Published December 1, 2018 | Version v1
Journal article

Improving fatigue life of gas turbine fan blade using advanced composite materials

  • 1. MLR Institute of Technology, Hyderabad (India)
  • 2. Dept.of Aero., MLR Institute of Technology, Hyderabad (India)

Description

The application of fiber reinforced composites in gas turbine engines for aircraft helps to increase fatigue life, and also provides the high stiffness, low weight and high strength. In the emerging technology, gas turbine engine performance has been keeps on improving day by day to achieve better in the market between the competitors. Based on all the needs aviation engine plans to reduce the weight of the components wherever it is possible by changing the material selection and design process. Composite material is one of the key materials using in most of aircraft structural components and parts now a days. Here we considered the fan blade of turbofan engine and replaced existing materials with composite material. The objective is to find and improve the fatigue life of gas turbine engine mechanical system components by using advanced composite materials in place of existing materials. Fatigue analysis will be done in commercial finite element packages, based on the results margin and life of the fan blade is calculated. (paper)

Availability note (English)

Available from http://dx.doi.org/10.1088/1757-899X/455/1/012035

Additional details

Publishing Information

Journal Title
IOP Conference Series. Materials Science and Engineering (Online)
Journal Volume
455
Journal Issue
1
Journal Page Range
[10 p.]
ISSN
1757-899X

Conference

Title
2. International Conference on Advancements in Aeromechanical Materials for Manufacturing
Dates
13-14 Jul 2018
Place
Telangana (India)

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
52102165
Subject category
S42: ENGINEERING;
Resource subtype / Literary indicator
Conference
Descriptors DEI
COMPOSITE MATERIALS; DESIGN; FATIGUE; FIBERS; FINITE ELEMENT METHOD; FLEXIBILITY; GAS TURBINE ENGINES; GAS TURBINES; PERFORMANCE; REINFORCED MATERIALS; TURBOFAN ENGINES
Descriptors DEC
CALCULATION METHODS; ENGINES; EQUIPMENT; HEAT ENGINES; INTERNAL COMBUSTION ENGINES; MACHINERY; MATERIALS; MATHEMATICAL SOLUTIONS; MECHANICAL PROPERTIES; NUMERICAL SOLUTION; TENSILE PROPERTIES; TURBINES; TURBOMACHINERY