V36 总体技术要求 标准查询与下载

GJB 5678-2006 军用直升机武器系统靶标通用规范

本规范规定了军用直升机武器系统试验、训练用靶标的通用要求。 本规范适用于军用直升机武器系统所使用的各种靶标。

General specification for target of weapon system on military helicopter

AIAA S-081A-2006 航天系统-综合过包装压力容器(COPVs)

This standard establishes baseline requirements for the design, fabrication, test, inspection, operation and maintenance of composite overwrapped pressure vessels (COPVs) containing a metallic liner. These vessels are used for pressurized, hazardous or non-hazardous liquid or gas storage in space systems including spacecraft and launch vehicles. These requirements when implemented on a particular system will assure a high level of confidence in achieving safe and reliable operation. This standard is applicable to COPVs with metallic liners and is written to address COPVs at the component (i.e., pressure vessel) level. This document may also be applicable for Reusable Launch Vehicles (RLV) if appropriate changes are agreed upon between the responsible safety authorities and RLV operators.

Space Systems - Composite Overwrapped Pressure Vessels (COPVs)

SAE ARP5151-2006 商业通用航空飞机和直升机的安全评价

This document describes a process that may be used to perform the ongoing safety assessment for (1) GAR aircraft and components (hereafter, aircraft), and (2) commercial operators of GAR aircraft. The process described herein is intended to support an overall safety management program. It is to help a company establish and meet its own internal standards. The process described herein identifies a systematic means, but not the only means, to assess continuing airworthiness Ongoing safety management is an activity dedicated to assuring that risk is identified and properly eliminated or controlled. The safety management process includes both safety assessment and economic decision-making. While economic decision-making (factors related to scheduling, parts, and cost) is an integral part of the safety management process, this document addresses only the Ongoing Safety Assessment Process. This Ongoing Safety Assessment Process includes safety problem identification and corrective action, tracking of problems, the application of Lessons Learned to improve the efficiency of the process, and reduction of the time to achieve corrective action in the field. ARP5150 is the standard for the safety assessment of Transport Airplanes in Commercial Service. ARP5151 specifies the safety assessment process for GAR aircraft in Commercial Services. While the processes are similar, their implementations are different due to operations, data availability, and sizes of individual operations.

Safety Assessment of General Aviation Airplanes and Rotorcraft in Commercial Service

ASTM F2245-06 轻型运动飞机的设计和性能的标准规范

1.1 This specification covers airworthiness requirements for the design of powered fixed wing light sport aircraft, an "airplane."1.2 This specification is applicable to the design of a light sport aircraft/airplane as defined by regulations and limited to VFR flight.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 requirements prior to use.

Standard Specification for Design and Performance of a Light Sport Airplane

GJB 5451-2005 直升机武器悬挂结构设计要求

本标准规定了军用直升机武器悬挂结构的设计和试验等要求。 本标准适用于军用直升机武器悬挂结构的设计。

Design requirements of weapon handing structure for helicopter

GJB 5446-2005 直升机旋翼动力学设计要求

本标准规定了直升机旋翼动力学的设计、分析、试验等相关要求。 本标准使用于单旋翼带尾桨直升机的旋翼系统，其它类型直升机的旋翼系统可参照使用。

Design requirements of rotor dynamics for helicopter

GJB 5447-2005 直升机自动倾斜器设计要求

本标准规定了直升机自动倾斜器设计和试验等要求。 本标准适用于直升机环状球铰式自动倾斜器的设计，其他类型自动倾斜器的设计可参照使用。

Design requirements of swashplate for helicopter

GJB 5436-2005 机载红外搜索跟踪系统通用规范

本标准规定了无人机鉴定和定型的程序及审查文件的要求。 本标准适用于固定翼无人机系统（简称无人机）产品鉴定和设计定型（简称定型），使用时可根据所属定委要求和实际情况进行适当剪裁。

Procedure and document check requirements for appraisal and validation of UAV

SAE ARP4737G-2005 飞行器除冰办法

This document establishes the minimum requirements for ground based aircraft deicing/anti-icing Methods and procedures to ensure the safe operation of aircraft during icing conditions. This document does not specify requirements for particular airplane models. NOTE: Patricular airline or aircraft manufacturers published manuals, procedures, or methods supplement the information contained in this document.

