首页> 外文OA文献 >Quiet, Efficient Fans for Spaceflight: An Overview of NASA's Technology Development Plan
【2h】

Quiet, Efficient Fans for Spaceflight: An Overview of NASA's Technology Development Plan

机译:安静,高效的航天飞机风扇:NASA技术发展计划概述

摘要

A Technology Development Plan to improve the aerodynamic and acoustic performance of spaceflight fans has been submitted to NASA s Exploration Technology Development Program. The plan describes a research program intended to make broader use of the technology developed at NASA Glenn to increase the efficiency and reduce the noise of aircraft engine fans. The goal is to develop a set of well-characterized government-owned fans nominally suited for spacecraft ventilation and cooling systems. NASA s Exploration Life Support community will identify design point conditions for the fans in this study. Computational Fluid Dynamics codes will be used in the design and analysis process. The fans will be built and used in a series of tests. Data from aerodynamic and acoustic performance tests will be used to validate performance predictions. These performance maps will also be entered into a database to help spaceflight fan system developers make informed design choices. Velocity measurements downstream of fan rotor blades and stator vanes will also be collected and used for code validation. Details of the fan design, analysis, and testing will be publicly reported. With access to fan geometry and test data, the small fan industry can independently evaluate design and analysis methods and work towards improvement.
机译:美国宇航局的探索技术开发计划已提交了一项技术开发计划,以改善航天风扇的空气动力学和声学性能。该计划描述了一项研究计划,旨在更广泛地利用NASA Glenn开发的技术,以提高效率并降低飞机发动机风扇的噪音。目标是开发一组特征鲜明的政府拥有的风扇,这些风扇名义上适用于航天器的通风和冷却系统。 NASA的探索生命支持社区将为研究中的粉丝确定设计要点条件。在设计和分析过程中将使用计算流体动力学代码。风扇将被制造并用于一系列测试。来自空气动力学和声学性能测试的数据将用于验证性能预测。这些性能图还将输入数据库,以帮助航天风扇系统开发人员做出明智的设计选择。风扇转子叶片和定子叶片下游的速度测量值也将被收集并用于代码验证。风扇设计,分析和测试的详细信息将公开报告。通过访问风扇的几何形状和测试数据,小型风扇行业可以独立评估设计和分析方法并进行改进。

著录项

  • 作者

    Koch L. Danielle;

  • 作者单位
  • 年度 2010
  • 总页数
  • 原文格式 PDF
  • 正文语种
  • 中图分类

相似文献

  • 外文文献
  • 中文文献
  • 专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号