CN116066257A - Mixed fuel supply device for liquid hydrocarbon fuel cracking gas carrying flow solid fuel - Google Patents

Mixed fuel supply device for liquid hydrocarbon fuel cracking gas carrying flow solid fuel Download PDF

Info

Publication number
CN116066257A
CN116066257A CN202310094666.7A CN202310094666A CN116066257A CN 116066257 A CN116066257 A CN 116066257A CN 202310094666 A CN202310094666 A CN 202310094666A CN 116066257 A CN116066257 A CN 116066257A
Authority
CN
China
Prior art keywords
fuel
storage chamber
solid fuel
supply device
fuel supply
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN202310094666.7A
Other languages
Chinese (zh)
Inventor
章思龙
左婧滢
郭玉杰
韦健飞
李欣
鲍文
秦江
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Harbin Institute of Technology Shenzhen
Original Assignee
Harbin Institute of Technology Shenzhen
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Harbin Institute of Technology Shenzhen filed Critical Harbin Institute of Technology Shenzhen
Priority to CN202310094666.7A priority Critical patent/CN116066257A/en
Publication of CN116066257A publication Critical patent/CN116066257A/en
Pending legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/14Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines with external combustion, e.g. scram-jet engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22Fuel supply systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

The invention relates to the technical field of ramjet engines, in particular to a mixed fuel supply device for carrying solid fuel with liquid hydrocarbon fuel pyrolysis gas, which comprises a fuel storage chamber, wherein a piston for pushing the solid fuel is slidably arranged in the fuel storage chamber, the fuel storage chamber is communicated with a gas collecting bin, the device is provided with the gas collecting bin, macromolecule hydrocarbon fuel pyrolysis gas enters a circumferential gas collecting chamber through three gas inlets, a flow guide circular table is arranged in the circumferential gas collecting chamber, the pyrolysis gas shears and flows the solid fuel in a radial centripetal manner through a slit between the flow guide circular table and an air outlet baffle, the carrying and mixing of the solid fuel are effectively realized through the shearing flow, the device is provided with an air inlet slit of the pyrolysis gas, the slit is composed of a flow guide table and the baffle, the slit distance is small, and even a small amount of pyrolysis gas still has a large speed to shear and carry the solid fuel through the slit.

Description

液体碳氢燃料裂解气携流固体燃料的混合燃料供给装置Mixed fuel supply device for liquid hydrocarbon fuel cracking gas carrying solid fuel

技术领域technical field

本发明涉及冲压发动机技术领域,具体涉及液体碳氢燃料裂解气携流固体燃料的混合燃料供给装置。The invention relates to the technical field of ramjet engines, in particular to a mixed fuel supply device for liquid hydrocarbon fuel cracking gas carrying solid fuel.

背景技术Background technique

固液混合高马赫冲压发动机是一种新概念发动机,它同时采用固体粉末和液体燃料作为推进剂。其工作过程原理为:液体燃料通过再生冷却通道对超声速燃烧室进行冷却,产生高温、高密度的燃油裂解气或蒸汽,裂解气以气力输运的方式实现对固体粉末燃料的流化、掺混、喷射并进入燃烧室进行燃烧,利用喷气推进原理产生推力。The solid-liquid mixed high Mach ramjet engine is a new concept engine, which uses both solid powder and liquid fuel as propellants. The principle of its working process is: the liquid fuel cools the supersonic combustion chamber through the regenerative cooling channel to generate high-temperature, high-density fuel cracking gas or steam, and the cracking gas realizes the fluidization and mixing of solid powder fuel by means of pneumatic transport , inject and enter the combustion chamber for combustion, and use the principle of jet propulsion to generate thrust.

