Aircraft fuel nozzle grounding plugs and sockets

1959 ◽  
Keyword(s):  
Aircraft Fuel ◽  
Fuel Nozzle

Aircraft Fuel Systems

2009 ◽  
Author(s):  
Roy Langton ◽  
Chuck Clark ◽  
Martin Hewitt ◽  
Lonnie Richards
Keyword(s):  
Aircraft Fuel

Fault Detection for Aircraft Fuel System with Neural Network

2020 ◽  
Author(s):  
Nithya Subramanian ◽  
Hongmei He ◽  
Ian Jennions
Keyword(s):  
Neural Network ◽  
Fault Detection ◽  
Fuel System ◽  
Aircraft Fuel

Ester formation fromn-alkanes by fungi isolated from aircraft fuel

1970 ◽  
Vol 10 (3) ◽  
pp. 189-196 ◽  
Author(s):  
H. Iizuka ◽  
H. T. Lin ◽  
M. Iida
Keyword(s):  
Aircraft Fuel ◽  
Ester Formation

scholarly journals Utilization of Low-Potential Energy Through to the Use in Aircraft Fuel System

2021 ◽  
Vol 1102 (1) ◽  
pp. 012007
Author(s):  
Renat R. Badykov ◽  
Roman A. Panshin ◽  
Olga V. Tremkina ◽  
Anastasia A. Prokofieva
Keyword(s):  
Potential Energy ◽  
Fuel System ◽  
Aircraft Fuel

Thermal Oxidation Behavior of TiAlCrSiN and AlCrTiN Films on HastelloyX

2012 ◽  
Vol 486 ◽  
pp. 400-405 ◽  
Author(s):  
K. Tuchida ◽  
Kessaraporn Wathanyu ◽  
S. Surinphong
Keyword(s):  
Thermal Oxidation ◽  
Oxidation Behavior ◽  
Oxide Scales ◽  
Surface Appearance ◽  
Turbine Engine ◽  
Testing Conditions ◽  
Working Temperature ◽  
Fuel Nozzle ◽  
Higher Temperature ◽  
Scratch Tests

In this paper, the thermal oxidation behavior of TiAlCrSiN and AlCrTiN films coated on hastelloyX substrate, typically used for fuel nozzle in gas turbine engine application, have been studied. The thermal oxidation behavior at 950, 1050 and 1150 °C in controlled atmosphere were investigated. The surface appearance, microstructure, chemical composition and adhesion of films were investigated. The thermal oxidations were observed in all testing conditions showing oxide films at the surface with thicker oxide film at higher temperature. However, spalling of oxide scales was found in both coated and uncoated specimens at 1150°C suggesting the maximum working temperature of < 1150 °C for turbine engine applications. The critical loads corresponding to the full delamination of the thermal oxidation coated specimens were found to be higher than the non-thermal oxidation specimens. The effect of thermal oxidation on damage patterns during scratch tests, i.e. less chipping and cracking for thermal oxidation specimen, were also observed.

Sign in / Sign up

Export Citation Format

Share Document