5 of this specification. This section does not include documents cited in other sections of this specification or recommended for additional information or as examples. While every ef
PROPELLANT PRESSURIZING AGENT, HELIUM
- ICS
- 49.140
- CCS
- V39
- 发布
- 2006
- 实施
This specification covers two types and three grades of propellant methane.
PROPELLANT, METHANE
- ICS
- 49.140
- CCS
- V39
- 发布
- 2006
- 实施
本规范规定了航空燃油－滑油热交换器的通用技术要求、质量保证规定和交货准备。 本规范适用于航空燃油－滑油热交换器（简称热交换器）的设计、试验与验收。
General specification for aviation heatexchanger for fuel-oil
- ICS
- CCS
- V39
- 发布
- 2005-12-12
- 实施
- 2006-05-01
The activities listed above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information using the ASSIST Online database at http://assist.daps.dla
PROPELLANT, NITROGEN TRIFLUORIDE
- ICS
- 49.140
- CCS
- V39
- 发布
- 2005
- 实施
The activities listed above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information using the ASSIST Online database at http://assist.daps.dla
PROPELLANT, DEUTERIUM
- ICS
- 49.140
- CCS
- V39
- 发布
- 2005
- 实施
The activities listed above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information using the ASSIST database at http://assist.daps.dla.mil.
PROPELLANT, ISOPROPYL ALCOHOL
- ICS
- 49.140
- CCS
- V39
- 发布
- 2005
- 实施
The activities listed above were interested in this document as of the date of this document.
PROPELLANT, PRIMING FLUID, ALCM ENGINE, GRADE PF-1
- ICS
- 49.140
- CCS
- V39
- 发布
- 2005
- 实施
1.1 This specification covers a reinforced plastic pipe and fittings system made from epoxy resin and glass-fiber reinforcement, together with adhesive for joint assembly, intended for service up to 150F (65.6C) and 150-psig (1034-kPa) operating pressure and surges up to 275 psig (1896 kPa) in aviation jet turbine fuel lines installed below ground.1.2 The dimensionless designator NPS has been substituted in this specification for such traditional terms as nominal diameter, size, and nominal size.1.3 The values stated in inch-pound units are to be regarded as standard. The values in parentheses are for information only.The following safety hazards caveat pertains only to the test method portion, Section , of this specification: This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use. Note 1There is no similar or equivalent ISO standard.
Standard Specification for Fiberglass (Glass-Fiber-Reinforced Thermosetting-Resin) Pipe and Pipe Fittings, Adhesive Bonded Joint Type, for Aviation Jet Turbine Fuel Lines
- ICS
- 23.040.20 (Plastic pipes); 23.040.45 (Plastic fitt
- CCS
- V39
- 发布
- 2005
- 实施
This Publicly Available Specification specifies the fuelling procedures, hydrogen boil-off management procedures, storage requirements of hydrogen, and characteristics of the ground support equipment required to operate an airport hydrogen fuelling facility.
Airport hydrogen fuelling facility operations
- ICS
- 49.100
- CCS
- V39
- 发布
- 2004-10
- 实施