这种新概念的固液混合高马赫冲压发动机采用高能金属或硼粉作为固体推进剂,兼具液体燃料冲压发动机推力可调、流量调节灵活、比冲高及固体火箭冲压发动机安全可靠、结构简单等优点。对于使用粉末燃料的冲压发动机,固体粉末本身没有流动属性,因此流量可调控性差、燃烧室的热防护依赖于耐高温材料的被动热防护、同时固体粉末在燃烧室内不容易点火燃烧,使用金属粉末颗粒作为燃料的好处是金属粉末化学性质稳定,安全性好、存储方便,作战反应时间短,同时燃烧产物为高沸点的金属氧化物,不易离解。使用液体燃料通过再生冷却通道产生的裂解气携流固体粉末颗粒,使得固体粉末颗粒获得了流动属性,流量可调控性大大增强。裂解气的点火燃烧能够作为固体颗粒的点火源,改善燃烧室的点火燃烧特性。燃料在裂解过程中的吸热特性,能够为燃烧室的热防护做出贡献。This new concept of solid-liquid mixed high Mach ramjet uses high-energy metal or boron powder as solid propellant, and has the advantages of adjustable thrust, flexible flow adjustment, high specific impulse of liquid fuel ramjet and safety, reliability and simple structure of solid rocket ramjet Etc. For the ramjet using powder fuel, the solid powder itself has no flow properties, so the flow controllability is poor, the thermal protection of the combustion chamber depends on the passive thermal protection of high-temperature resistant materials, and at the same time, the solid powder is not easy to ignite and burn in the combustion chamber, so metal powder is used The advantage of particles as fuel is that the metal powder has stable chemical properties, good safety, convenient storage, short combat reaction time, and the combustion product is a metal oxide with a high boiling point, which is not easy to dissociate. The pyrolysis gas generated by using liquid fuel through the regenerative cooling channel carries the solid powder particles, so that the solid powder particles obtain flow properties, and the flow controllability is greatly enhanced. The ignition and combustion of the cracked gas can be used as an ignition source for solid particles to improve the ignition and combustion characteristics of the combustion chamber. The endothermic properties of the fuel during pyrolysis contribute to the thermal protection of the combustion chamber.

发动机在长时间运行过程中,需要持续消耗混合燃料,混合燃料气固两相区掺混均匀后在燃烧室内与来流空气发生进一步掺混后点火燃烧。During the long-term operation of the engine, the mixed fuel needs to be continuously consumed. After the mixed fuel is evenly mixed in the gas-solid two-phase region, it is further mixed with the incoming air in the combustion chamber and then ignited and burned.

发明内容Contents of the invention

本发明的目的是提供一种固液混合超燃冲压发动机混合燃料供给装置。微米级高能固体燃料由活塞推动,在大分子碳氢燃料裂解气的剪切携流作用下,获得流动属性,与发动机多工况运行条件相适应,实现固液混合超燃冲压发动机混合燃料供给气固两相掺混均匀的功能。The object of the present invention is to provide a solid-liquid mixed scramjet mixed fuel supply device. The micron-sized high-energy solid fuel is propelled by the piston, and under the action of the shear entrainment of the cracked gas of the macromolecular hydrocarbon fuel, it obtains flow properties, adapts to the multi-working conditions of the engine, and realizes the mixed fuel supply of the solid-liquid mixed scramjet engine The gas-solid two-phase mixing function is uniform.

本发明采用的技术方案在于:包括用于大分子液体碳氢燃料推动的柱塞泵、用于大分子液体碳氢燃料裂解的再生冷却通道,和对固体燃料进行携流掺混的燃料供给装置;The technical scheme adopted by the present invention is: including a plunger pump for driving macromolecular liquid hydrocarbon fuel, a regenerative cooling channel for cracking macromolecular liquid hydrocarbon fuel, and a fuel supply device for entraining and mixing solid fuel ;

所述燃料供给装置包含燃料贮室,燃料贮室内滑动安装有用于固体燃料推动的活塞,燃料贮室连通有集气仓。The fuel supply device includes a fuel storage chamber, in which a piston for pushing solid fuel is slidably installed, and the fuel storage chamber is communicated with a gas collection bin.

进一步地,所述燃料贮室分为贮室直段、贮室收缩段和细直段三个部分。Further, the fuel storage chamber is divided into three parts: the straight section of the storage chamber, the constricted section of the storage chamber and the thin straight section.

