V32 发动机零部件 标准查询与下载



共找到 122 条与 发动机零部件 相关的标准,共 9

Drive-Accessory, (254) 10.000 BC Round, QAD, Design Standard for

Drive-Accessory, (254) 10.000 BC Round, QAD, Design Standard for

ICS
49.050
CCS
V32
发布
1993-08-01
实施

Drive-Accessory, (203.2) 8.000 BC Round, QAD, Design Standard for

Drive-Accessory, (203.2) 8.000 BC Round, QAD, Design Standard for

ICS
49.050;
CCS
V32
发布
1993-08-01
实施

Light Duty Gas Turbine Raised Panel Slip On Steel Pipe Flanges

ICS
CCS
V32
发布
1993-02-22
实施
1993-08-01

本标准规定了轻型燃气轮机钢制管法兰用耐油石棉橡胶垫片的形式、尺寸、技术要求。   本标准适用于轻型燃气轮机凸面带颈承插焊钢管法兰用耐油石棉橡胶垫片,也适用于轻型燃气轮机凸面板式平焊钢制管法兰用耐油石棉橡胶垫片。

Oil-resistant asbestos rubber gaskets for steel pipe flanges of light gas turbines

ICS
CCS
V32
发布
1993-02-22
实施
1993-08-01

本标准规定了轻型燃气机钢制管法兰的技术要求、试验、检验和验收、包装和贮存。   本标准适用于轻型燃气机钢制管法兰。

Specifications for steel pipe flanges for light duty gas turbines

ICS
CCS
V32
发布
1993-02-22
实施
1993-08-01

Light Duty Gas Turbine Raised Face Neck Socket Welding Steel Pipe Flanges

ICS
CCS
V32
发布
1993-02-22
实施
1993-08-01

THREAD LONGITUDINAL STRAPPING, ITEM 2, BEMIEEN THE DECK WIRES OF PALLET, E M 1, AS SHOWN IN DETAIL B.

UNIT LOAD FOR UNDERWAY REPLENISHMENT CANISTER, ADAPTER ASSEMBLY, MK 18 MOD 0

ICS
49.050
CCS
V32
发布
1992-07-29
实施

MIL-F-81256(WP), dated 4 March 1965, and Amendment 1, dated 16 November 1966, are inactive for new design and no longer used by the Navy except for replacement purposes.

SILICA FABRIC, PHENOLIC IMPREGNATED

ICS
49.050
CCS
V32
发布
1992-05-20
实施

MIL-P-l9086E, dated 25 July 1975 is inactive for new design and is no longer used, except for replacement purposes.

EXPANDING SHIELDED MILD DETONATING CORD ASSEMBLY

ICS
49.050
CCS
V32
发布
1991-08-14
实施

This SAE Aerospace Recommended Practice (ARP) addresses the characteristics required for the definition, development, and acquisition of a satisfactory airframe mounted accessory gearbox (AMAG).

Gearbox - Airframe Mounted Accessory

ICS
49.050
CCS
V32
发布
1991-06-21
实施

This specification covers panelized prefabricated modular building components for prefabricated, ready-cut, relocatable building with gabled roofs, vertical walls of variable lengths and heights.

BUILDING COMPONENTS, PANELIZED, PREFABRICATED, READY-CUT, RELOCATABLE

ICS
49.050
CCS
V32
发布
1991-03-25
实施

This specification covers the requirements for the manufacture, acceptance, and delivery of one type of delay composition designated T 10

DELAY COMPOSITION, T-10

ICS
49.050
CCS
V32
发布
1991
实施

This metric Aerospace Information Report (AIR) details a ball-on-cylinder (BOC) test device and specifies a method of rating the relative lubricity of aviation turbine fuel samples. The BOC produces a wear scar on a stationary steel ball by forcing it with a fixed load against a fuel wetted steel test ring in a controlled atmosphere. The test ring is rotated at a fixed speed so its surface is wetted by a momentary exposure to the fluid under test. The size of the wear scar is a measure of the test fluid lubricity and provides a basis for predicting friction or wear problems. This ARP is intended as a guide toward a standard practice, but may be subject to frequent change reflecting experience and technical advances. Use of this AIR is not recommended where flexibility of revision is impractical. Anyone interested in current information on BOC developments and technology should contact the Coordinating Research Council (CRC) Aviation Group on Aviation Fuel Lubricity.

BALL-ON-CYLINDER (BOC) AIRCRAFT TURBINE FUEL LUBRICITY TESTER [Superseded: SAE MAP 1794]

ICS
49.050;75.100
CCS
V32
发布
1990-05-01
实施

This specification covers the requirements for the manufacture, acceptance, and delivery of one type of Z-1 delay composition

DELAY COMPOSITION, Z-1

ICS
49.050
CCS
V32
发布
1990
实施

PACKING, PREFORMED O-RING SEAL, FLUOROCARBON (MIL-R-83485, TYPE I), METRIC FSC 5330Table1 dimensionsTABLE 2 - O-RING SEALS FOR MA2093PORT FITTING END CONFIGURATIONINTO MA2012 PORTTABLE 3 - O-RING SEALS FOR MA2111, MA2112 & MA2113PORT FITTING END CONNECTION INTO MA2110 PORT

PACKING, PREFORMED O-RING SEAL, FLUOROCARBON (MIL-R-83485, TYPE I), METRIC FSC 5330

ICS
49.035
CCS
V32
发布
1988-09-01
实施

This recommended practice describes a method of conducting an endurance test using contaminated air when the applicable specification requires non-recirculation of the contaminants. The objective of the test is to determine the resistance of the engine mounted components to wear or damage caused by the contaminated air. The method described herein calls for non-recirculation of the contaminants and is intended to provide a uniform distribution of the contaminant at the inlet to the Unit Under Test (UUT). The UUT may require the use of a hydraulic fluid for actuation of components within the test unit. Contamination of this test fluid is not part of this recommended practice, however, if required by applicable test specification refer to MAP 749A.

AIRCRAFT TURBINE ENGINE PNEUMATIC COMPONENT CONTAMINATED AIR ENDURANCE TEST

ICS
49.050;49.080
CCS
V32
发布
1988-08-31
实施

This specification covers the procurement requirements for metric corrosion resistant steel retaining rings of the tapered width type with rectangular and beveled cross-sections.

Rings, Retaining - Tapered Width, Uniform Thickness Corrosion Resistant, Procurement Specification For, Metric FSC 5365

ICS
49.050
CCS
V32
发布
1988-06-09
实施

This specification covers the procurement requirements for corrosion resistant steel retaining rings of the spiral wound type with uniform rectangular cross-sections.

Rings, Retaining - Spiral Wound, Uniform Section Corrosion Resistant, Procurement Specification For, Metric

ICS
49.050
CCS
V32
发布
1988-06-09
实施

本标准规定了在CL—100齿轮试验机上测定试验齿轮副的胶合承载能力的试验方法。   本标准适用于航空齿轮所用“材料—油”组合[G]的齿轮副的胶合承载能力的测定。结合航空工业部标准HB/Z84.4-84《航空渐开线圆柱齿轮胶合承载能力计算》和HB/Z89.4-85《航空锥齿轮胶合承载能力计算》,可分别计算出各种“材料—油”组合的齿轮胶合温度。

Aeronautical gear bonded bearing capacity test method

ICS
CCS
V32
发布
1988-04-10
实施
1988-10-01

This specification establishes the requirements for manufacture and acceptance of the Module Assembly, PersonnelStorage. This item is the only one of its type.

MODULE ASSEMBLY, PERSONNEL STORAGE

ICS
49.050
CCS
V32
发布
1988-01-20
实施



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