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Test results of the Northrop Grumman corporation turbine engine bleed air/fuel heat exchanger after 165 hours of operation with JP-8+100 fuel

机译：在JP-8 + 100燃料运行165小时后，北罗姆曼公司涡轮发动机出血空气/燃料换热器的测试结果

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Advanced Integrated Fuel System III, Contract No. F33615-94-C-2498, was awarded to Northrop Grumman Corporation (NGC) by the U.S. Air force to investigate a new thermal management system based on using a heat exchanger designed to cool 1100°F (593°C) turbine engine bleed air with JP-8+100 fuel (e.g., JP-8 with an additive package that increases fuel thermal stability by 100°F (55°C)). As part of the contract, NGC agreed to test the heat exchanger at the Advanced Reduced Scale Fuel System Simulator facility at Wright-Patterson AFB, OH. This paper documents the test conditions and results from the heat exchanger's first 165 hours of operation.

机译：先进的集成燃油系统III，合同编号F33615-94-C-2498，由美国空军授予北罗姆格·格鲁曼公司（NGC），以研究基于使用设计用于冷却1100°F的热交换器的新型热管理系统（593°C）涡轮发动机与JP-8 + 100燃料的空气（例如，JP-8，添加剂封装，通过100°F（55°C）增加燃料热稳定性）。作为合同的一部分，NGC同意在Wright-Patterson AFB的先进减少燃油系统模拟器设施中测试热交换器，哦。本文介绍了热交换器的首次运行前165小时的测试条件和结果。

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《World Aviation Congress and Exposition》|1999年||共9页
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作者
Gregory B. Tibbs;
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原文格式 PDF
正文语种
中图分类 U46-53;
关键词
Cooling systems; Fuel additives; Heat exchangers; Military aircraft; Simulation; Turbojet engines;

机译：冷却系统;燃料添加剂;换热器;军用飞机;模拟;涡轮喷气发动发动机;

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Test results of the Northrop Grumman corporation turbine engine bleed air/fuel heat exchanger after 165 hours of operation with JP-8+100 fuel

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