进一步地,所述集气仓两端安装有挡板,分别为前挡板和后挡板,前挡板偏心位置设置有进气孔,贮室细直段远离贮室收缩段的一端设置有导流台,导流台与后挡板之间形成有狭缝。Further, baffles are installed at both ends of the gas-collecting bin, which are respectively a front baffle and a rear baffle, an air inlet is provided at the eccentric position of the front baffle, and an end of the thin straight section of the storage chamber away from the contracted section of the storage chamber is provided with a The deflector, a slit is formed between the deflector and the tailgate.

进一步地,所述进气孔设置有三个。Further, there are three air intake holes.

进一步地,所述活塞上设置有活塞杆,活塞杆安装在电机的输出端。Further, the piston is provided with a piston rod, and the piston rod is installed at the output end of the motor.

进一步地,所述贮室直段远离贮室收缩端的一端设置有圆台,其远离贮室直段的一端安装有挡板,活塞杆滑动安装在挡板上。Further, the end of the straight section of the storage chamber away from the shrinking end of the storage chamber is provided with a circular platform, and the end of the straight section of the storage chamber away from the straight section of the storage chamber is installed with a baffle plate, and the piston rod is slidably installed on the baffle plate.

进一步地,所述挡板与活塞杆之间安装有滑动轴承。Further, a sliding bearing is installed between the baffle plate and the piston rod.

进一步地,所述后挡板与前挡板通过螺栓相连接。Further, the rear baffle is connected to the front baffle by bolts.

进一步地,所述后挡板上安装有掺混管。Further, a blending pipe is installed on the tailgate.

进一步地,所述柱塞泵的输出位置设置有流量调节阀。Further, the output position of the plunger pump is provided with a flow regulating valve.

本发明的有益效果是:The beneficial effects of the present invention are:

本装置设置了集气仓,大分子碳氢燃料裂解气通过三个进气孔进入周向集气室,周向集气室内设有导流圆台,裂解气通过导流圆台和出气挡板之间的狭缝沿径向向心对固体燃料进行剪切流动,剪切流动有效的实现了对固体燃料的携带和掺混,本装置设置了裂解气的进气狭缝,狭缝由导流台和挡板组成,狭缝距离较小,即使少量的裂解气通过狭缝依然具有较大的速度对固体燃料进行剪切携流,通过控制电机的转速可实现对固体燃料流量的控制;裂解气流量的调控可通过裂解气分流前管道阀门进行控制;实现了混合燃料单相流量的分别调节,混合燃料的固气比可调范围广,与发动机款工况运行条件相匹配。The device is equipped with a gas collection chamber. The pyrolysis gas of macromolecular hydrocarbon fuel enters the circumferential gas collection chamber through three air inlets. The slit between the solid fuels shears the flow radially and centripetally, and the shearing flow effectively realizes the carrying and mixing of the solid fuel. Composed of table and baffle plate, the slit distance is small, even if a small amount of cracked gas passes through the slit, it still has a relatively high speed to shear and carry the solid fuel, and the flow control of the solid fuel can be realized by controlling the speed of the motor; pyrolysis The regulation of the gas flow can be controlled by the pipeline valve before splitting the cracked gas; the single-phase flow of the mixed fuel can be adjusted separately, and the solid-gas ratio of the mixed fuel can be adjusted in a wide range, which matches the operating conditions of the engine model.

附图说明Description of drawings

图1是本发明所述液体碳氢燃料裂解气携流固体燃料的混合燃料供给装置的结构示意图;Fig. 1 is the structural representation of the mixed fuel supply device of liquid hydrocarbon fuel cracking gas carrying flow solid fuel of the present invention;

图2是本发明所述燃料供给装置的示意图;Fig. 2 is a schematic diagram of the fuel supply device of the present invention;

图3是本发明所述燃料供给装置的截面结构示意图;Fig. 3 is a schematic cross-sectional structure diagram of the fuel supply device of the present invention;

图中:储油罐1;柱塞泵2;流量调节阀3;再生冷却通道4;燃料供给装置5;活塞杆51;密封圈52;挡板53;活塞54;燃料贮室55;集气仓56;挡板53;进气孔57;挡板53;导流台58;掺混管59;电机6。In the figure: oil storage tank 1; plunger pump 2; flow regulating valve 3; regenerative cooling passage 4; fuel supply device 5; piston rod 51; sealing ring 52; baffle plate 53; piston 54; fuel storage chamber 55; gas collection Storehouse 56; baffle plate 53; air intake hole 57; baffle plate 53; flow guide table 58; mixing pipe 59;

