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acceleration test scopethis part specifies acceleration environment steady-state acceleration tests acceleration severity levels airborne equipment hairless camel hair prestressed concrete turnout sleepers medical plan
HB 6167.16-2014 in English

HB 6167.16-2014 in English

VALID

Environmental conditions and test procedures for airborne equipment of cifvil airplane-Part 16:Acceleration test

  • Issued on:2014-05-06
  • Implemented on:2014-10-01
  • File Format:PDF
  • Delivery:Via email within 1~3 business days
Price(USD): $210.00
$204.00
Standard No: HB 6167.16-2014
Document status: VALID
Title in English: Environmental conditions and test procedures for airborne equipment of cifvil airplane-Part 16:Acceleration test
Title in Chinese: 民用飞机机载设备环境条件和试验方法 第16部分:加速试验
Language: English
File Format: Electronic (PDF)
Delivery: Via email within 1~3 business days
Issued on: 2014-05-06
Implemented on: 2014-10-01
Professional Classification: HB-Aviation
Related Keywords: acceleration test scopethis part specifies
acceleration environment
steady-state acceleration tests
acceleration severity levels
airborne equipment
Related Topics: hb2014
hb 2014
airborne equipment
acceleration
Classification of test equipment
Accelerated test intermediate conditions
Aircraft airborne equipment environmental conditions and test methods
acceleration test
acceleration test
Trial implementation of environmental test methods for aircraft motors and electrical appliances
Equipment environmental conditions
Accelerated test intermediate conditions
will accelerate
Civil aircraft software loading
aircraft reinforcement equipment
Civil aircraft parts forming

本部分规定了两类稳态加速度试验,并规定了四种加速度严酷等级来模拟民用飞机机载设备使用中可能遇到的缓变加速度环境。
本部分适用于民用飞机机载设备正常飞行过程中受机动过载诱发的加速度环境。


Scope

This part specifies two types of steady-state acceleration tests and four acceleration severity levels to simulate the slowly changing acceleration environment that may be encountered in the use of onboard equipment on civil aircraft. This section applies to the acceleration environment induced by maneuvering overload during normal flight of civil aircraft airborne equipment. Emergency landing situations are not included in the scope of this section. In this case, reference should be made to HB 6167.5-2014.

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