blisk engine

A blisk (portmanteau of bladed disk) is a turbomachine component comprising both rotor disk and blades as a single part ...

blisk engine

A blisk (portmanteau of bladed disk) is a turbomachine component comprising both rotor disk and blades as a single part instead of a disk assembled with ... ,This multi-axis milled bladed disk is termed a “blisk” and is the latest trend in aircraft engine compressor wheels. Conventional competitor turbines have ...

相關軟體 Blisk 資訊

Blisk
Blisk 是一個基於鉻的瀏覽器,用於 web 開發的基本工具。將其用於同時構建和測試您的網站的桌面和移動版本。 Blisk 使開發人員能夠同時在多個設備上編碼,預覽其更改! 4 使用原因 Blisk:TIME SAVING以光速發展!現在您不需要一直刷新頁面,搜索並滾動到所需的元素。 Blisk 從根本上節省了開發和測試的時間。瀏覽器將使你的生產力達到 200%。所以你可以把你的工作快兩倍,把時... Blisk 軟體介紹

blisk engine 相關參考資料
Aerospace - Blisk - Industries - Tungaloy

Blisk is a structural component of aircraft jet engine that integrates blades and a disk. Blisk is machined by a 5-axis controlled milling machine because ...

https://tungaloy.com

Blisk

A blisk (portmanteau of bladed disk) is a turbomachine component comprising both rotor disk and blades as a single part instead of a disk assembled with ...

https://en.wikipedia.org

Blisk design - ETgroup

This multi-axis milled bladed disk is termed a “blisk” and is the latest trend in aircraft engine compressor wheels. Conventional competitor turbines have ...

https://www.etgroup.nl

Blisk development: How blade and disk became one

The space-saving and lighter blisks make engines more compact and more economical: their success story begins in the Eurofighter EJ200 engine.

https://aeroreport.de

Efficient jet engine blade and blisk production

A blisk (bladed disk) is an aeroengine component consisting of a rotor disk and multiple blades in a single part. Replacing the traditional assembly of an ...

https://www.aerospacemanufactu

LEAP engine - Blisk

https://www.youtube.com

Machining the Integral Impeller and Blisk of Aero-Engines

由 Y Fu 著作 · 2017 · 被引用 74 次 — When an integral impeller and a blisk are in operation, stress concentration usually occurs at the blade root, and FOD appears near blade edges.

https://cjme.springeropen.com

Recent Progress in Turbine Blade and Compressor Blisk ...

由 J Aschenbruck 著作 · 2014 · 被引用 63 次 — Abstract. The regeneration process of jet engines is a highly complex, expensive and time-consuming. Especially the regeneration of high pressure turbine b...

https://www.sciencedirect.com