Published November 1, 2019 | Version v1
Journal article

Derated Thrust: Method Analysis for Optimizing Turbofan Engine Takeoff Performances (SFC, EGT) Due to Lower Maximum Takeoff Weight (MTOW) Requirement

  • 1. Department of Mechanical Engineering, Universitas Indonesia, Depok, West Java, 16424 (Indonesia)

Description

Reduced thrust or derate has been practiced commonly nowadays as a standard procedure of takeoff. Since power is being used at maximum during takeoff phase, the practice has many benefits for the operation of aircraft. Not only it reduced fuel consumption during the takeoff phase, but also reduced engine's wear and tear that caused by stress and a very high temperature. Exhaust Gas Temperature (EGT) is one of the most important parameters that used to monitor the engine deterioration. There is a definite correlation between reducing takeoff thrust and EGT reduction, where both values are contradicting one another. However, there must be some calculation by the flight crew on how much percentage of derate is eligible prior to takeoff. The goal of this paper is to find the effectiveness of derate to reduce EGT in order to improve performance, prolong engine life and reduce operating costs of the operators. (paper)

Availability note (English)

Available from http://dx.doi.org/10.1088/1757-899X/685/1/012007

Additional details

Publishing Information

Journal Title
IOP Conference Series. Materials Science and Engineering (Online)
Journal Volume
685
Journal Issue
1
Journal Page Range
[6 p.]
ISSN
1757-899X

Conference

Title
3. International Conference on Aerospace Technology, Communications and Energy Systems
Acronym
ATCES 2019
Dates
26-29 Sep 2019
Place
Nanjing (China)

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
54077245
Subject category
S42: ENGINEERING;
Resource subtype / Literary indicator
Conference
Descriptors DEI
AIRCRAFT; FUEL CONSUMPTION; OPTIMIZATION; PERFORMANCE; TURBOFAN ENGINES
Descriptors DEC
ENERGY CONSUMPTION; ENGINES; EQUIPMENT; HEAT ENGINES; INTERNAL COMBUSTION ENGINES; MACHINERY; TURBOMACHINERY