Integrated computational methodology for next generation of aircraft landing gear solution

下一代飞机起落架解决方案的集成计算方法

• 批准号: 486968-2015
• 负责人: Behdinan, Kamran
• 金额: $ 13.17万
• 依托单位: University of Toronto
• 依托单位国家: 加拿大
• 项目类别: Collaborative Research and Development Grants
• 财政年份: 2016
• 资助国家: 加拿大
• 起止时间: 2016-01-01 至 2017-12-31
• 项目状态: 已结题
• 来源: https://www.nserc-crsng.gc.ca/ase-oro/Details-Detailles_eng.asp?id=600365
• 关键词: Integrated; computational; methodology; next; generation

Landing gear is an integral and indispensable part of the aircraft. Although the landing gear design dates back since the aircraft was invented, a standardized methodology for its design is hard to find in the industry. The objective of the proposal is to develop an integrated computational methodology for transport category aircraft landing gear solution. The proposed project integrates different phases of landing gear design, often conducted separately, into an integrated computational methodology for robust landing gear solution. The high-fidelity simulations in the proposed project would aid in virtual design of a complete landing gear system that can be built efficiently, thus reducing time, cost, and risk.

起落架是飞机不可分割的一部分。尽管起落架的设计可以追溯到飞机发明之初，但业界很难找到标准化的设计方法。该提案的目标是为运输类飞机起落架解决方案开发综合计算方法。拟议的项目将起落架设计的不同阶段（通常单独进行）集成到一个集成的计算方法中，以实现稳健的起落架解决方案。拟议项目中的高保真模拟将有助于虚拟设计完整的起落架系统，该系统可以高效构建，从而减少时间、成本和风险。