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Aircraft Fuel System and Component Icing Test 飞机燃油系统和部件结冰试验
发布日期: 2012-06-06
本航空航天推荐规程(ARP)简要讨论了飞机燃油系统中的结冰问题以及用于结冰的不同方法。本文提出了飞机燃油系统和部件的燃油制备程序和结冰试验,作为飞机工业中仅用于固定翼飞机及其运行环境的推荐做法。在本ARP中,发动机(和APU)不被视为飞机燃油系统的一个部件,因为发动机燃油系统由发动机/APU制造商进行结冰试验,用于商业和特定军事应用。 本ARP主要用于解决燃油系统液位测试问题。它还提供了满足14 CFT 23.951(c)和25.951(c)要求的方法。本文档中描述的一些方法可应用于发动机和APU级测试或这些应用领域的组件。本次修订并未完全解决管道内部流动导致的积冰的新发展。当将来有更多的实验数据可用时,ina将进行修订。有关该主题的一些背景信息计划在AIR 790上提供。
This Aerospace Recommended Practice (ARP) covers a brief discussion of the icing problem in aircraft fuel systems and different means that have been used for icing. Fuel preparation procedures and icing tests for aircraft fuel system and components are proposed herein as a recommended practice to be used in the aircraft industry for fixed wing aircraft and their operational environment only. In the context of this ARP, the engine (and APU) is not considered to be a component of the aircraft fuel system, for the engine fuel system is subjected to icing tests by the engine/APU manufacturer for commercial and specific military applications. This ARP is written mostly to address fuel system level testing. It also provides a means to address the requirements of 14 CFT 23.951(c) and 25.951(c). Some of the methods described in this document can be applied to engine and APU level testing or components of those application domains.This revision does not completely address new developments in ice accretion resulting from internal flow in tubing. This will be addressed ina future revision when more experimental data is available. Some background information on the topic is planned to be available in AIR 790.
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