Aircraft Deicing/Anti-Icing Methods

ISO 8267-2:2005 飞行器.牵引杆附属接头的接口要求.第2部分:地方飞行器

This part of ISO 8267 specifies the interface requirements for tow bar attachment fittings on the nose gear (when towing operations are performed from the nose gear) of conventional tricycle type landing gears of commercial civil transport aircraft. Its purpose is to achieve tow bar attachment fittings interface standardization by aircraft mass category (which determines tow bar forces) in order to ensure that a single type of tow bar with a standard connection can be used for all aircraft types within or near that mass category, so as to assist operators and airport handling companies in reducing the number of different tow bar types used. This part of ISO 8267 is applicable to all new models of regional aircraft within the specified maximum ramp mass range which enter service or are designed after its date of publication. It does not apply to previously in service regional aircraft models, which present a considerable variety of tow bar attachment fittings. However, a simple retrofit modification is described that may make certain in-service fittings compatible with a tow bar head in conformity with this part of ISO 8267, where deemed appropriate in order to facilitate operation of such aircraft types at airports. This part of ISO 8267 is applicable to regional commercial transport aircraft airworthiness certified under FAR/JAR Parts 25 with a maximum ramp mass of ≤ 50 000 kg (110 000 Ib). It does not apply to — aircraft airworthiness certified under FAR/JAR Parts 23 as commuter category aeroplanes; — aircraft airworthiness certified under FAR/JAR Parts 25 but with a maximum ramp mass of > 50 000 kg (110 000 Ib), which are covered by ISO 8267-1. Where a family of existing or contemplated aircraft types bridges two mass categories, use a single tow bar attachment fitting interface for all of them, and consider the use of the standard dimensions for the higher mass category, be it part of this part of ISO 8267 or ISO 8267-1, throughout the family. NOTE As far as practical, this part of ISO 8267 was defined in order to be compatible with as many existing aircraft types as possible in the mass category concerned.

Aircraft - Tow bar attachment fittings interface requirements - Part 2: Regional aircraft

ISO 8267-1:2005 飞行器.牵引杆附属接头的接口要求.第1部分:干线飞行器

This part of ISO 8267 specifies the interface requirements for tow bar attachment fittings on the nose gear (when towing operations are performed from the nose gear) in conventional tricycle type landing gears of commercial civil transport passenger and freight aircraft. Its purpose is to achieve tow bar attachment fittings interface standardization by aircraft mass category (which determines tow bar forces) in order to ensure that a single type of tow bar with a standard connection can be used for all aircraft types within or near that mass category, so as to assist operators and airport handling companies in reducing the number of different tow bar types used. This part of ISO 8267 is applicable to all new models of main line aircraft within the specified maximum ramp mass range, entering service or designed after its date of publication. This part of ISO 8267 is applicable to main line commercial transport aircraft of airworthiness certified under FAR/JAR Parts 25 with a maximum ramp mass of > 50 000 kg (110 000 Ib). It does not apply to aircraft of airworthiness certified under FAR/JAR Parts 25 but with a maximum ramp mass of ≤ 50 000 kg (110 000 Ib), which are covered by ISO 8267-2. Where a family of existing or contemplated aircraft types bridges two mass categories, use a single tow bar attachment fitting interface for all of them, and consider the use of the standard dimensions for the higher mass category throughout the family. NOTE As far as practical, this part of ISO 8267 was defined in order to be compatible with as many existing aircraft types as possible in the mass category concerned.

