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41. 发明公开

KR1020130090848A 항공기 성능의 최적화 방법, 장치, 및 항공기 有权
标题翻译：优化飞机，设备和飞机性能的方法
公开(公告)号：KR1020130090848A
公开(公告)日：2013-08-14
申请号：KR1020130013617
申请日：2013-02-06
申请人： 에어버스 헬리콥터스
发明人： 에브라트,장-필리프 , 코프론,알반
IPC分类号： B64F5/00 , F02C9/28 , B64D27/10 , F02C6/20
CPC分类号： G01M15/14 , B64C27/04 , F02C9/00 , F05D2220/329 , F05D2260/80 , F05D2260/821 , F05D2270/303 , F05D2270/304 , F05D2270/332 , F05D2270/335 , F05D2270/803 , Y02T50/671
摘要： PURPOSE: An apparatus, method and aircraft for optimizing the performance of the aircraft are provided to optimize vehicle performance by health check of a turbine engine in order to maximize power margin. CONSTITUTION: A method for optimizing performance of an aircraft comprises following steps. Each turbine engine (2) comprises a gas generator (2') and a turbine assembly with one or more turbines (2", 2"'), and manufacturers determine the first minimum performance level and the second maximum performance level of an aircraft (1). Current power transferred to each turbo engine (2) is determined during a health check step. Current temperature and rotary speed of gas are measured in the turbine assembly. The first power margin is determined to ensure the first performance level at the current rotary speed. The health check for each turbine engine is performed by determining a second power margin and second minimum power in order to ensure the first performance level.
摘要翻译：目的：提供一种用于优化飞机性能的装置，方法和飞机，以通过涡轮发动机的健康检查来优化车辆性能，以最大化功率余量。构成：优化飞机性能的方法包括以下步骤。每个涡轮发动机（2）包括气体发生器（2'）和具有一个或多个涡轮机（2“，2”'）的涡轮机组件，制造商确定飞机的第一最低性能水平和第二最大性能水平（ 1）。在健康检查步骤期间确定传送到每个涡轮发动机（2）的当前功率。在涡轮组件中测量气体的当前温度和转速。确定第一功率余量以确保当前转速下的第一性能水平。通过确定第二功率裕度和第二最小功率来执行每个涡轮发动机的健康检查，以确保第一性能水平。

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