Fastener Lightning Current Assessment in Aircraft Fuel Tank

2019 ◽  
Author(s):  
P. Monferran ◽  
C. Guiffaut ◽  
A. Reineix ◽  
F. Fustin ◽  
F. Tristant
Keyword(s):  
Fuel Tank ◽  
Lightning Current ◽  
Aircraft Fuel ◽  
Current Assessment

scholarly journals Lightning Currents on Fastening Assemblies of an Aircraft Fuel Tank—Part III: Validation of the Current Assessment Method With Measurement

2020 ◽  
Vol 62 (5) ◽  
pp. 2174-2185
Author(s):  
Paul Monferran ◽  
Christophe Guiffaut ◽  
Alain Reineix ◽  
Fabian Fustin ◽  
Fabrice Tristant
Keyword(s):  
Assessment Method ◽  
Fuel Tank ◽  
Aircraft Fuel ◽  
Current Assessment

scholarly journals Development of a Novel Test Rig for the Evaluation of Aircraft Fuel Tank Sealant

2012 ◽  
Vol 40 (1) ◽  
pp. 103420
Author(s):  
M. R. Mitchell ◽  
R. E. Link ◽  
M. N. Hooper ◽  
A. R. Hutchinson ◽  
J. G. Broughton ◽  
...  
Keyword(s):  
Fuel Tank ◽  
Test Rig ◽  
Aircraft Fuel

Raw Scanned Point Cloud Registration with Repetition for Aircraft Fuel Tank Inspection

2021 ◽  
pp. 103164
Author(s):  
Xuanming Cao ◽  
Xiaoxi Gong ◽  
Qian Xie ◽  
Jiayi Huang ◽  
Yabin Xu ◽  
...  
Keyword(s):  
Point Cloud ◽  
Fuel Tank ◽  
Point Cloud Registration ◽  
Aircraft Fuel

Key Protective Techniques Study for Strain Gauges in the Oil-Water Mixture and Pressurization Environment

2013 ◽  
Vol 401-403 ◽  
pp. 912-915 ◽  
Author(s):  
Jia Zuo ◽  
Jian Feng Zhang ◽  
Shen Ke Teng
Keyword(s):  
Survival Rate ◽  
Protective Coating ◽  
Fuel Tank ◽  
Strain Gauges ◽  
Lead Wire ◽  
Static Fatigue ◽  
Water Mixture ◽  
Aircraft Fuel ◽  
Oil Water ◽  
Protective Performance

In order to improve the survival rate of the strain gauges in the oil-water mixture and pressurization environment in the static/fatigue test of aircraft fuel tank, some key installing and protecting techniques were researched. The protective performance of single and double covering with Different protective agents, the various treatment scopes on the specimen and different lengths of lead wire embedded in the protective coating were investigated in a fuel tank which was designed and manufactured specially for the contrast test. Several effective protective techniques are gained, and when these techniques are applied to the practice, a satisfactory survival rate of strain gauges is reached.

scholarly journals On the influence of filling level in CFRP aircraft fuel tank subjected to high velocity impacts

2014 ◽  
Vol 107 ◽  
pp. 570-577 ◽  
Author(s):  
J.A. Artero-Guerrero ◽  
J. Pernas-Sánchez ◽  
J. López-Puente ◽  
D. Varas
Keyword(s):  
High Velocity ◽  
Fuel Tank ◽  
Aircraft Fuel ◽  
High Velocity Impacts

scholarly journals Method of Aircraft Fuel Tank System Ignition Source Fail-Safe Feature Analysis

2011 ◽  
Vol 17 ◽  
pp. 638-644 ◽  
Author(s):  
Zhang Yanjun ◽  
Sun Youchao ◽  
Wang Fengchan ◽  
Zeng Haijun
Keyword(s):  
Fuel Tank ◽  
Ignition Source ◽  
Feature Analysis ◽  
Aircraft Fuel ◽  
Tank System ◽  
Fail Safe

scholarly journals Effect of fuel type on the performance of an aircraft fuel tank oxygen-consuming inerting system

2021 ◽  
Vol 34 (3) ◽  
pp. 82-93
Author(s):  
Xiaotian PENG ◽  
Shiyu FENG ◽  
Chaoyue LI ◽  
Chen CHEN ◽  
Weihua LIU
Keyword(s):  
Fuel Tank ◽  
Fuel Type ◽  
Aircraft Fuel ◽  
Inerting System

Numerical Study of the Influence of Ambient Pressure on the Inerting Effect of an Aircraft Fuel Tank Inerting System

2014 ◽  
Vol 1061-1062 ◽  
pp. 1140-1143
Author(s):  
Dong Jie Liu
Keyword(s):  
Dissolved Oxygen ◽  
Oxygen Concentration ◽  
Numerical Study ◽  
Ambient Pressure ◽  
Ideal Gas ◽  
Fuel Tank ◽  
Dissolved Oxygen Concentration ◽  
State Equations ◽  
Aircraft Fuel ◽  
Inerting System

The numerical study of the influence of the ambient pressure of the fuel tank on the inerting effect of an aircraft fuel tank inerting system was carried out. The mathematical model of ullage equilibrium oxygen concentration has been established using the differential time calculation method based on the mass conservation and ideal gas state equations. The variations of ullage oxygen concentration and dissolved oxygen concentration in the fuel with time under different working conditions have been obtained. The results have shown that the as the ambient pressure of the fuel tank became lower, the speed of the decreasing of oxygen concentration of the fuel tank ullge and the dissolved oxygen concentration of the fuel was slower.

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