航空航天发动机和推进系统标准-分析测试百科网

SAE AS3494A-2014 垫圈.XIII型引擎辅机驱动

Scope is unavailable.

GASKET - TYPE XIII ENGINE ACCESSORY DRIVE

ICS: 49.050
CCS: J13
发布: 2014-02-13
实施

SAE AMS2647E-2014 荧光渗透剂检查法进行航空器和发动机组件维修

This specification details requirements and procedures for the detection of defects in aircraft and engine components during maintenance and overhaul operations.

Fluorescent Penetrant Inspection, Aircraft and Engine Component Maintenance

ICS: 49.050
CCS: V30
发布: 2014-02-06
实施

SAE AS84D-2014 曲线,渐伸线(全部饰线)

This SAE Aerospace Standard (AS) defines an involute with a 30° pressure angle and a full radius at the roots thus reducing the stress concentration in the area of the root.

Splines, Involute (Full Fillet)

ICS: 49.050
CCS
发布: 2014-02-06
实施

ASTM F3005-14 用于小型无人机系统的电池的标准规范

1.1 This standard defines the requirements for batteries used in small Unmanned Aircraft Systems (sUAS). 1.2 This standard does not define requirements for the systems in which sUAS battery packs may be utilized. 1.3 This standard is subordinate to Specification F2910. 1.4 If allowed by a nation’s GAA, certain sUAS may be exempt from this standard and may use commercial off-the-shelf (COTS) batteries. Air transport regulations still shall be adhered to when air transport is used for COTS cells or batteries in bulk. 1.5 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.

Standard Specification for Batteries for Use in Small Unmanned Aircraft Systems (sUAS)

ICS: 49.050
CCS
发布: 2014-01-15
实施

SAE AS3497A-2014 垫圈.XIX型发动机附件传动装置

Scope is unavailable.

GASKET - TYPE XIX ENGINE ACCESSORY DRIVE

ICS: 49.050
CCS: J13
发布: 2014-01-09
实施

SAE AS3496A-2014 垫圈.XVI型发动机附件传动装置

Scope is unavailable.

GASKET - TYPE XVI ENGINE ACCESSORY DRIVE

ICS: 49.050
CCS: J13
发布: 2014-01-09
实施

SAE AIR5433B-2014 航空推进和驱动系统中使用润滑剂的润滑特性和典型性能

This SAE Aerospace Information Report (AIR) establishes guidance for the specification of formulated lubricant properties which contribute to the lubricating function in bearings, gears, clutches and seals of aviation propulsion and drive systems.

Lubricating Characteristics and Typical Properties of Lubricants Used in Aviation Propulsion and Drive Systems

ICS: 49.050
CCS: E34
发布: 2014-01-03
实施

SAE AS3493A-2014 垫片. XII, XIV A以及XIV B型发动机附件传动装置

Scope is unavailable.

GASKET - TYPE XII, XIV A AND XIV B ENGINE ACCESSORY DRIVE

ICS: 49.050
CCS
发布: 2014-01-02
实施

GOST R 56099-2014 液体火箭发动机. 强制试验方法

Engines rocket liquid. Methods of the forced test

ICS: 49.050
CCS: V72
发布: 2014
实施: 2015-03-01

GOST R 56181-2014 航空发动机和发动机部件. 航空发动机零件的清洁方法. 通用技术要求

Aviation engines and engine components. Methods of aviation engine part cleaning. General technical requirements

ICS: 49.050
CCS
发布: 2014
实施: 2015-01-01

ASTM F2840-14 设计和制造轻型运动飞行器用电力推进装置的标准实践规程

3.1 This specification provides designers and manufacturers of electric propulsion for light sport aircraft design references and criteria to use in designing and manufacturing EPUs. 3.2 Declaration of compliance is based on testing and documentation during the design, ground testing and flight testing of the EPU by the manufacturer or under the manufacturers’ guidance. 3.3 Manufacturers of the EPUs are encouraged to review and incorporate appropriate standards and lessons learned from ground based systems as documented in SAE J2344 and EASA CRI F-58 (see Appendix X2). 3.4 Electric aircraft may contain potentially hazardous level of electrical voltage or current. It is important to protect persons from exposure to this hazard. Under normal operating conditions, adequate electrical isolation is achieved through physical separation means such as the use of insulated wire, enclosures, or other barriers to direct contact. There are conditions or events that can occur outside normal operation that can cause this protection to be degraded. Some means should be provided to detect degraded isolation or ground fault. In addition, processes or hardware, or both, should be provided to allow for controlled access to the high voltage system for maintenance or repair. A number of alternative means may be used to achieve these electrical safety goals including automatic hazardous voltage disconnects, manual disconnects, interlock systems, special tools and grounding. The intention of all these means is either to prevent inadvertent contact with hazardous voltages or to prevent damage or injury from the uncontrolled release of electric energy. Lightning strikes are not addressed in this Standard Practice because LSA aircraft are limited to VMC flight only. 1.1 This practice covers minimum requirements for the design and manufacture of Electric Propulsion Units (EPU) for light sport aircraft, VFR use. The EPU shall as a minimum consist of the electric motor, associated controllers, disconnects and wiring, an Energy Storage Device (ESD) such as a battery or capacitor, or both, and EPU monitoring gauges and meters. Optional onboard charging devices, in-flight charging devices or other technology may be included. 1.2 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.

Standard Practice for Design and Manufacture of Electric Propulsion Units for Light Sport Aircraft