具体实施方式:Detailed ways:

实施例1Example 1

针对飞行马赫数8~10的飞行任务,提出了一种使用液体燃料裂解气携带固体粉末颗粒作为燃料的高马赫数超燃冲压发动机,称为固液混合超燃冲压发动机。该发动机的燃料供给装置需要实现液体碳氢燃料将固体粉末颗粒流化、相互掺混并带入燃料室燃烧。本发明给出了该发动机一种燃料供给装置,固体燃料储存在燃料贮室55中,液体碳氢燃料储存在储油罐1中,发动机实际运行中,液体碳氢燃料首先流经发动机燃烧室壁面的再生冷却通道,在再生冷却通道高温高压的环境下,液体碳氢燃料裂解称为小分子的燃油裂解气,冷却通道出口的裂解气从集气仓56进气孔进入,从集气仓56的狭缝流出,对由活塞54进行推动的固体燃料进行剪切携流,在掺混管59进行掺混,随后进入发动机燃烧室内进行燃烧。Aiming at flight missions with a Mach number of 8-10, a high Mach number scramjet using liquid fuel pyrolysis gas to carry solid powder particles as fuel is proposed, which is called a solid-liquid hybrid scramjet. The fuel supply device of the engine needs to realize that the liquid hydrocarbon fuel fluidizes the solid powder particles, mixes them with each other and brings them into the fuel chamber for combustion. The present invention provides a fuel supply device for the engine. The solid fuel is stored in the fuel storage chamber 55, and the liquid hydrocarbon fuel is stored in the oil storage tank 1. During the actual operation of the engine, the liquid hydrocarbon fuel first flows through the combustion chamber of the engine. The regenerative cooling channel on the wall, under the high temperature and high pressure environment of the regenerative cooling channel, the liquid hydrocarbon fuel is cracked into fuel oil cracking gas called small molecules, and the cracking gas at the outlet of the cooling channel enters from the air inlet of the gas collection chamber 56, and from the gas collection chamber The flow out through the slit of the piston 56 carries out shear entrainment to the solid fuel pushed by the piston 54, mixes it in the mixing tube 59, and then enters the combustion chamber of the engine for combustion.

本发明涉及液体碳氢燃料裂解气携流固体燃料的混合燃料供给装置,包括用于大分子液体碳氢燃料推动的柱塞泵2,柱塞泵3将储油罐1内大分子液体碳氢燃料推动进入至超燃冲压发动机的再生冷却通道4后,大分子液体碳氢燃料吸热裂解为小分子的裂解气,再生冷却通道4出口的裂解气进入燃料供给装置5,燃料供给装置5实现对固体燃料进行携流掺混的功能。The invention relates to a mixed fuel supply device for liquid hydrocarbon fuel cracking gas carrying solid fuel, comprising a plunger pump 2 for driving macromolecular liquid hydrocarbon fuel, and a plunger pump 3 to drive the macromolecular liquid hydrocarbon in an oil storage tank 1 After the fuel is pushed into the regenerative cooling channel 4 of the scramjet engine, the macromolecular liquid hydrocarbon fuel absorbs heat and cracks into small molecule cracked gas, and the cracked gas at the outlet of the regenerative cooling channel 4 enters the fuel supply device 5, and the fuel supply device 5 realizes The function of entrainment mixing of solid fuels.

所述燃料供给装置5包含燃料贮室55,固体燃料位于燃料贮室55内,燃料贮室55内滑动安装有用于固体燃料推动的活塞54,燃料贮室55连通有集气仓56,固体燃料经由活塞54推动进入至集气仓56,燃料贮室55与集气仓56同轴布置,集气仓56内设置有狭缝,液体碳氢燃料裂解气由发动机再生冷却通道4产生后进入集气仓56,并自集气仓56出口的周向狭缝流出,实现对固体燃料进行剪切、携流和掺混的功能。The fuel supply device 5 includes a fuel storage chamber 55. The solid fuel is located in the fuel storage chamber 55. A piston 54 for solid fuel is slidably installed in the fuel storage chamber 55. The fuel storage chamber 55 is connected with a gas collection bin 56. The solid fuel Pushed by the piston 54 into the gas collection chamber 56, the fuel storage chamber 55 is coaxially arranged with the gas collection chamber 56, and a slit is arranged in the gas collection chamber 56, and the liquid hydrocarbon fuel cracking gas is generated by the engine regenerative cooling passage 4 and then enters the collection chamber. The gas chamber 56 flows out from the circumferential slit at the outlet of the gas collection chamber 56, and realizes the functions of shearing, carrying and mixing the solid fuel.

