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所在平台: Udemy |
课程主页: https://www.udemy.com/course/advanced-gas-turbine-engine-blade-design-using-catia/
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**课程名称：** 使用 CATIA 进行先进燃气轮机叶片设计 **课程概述：** 本课程深入探讨燃气轮机叶片的设计，这是飞机动力系统的关键组成部分。燃气轮机发动机的功率输出及其效率，很大程度上取决于它吸入的空气量以及空气在发动机内的流动效率，最终在涡轮和排气部分得到利用。而这一切又都依赖于发动机内部数以千计的叶片。 叶片是燃气轮机发动机中最关键且承受负担最重的部件。燃气轮机发动机作为飞机的动力心脏，赋予其前进的动力。由于其优秀的功率重量比，燃气轮机应用范围极其广泛，包括驱动飞机、直升机、舰船、火车、发电厂、泵、燃气压缩机、坦克等。 每一台成功的燃气轮机背后，都离不开一套高度复杂且精确的叶片系统，尤其是涡轮叶片。涡轮叶片在发动机内部运行时，会承受极高的疲劳载荷和超过1000摄氏度的高温。出于这个原因，涡轮叶片通常设计有 Firtree 根部、叶冠 (Shroud) 以及用于空气密封和内部冷却通道的迷宫密封 (labyrinths)。 本课程将为您提供关于涡轮叶片设计的全面知识。 **课程项目：** 本课程包含两个实际项目： 1. **航空发动机第二级涡轮叶片设计：** 此项目将包含 Firtree 根部和带迷宫密封的叶冠。 2. **航空发动机第四级涡轮叶片设计：** 此项目将设计一个具有 Firtree 根部（以迷宫密封作为根部平台）和内部冷却通道的涡轮叶片，以在运行时对叶片进行冷却。 在完成这两个项目时，您将有机会接触到涡轮叶片的工业图纸，并学习如何解读这些图纸。 **课程特色：** * **工业化内容：** 本课程所有知识均基于实际工业应用，旨在提升您的专业知识水平，使其与燃气轮机行业的专业人士相匹配。 * **实践操作：** 通过两个具体的项目，您将获得宝贵的实践经验。 **立即行动，提升您的技能！**
The power generation in a gas turbine engine mainly depends upon the amount of air it can suck from the atmosphere and how efficiently the air flow through the engine to finally get utilised in the turbine and exhaust section.All these depend on the 1000's of blades that are used inside the gas turbine engine. Blades are the most critical and abused part inside the gas turbine engine which is the powerplant of an aircraft which gives it the ability to propel ahead.The gas turbine engine's application is limitless as it has great power to weight ratio. It is used for powering aeroplanes, helicopters, ships, trains, power plants, pumps, gas compressors, tanks etc.And behind each successful gas turbine is a set of highly sophisticated and precise blades. Particularly Turbine blades. Turbine blades are subjected to very high fatigue load and Temperature over 1000 deg.C during its operation inside the engine. Due to this fact they come with Firtree root, Shroud and root with labyrinth for sealing the air and internal cooling channels.In this course; we have the right content covered which will give you ample knowledge on Turbine blades.There are 2 Projects included in this Course: 2nd Stage Turbine Blade of an Aero Engine4th Stage Turbine Blade of an Aero EngineThe first project contains a Firtree root and a Shroud with labyrinth.The Second project is on a Turbine blade having Firtree root with labyrinth as root platform and Internal cooling channels for Cooling the blade during operation. In both Projects you will experience the Turbine blade industrial drawing and the process for studying those drawings.All the knowledge that you will get in this course is purely industrial based and this will upgrade you knowledge level to match with the Gas Turbine industry professionals.So STOP Thinking; Take free lectures and Join Today.
