Research status and development trend of air-breathing high-speed vehicle/engine integration

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2024-10-18 DOI:10.1016/j.ast.2024.109675
Shibin Luo , Yuhang Sun , Jun Liu , Xun Xie , Jiaqi Tian , Jiawen Song
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Abstract

Air-breathing vehicles, a crucial field of the aerospace industry in recent years, are required to have exceptional flight performance in a wide range. As a practical and essential way to realize efficient flight, the integration design emerges as a prominent characteristic of air-breathing vehicles. This article reviews and analyzes the design connotation, critical progress, and technical attributes of high-speed air-breathing integration vehicles, including supersonic aerodynamics/propulsion integration, hypersonic cruise-type airframe/engine integration, and wide-range aircraft/engine integration. In the supersonic aerodynamics/propulsion integrated design phase, creating a vehicle with excellent maneuverability and stealth performance has become the design focus. While in the hypersonic cruise-type airframe/engine integrated design phase, designers proposed various rotational symmetrical slender body and lifting-body configurations to match the scramjet engines. This provided strong support for breaking through thrust-drag matching in hypersonic cruise. For wide-range aircraft/engine integration vehicles, a more complex service environment imposes higher requirements on their levels of integration. The progression from supersonic aerodynamics/propulsion integration to hypersonic cruise-type airframe/engine integration, and further to wide-range aircraft/engine integration, signifies the exploration of air-breathing aircraft towards wider speed range and broader airspace. Finally, a detailed analysis of the distinctions among these three types of integrated vehicles is presented, and the development proposals and trends of wide-range aircraft/engine integration vehicles are discussed.
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喷气式高速飞行器/发动机集成的研究现状和发展趋势
空气呼吸飞行器是近年来航空航天工业的一个重要领域,要求其在大范围内具有优异的飞行性能。作为实现高效飞行的重要实用途径,一体化设计成为喷气飞行器的突出特点。本文从超音速气动/推进一体化、高超声速巡航型机体/发动机一体化、大航程飞行器/发动机一体化等方面,对高速喷气式一体化飞行器的设计内涵、关键进展和技术特性进行了回顾和分析。在超音速气动/推进一体化设计阶段,设计的重点是创造一种具有优异机动性和隐身性能的飞行器。而在高超声速巡航型机体/发动机集成设计阶段,设计人员提出了各种旋转对称的细长机体和升力机体构型,以匹配涡喷发动机。这为在高超音速巡航中突破推力-阻力匹配提供了有力支持。对于大范围的飞机/发动机集成飞行器来说,更复杂的服役环境对其集成水平提出了更高的要求。从超音速气动/推进集成到高超声速巡航型机体/发动机集成,再到大航程飞行器/发动机集成,标志着喷气式飞行器正朝着更宽的速度范围和更广阔的空域探索。最后,详细分析了这三类集成飞行器的区别,并讨论了大航程飞机/发动机集成飞行器的发展建议和趋势。
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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