Transient Thermal Stresses in Multilayered Devices

1993 ◽  
pp. 139-172 ◽  
Author(s):  
An-Yu Kuo ◽  
Kuan-Luen Chen
Keyword(s):  
Thermal Stresses ◽  
Transient Thermal

Comprehending Occurrence of Premature Failure in Compressor Turbine (CT) Blades for Short-Haul Aircraft Fleet

2019 ◽  
Vol 42 ◽  
pp. 10-23
Author(s):  
Joshua Kimtai Ngoret ◽  
Venkata Parasuram Kommula
Keyword(s):  
Finite Element Analysis ◽  
Finite Element ◽  
High Pressure ◽  
Thermal Stresses ◽  
Geometrical Model ◽  
Mechanical Stresses ◽  
Element Analysis ◽  
Premature Failure ◽  
Structural Stresses ◽  
Transient Thermal

This paper presents results from modeling of Compressor Turbine (CT) blades for short-haul aircraft fleet occasioned by thermo-mechanical stresses in order to comprehend the occurrence of premature failure. A 3D PT6A-114A engine high pressure (HP) CT blade geometrical model was developed in commercial CAD-SolidWorks, then imported to ANSYS 15.0 environment for finite element analysis (FEA). The CT blade was investigated for transient thermal stresses from heat generated by the combustors and static structural stresses from rotational velocities of the engine which account for 80% of inertial field during flight. The results revealed that the blades could have served for another 1.44% of the time they were in service.

scholarly journals The axisymmetric Boussinesq-type problem for a half-space under optimal heating of arbitrary profile

2004 ◽  
Vol 2004 (40) ◽  
pp. 2123-2131
Author(s):  
J. Rokne ◽  
B. M. Singh ◽  
R. S. Dhaliwal ◽  
J. Vrbik
Keyword(s):  
Temperature Field ◽  
Half Space ◽  
Analytical Method ◽  
Thermal Stresses ◽  
Type Problem ◽  
Total Load ◽  
Arbitrary Profile ◽  
Laplace And Hankel Transforms ◽  
Transient Thermal ◽  
Optimal Heating

A solution of the axisymmetric Boussinesq-type problem is derived for transient thermal stresses in a half-space under heating by using the Laplace and Hankel transforms. An analytical method is developed to predict the temperature field that satisfies the prescribed mechanical conditions. Several simple shapes of punches of arbitrary profile are considered and an expression for the total load is derived to achieve penetration. The numerical results for the temperature and the total load on the punch are shown graphically.

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