Optimization Study of Inert Gas Distribution for Multiple-Bay Fuel Tank

Author:

Shao Lei12ORCID,He Jiawei12,Lu Xia3,Liu Weihua4

Affiliation:

1. School of Aeronautics, Chongqing Jiaotong University, Chongqing 400074, China

2. The Green Aerotechnics Research Institute of Chongqing Jiaotong University, Chongqing 401135, China

3. AVIC Hefei Jianghuai Aircraft Equipment Co., Ltd., Aviation Industry Corporation of China, Hefei 230051, China

4. School of Aeronautics, Nanjing University of Aeronautics and Astronautics, Nanjing 210007, China

Abstract

Inert gas distribution has a great influence on the inerting effect, especially for the multiple-bay fuel tank. In order to find out the optimal scheme, an optimization method based on the entropy-weight improvement TOPSIS method is proposed, and an experimental system of inert gas distribution is established to measure the speed index and uniformity index. The results show that the position of the inlet and outlet has a significant effect on the overall inerting effect. The inerting scheme designed by the entropy-weight improvement TOPSIS method can not only reduce the flow demand of inert gas but also make the oxygen distribution more uniform. The optimization inerting scheme of the Boeing 747 aircraft has improved the average speed index by 3.01% and the average uniformity index by 26.18%. The smoke visualization experiment also showed that the scheme designed by the entropy-weight improvement TOPSIS method has the denser white smoke, which means that the scheme has better performance.

Funder

National Natural Science Foundation of China—Civil Aviation Research Fund

Research Fund of Key Laboratory of Aircraft Environment Control and Life Support, MIIT, Nanjing University of Aeronautics and Astronautics

Science and Technology Research Program of Chongqing Municipal Education Commission

Natural Science Foundation of Chongqing, China

Publisher

MDPI AG

Subject

Process Chemistry and Technology,Chemical Engineering (miscellaneous),Bioengineering

Reference29 articles.

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2. Electrochemical gas separation and inerting system;Aryal;J. Power Sources,2021

3. Boeing Phantom Works (2001). Report No.: NASA/CR 2001-210950, Boeing Phantom Works.

4. Summer, S.M. (1999). Mass Loading Effects on Fuel Vapor Concentration in an Aircraft Fuel Tank Ullage.

5. Federal Aviation Administration (1999). Report No.: DOT/FAA/AR-TN99/65.

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