大分子液体碳氢燃料:航空发动机广泛使用航空煤油RP-3作为燃料,其单位分子平均含碳量约为10,研究人员一般使用正癸烷作为替代物。化学动力学研究中,将含碳量较小的分子叫做小分子碳氢燃料,如C1-C4,此时为燃料气态,将含碳量较高的叫做大分子碳氢燃料,如C10,C11。“大分子碳氢燃料”已广泛出现在多个文献中,如哈尔滨工业大学的左婧滢在《超燃冲压发动机碳氢燃料气膜的冷却和减阻特性研究》中提到使用高温气态大分子碳氢燃料组织超声速气膜,香港理工大学的池奕承在《大分子支链烷烃CnH2n+2+(H,OH,HO2)夺氢反应高精度理论热化学研究》提到发展大分子碳氢燃料高精度化学反应机理对发展航空煤油化学反应机理至关重要。Macromolecular liquid hydrocarbon fuel: Aviation kerosene RP-3 is widely used as fuel in aviation engines, and its average carbon content per unit molecule is about 10. Researchers generally use n-decane as a substitute. In the study of chemical kinetics, the molecules with a small carbon content are called small molecule hydrocarbon fuels, such as C1-C4, which are in the fuel gaseous state at this time, and those with higher carbon content are called macromolecular hydrocarbon fuels, such as C10, C11 . "Macromolecular hydrocarbon fuels" have been widely used in many documents. For example, Zuo Jingying from Harbin Institute of Technology mentioned the use of high-temperature gaseous large Molecular hydrocarbon fuel organizes supersonic gas film. Chi Yicheng of Hong Kong Polytechnic University mentioned the development of macromolecular carbon The high-precision chemical reaction mechanism of hydrogen fuel is crucial to the development of aviation kerosene chemical reaction mechanism.

吸热裂解条件及完成工作段:在超燃冲压发动机实际运行中,燃烧室核心温度可达2500K,已远远超过发动机材料的熔点,因此,实际运行过程中需要对发动机燃烧室壁面进行冷却,防止发动机烧毁,再生冷却是一种广泛使用的冷却方式。通过在发动机燃烧室壁面铸造再生冷却通道4,使液体燃料在进入燃烧室燃烧之前,先通过再生冷却通道4,利用燃料的物理热沉和化学热沉对壁面进行冷却。由于燃烧室内部为高压,再生冷却通道4出口与燃烧室相通,因此再生冷却通道内部也为高压环境,同时冷却通道壁面为发动机燃烧室壁面,通道内温度非常高,在高温高压环境下,大分子液体碳氢燃料通过发动机再生冷却通道时,会裂解为小分子的碳氢燃料。Endothermic cracking conditions and completion of the work section: In the actual operation of the scramjet engine, the core temperature of the combustion chamber can reach 2500K, which has far exceeded the melting point of the engine material. Therefore, the wall of the engine combustion chamber needs to be cooled during the actual operation. To prevent engine burnout, regenerative cooling is a widely used cooling method. By casting the regenerative cooling passage 4 on the wall of the combustion chamber of the engine, the liquid fuel passes through the regenerative cooling passage 4 before entering the combustion chamber for combustion, and the wall is cooled by the physical heat sink and the chemical heat sink of the fuel. Since the interior of the combustion chamber is under high pressure, the outlet of regenerative cooling channel 4 communicates with the combustion chamber, so the inside of the regenerative cooling channel is also in a high-pressure environment. At the same time, the wall of the cooling channel is the wall of the engine combustion chamber, and the temperature in the channel is very high. Under high temperature and high pressure environment, large Molecular liquid hydrocarbon fuels are cracked into small molecular hydrocarbon fuels as they pass through the engine regeneration cooling passages.

