Solved 3. Shrouds are often used at the tips of turbine | Chegg.com
The Turbine Blade: ROOTS, SHROUD AND AIRFOIL | WENZEL America
![Turbine blade tip shroud and mid-span snubber with compound contact angle Patent Grant Puram , et al. No [General Electric Company]](https://uspto.report/patent/grant/10465531/US10465531-20191105-D00000.png "Turbine blade tip shroud and mid-span snubber with compound contact angle Patent Grant Puram , et al. No [General Electric Company]")
Turbine blade tip shroud and mid-span snubber with compound contact angle Patent Grant Puram , et al. No [General Electric Company]
Investigation of dynamical characteristic of shrouded blade of aero-engine subjected to impact and friction | Semantic Scholar
Tubine Blades Knife Edge Seals - YouTube
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7.1.3 Blade Tip Rubbing Damage [Aeroengine Safety]
terminology - What is meant by "shroud" in a gas turbine? For example, an inner shroud and an outer shroud in a vane device in a gas turbine? Thank You - Aviation
ENGINE CONSTRUCTION
The Turbine Blade: ROOTS, SHROUD AND AIRFOIL | WENZEL America
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11.2.3.2 Turbine Damage [Aeroengine Safety]
Energies | Free Full-Text | Feasible Concept of an Air-Driven Fan with a Tip Turbine for a High-Bypass Propulsion System
Nonlinear Dynamic Analysis of Shrouded Turbine Blade of Aero-engine Subjected to Combination Effect of Impact and Friction | Semantic Scholar
EP1605134A2 - Device for balancing a gas turbine rotor and gas turbine engine comprising such a device - Google Patents
Diagnostics of shroud ties of blade system of steam turbines
Z-notch shape for a turbine blade tip shroud - Eureka | Patsnap
Axial Turbine Blade Tips: Function, Design, and Durability
Solved 2.7 Shrouds are often used at the tips of turbine | Chegg.com
A review of blade tip clearance–measuring technologies for gas turbine engines - Bing Yu, Hongwei Ke, Enyu Shen, Tianhong Zhang, 2020
EP1701004A1 - Gas turbine blade having a monocrystalline airfoil with a repair squealer tip, and repair method - Google Patents
Noise characteristics of a reduced blade count rotor with improved stage efficiency
Aircraft Gas Turbine Engine Turbine Section
Research on turbine blade squealer tip film holes arrangement and moving shroud | Aerospace Systems
Center-located cutter teeth on shrouded turbine blades - Patent 1507066
Automated Preliminary Thermal and Stress Analyses Applied to a Turbine Housing Assembly
