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2020•IOP Conference Series Materials Science and EngineeringOpen access

Prospective helicopter crash-resistance fuel systems testing

S. V. Grachev, Денис Игоревич Смагин, Роман Сергеевич Савельев, Константин Сергеевич Напреенко

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Abstract

Abstract This article discusses the main requirements for testing helicopter fuel systems in accordance with the regulatory documentation. The analysis of existing solutions for testing aircraft fuel systems both in Russia and abroad was carried out. The concept of a test complex designed for testing fuel systems of helicopters is presented, which includes rotary platforms designed to simulate different angular positions of test objects, technological equipment, and a set of mathematical modeling tools. This test facility allows for joint full-scale and digital tests of the fuel system at all stages of the helicopter’s life cycle.

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What this paper is about

Abstract This article discusses the main requirements for testing helicopter fuel systems in accordance with the regulatory documentation. The analysis of existing solutions for testing aircraft fuel systems both in Russia and abroad was carried out. The concept of a test complex designed for testing fuel systems of helicopters is presented, which includes rotary platforms designed to simulate different angular positions of test objects, technological equipment, and a set of mathematical modeling tools. This test facility allows for joint full-scale and digital tests of the fuel system at all stages of the helicopter’s life cycle.

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Available abstract

Abstract This article discusses the main requirements for testing helicopter fuel systems in accordance with the regulatory documentation. The analysis of existing solutions for testing aircraft fuel systems both in Russia and abroad was carried out. The concept of a test complex designed for testing fuel systems of helicopters is presented, which includes rotary platforms designed to simulate different angular positions of test objects, technological equipment, and a set of mathematical modeling tools. This test facility allows for joint full-scale and digital tests of the fuel system at all stages of the helicopter’s life cycle.

Key concepts: Crash, Documentation, Engineering, Systems engineering, Test (biology), Automotive engineering, Set (abstract data type), Aeronautics

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