Aircraft - Tow bar attachment fittings interface requirements - Part 1: Main line aircraft

GJB 5435.10-2005 无人机强度和刚度规范 第10部分：飞行试验

本部分规定了无人机结构强度检查和载荷验证的飞行试验要求，以及为达到这些要求所应遵循的原则。 本部分适用于有固定机翼和可调固定机翼的无人机；也适用于新研制的、改进的、改型的或改变用途的无人机。 本部分不适用于微型无人机和无人战斗机。

Specification for unmanned aerial vehicles strength and rigidity Part 10: Flight tests

GJB 5435.2-2005 无人机强度和刚度规范 第2部分：飞行载荷

本部分规定了无人机在飞行载荷下的设计要求，还规定了为达到这些要求所应遵循的原则。 本部分适用于有固定机翼和可调固定机翼的无人机，适用于新研制的、改进的、该型的或改变用途的无人机。 本部分不适用于微型无人机和无人战斗机。

Specification for unmanned aerial vehicles strength and rigidity Part 2: Flight loads

GJB 5435.1-2005 无人机强度和刚度规范 第1部分：总则

本部分规定了无人机结构强度和刚度设计要求，以及为达到这些要求所应遵循的原则。 本部分适用于有固定机翼和可调固定机翼的无人机：适用于新研制的、改进的、改型的或改变用途的无人机。 本部分不适用于微型无人机和无入战斗机。

Specification for unmanned aerial vehicles strength and rigidity Part 1: General specification

GJB 5435.4-2005 无人机强度和刚度规范 第4部分：发射及回收载荷

本部分规定了自主起降无人机在发射及回收过程中作用在机体上的载荷及相应的质量保证规定。 本部分适用于有固定机翼和可调机翼的无人机：适用于研制的、改进的、改型的或改变用途的无人机。 本部分不适用于微型无人机和无人战斗机。

Specification for unmanned aerial vehicles strength and rigidity Part 4: Launching and recovery system load

GJB 5435.5-2005 无人机强度和刚度规范 第5部分：其它载荷

本部分规定了无人机在其它载荷下的强度和刚度要求，以及为达到这些要求所应遵循的原则。 本部分适用于有固定机翼和可调固定机翼的无人机：电适用于新研制的、改进的、改型的或改变用途的无人机。 本部分不适用于微型无人机和无人战斗机。

Specification for unmanned aerial vehicles strength and rigidity. Part 5: Miscellaneous loads

GJB 5435.7-2005 无人机强度和刚度规范 第7部分：振动

本部分规定了无人机结构振动方面的设计要求,以及为达到这些要求所应遵循的原则。 本部分适用于有固定机翼和可调固定机翼的无人机:适用于新研制的、改进的、改型的或改变用途的无人机。 本部分不适用于微型无人机和无人战斗机。

Specification for unmanned aerial vehicles strength and rigidity Part 7: Vibration

GJB 5435.8-2005 无人机强度和刚度规范 第8部分：气动弹性不稳定性

本部分规定了无人机结构气动弹性不稳定性设计方面的要求，以及为达到这些要求所应遵循的原则。 本部分适用于有固定机翼和可调固定机翼的无人机：适用于新研制的、改进的、改型的或改变用途的无人机。 本部分不适用于微型无人机和无人战斗机。

Specification for unmanned aerial vehicles strength and rigidity Part 8: Aeroelastic instabilities

GJB 5435.9-2005 无人机强度和刚度规范 第9部分：地面试验

本部分规定了无人机结构鉴定和验证的地面试验要求，以及为达到这些要求所应遵循的原则。 本部分适用于有固定机翼和可调固定机翼的无人机；也适用于帮研制的、改进的、改型的或改变用途的无人机。 本部分不适用于微型无人机和无人战斗机。

Specification for unmanned aerial vehicles strength and rigidity Part 9: Ground tests

GJB 5435.3-2005 无人机强度和刚度规范 第3部分：地面载荷

本部分规定了具有常规起落架形式的无人机在着陆和地面操作载荷下的强度和刚度要求，以及为达到这些要求所应遵循的原则。 本部分适用于有固定机翼和可调固定机翼的具有常规起落架形式的无人机：适用于新研制的、改进的、改型的或改变用途的无人机。 本部分不适用于微型无人机和无人战斗机。

Specification for unmanned aerial vehicles strength and rigidity Part 3: Ground loads