因此,裂解吸热的条件是发动机再生冷却通道4内的高温高压环境,在燃烧室壁面的再生冷却通道4内完成,利用大分子液体碳氢燃料的物理热沉和裂解反应吸热的化学热沉实现了对发动机燃烧室壁面的冷却。裂解反应需要在高温高压条件下实现,而燃烧室壁面的再生冷却通道具备这一条件。Therefore, the conditions for pyrolysis to absorb heat are the high-temperature and high-pressure environment in the regenerative cooling channel 4 of the engine, which is completed in the regenerative cooling channel 4 on the wall of the combustion chamber, utilizing the physical heat sink of the macromolecular liquid hydrocarbon fuel and the chemical heat of the pyrolysis reaction endothermic The sink realizes the cooling of the wall of the engine combustion chamber. The cracking reaction needs to be realized under high temperature and high pressure conditions, and the regenerative cooling channel on the wall of the combustion chamber has this condition.

实施例2Example 2

在实施例1的基础上,本实施例中,所述燃料贮室55分为贮室直段、贮室收缩段和细直段三个部分,贮室收缩段为圆锥状,固体燃料受活塞54推动的作用,固体燃料自贮室直段依次通过贮室收缩段和细直段进入至集气仓56,由于在固体燃料推动过程中,燃料贮室55内径逐渐变小,从而实现控制固体燃料的流速,使固体燃料进入集气仓56的位置位于集气仓56的中心位置。On the basis of Embodiment 1, in this embodiment, the fuel storage chamber 55 is divided into three parts: the straight section of the storage chamber, the contracted section of the storage chamber and the thin straight section. The contracted section of the storage chamber is conical, and the solid fuel is received by the piston. 54, the solid fuel enters the gas collection chamber 56 from the straight section of the storage chamber through the contracted section and the thin straight section of the storage chamber in turn. Since the internal diameter of the fuel storage chamber 55 gradually becomes smaller during the pushing process of the solid fuel, the control of solid fuel is realized. The flow rate of the fuel makes the position where the solid fuel enters the gas collection bin 56 be located at the center of the gas collection bin 56 .

实施例3Example 3

在实施例2的基础上,本实施例中,所述集气仓56为环装结构,其两端均安装有挡板53,分别为前挡板和后挡板,挡板53为环形薄片状,其中前挡板套装在贮室收缩段的外壁上,其安装方式选用铸造方式,(也可采用压接和焊接等已知技术手段),后挡板与集气仓56之间安装有密封圈52,通过两个挡板53实现对集气仓56密封的功能,前挡板偏心位置设置有进气孔57,贮室细直段远离贮室收缩段的一端设置有导流台58,导流台58同轴布置在贮室收缩段的外壁上,导流台58与后挡板之间形成有狭缝,导流台58为环装结构,其远离贮室收缩段的边线上倒有缓冲圆角,进气孔57进入的液体碳氢燃料裂解气作用在导流台58上,经由导流台58导流引向,使液体碳氢燃料裂解气向导流台58四周流动,从而控制液体碳氢燃料裂解气流向,实现对集气仓56内的固体燃料进行剪切、携流和掺混的功能。On the basis of Embodiment 2, in this embodiment, the gas-collecting bin 56 is a ring-mounted structure, and baffles 53 are installed at both ends thereof, which are respectively a front baffle and a rear baffle, and the baffle 53 is an annular sheet shape, wherein the front baffle is set on the outer wall of the shrinkage section of the storage chamber, and the installation method is cast, (known technical means such as crimping and welding can also be used), and the rear baffle and the gas collection bin 56 are installed The sealing ring 52 realizes the function of sealing the gas collection chamber 56 through two baffles 53, the eccentric position of the front baffle is provided with an air inlet 57, and the end of the thin straight section of the storage chamber away from the contracted section of the storage chamber is provided with a deflector 58 , the deflector 58 is coaxially arranged on the outer wall of the contracted section of the storage chamber, a slit is formed between the deflector 58 and the rear baffle, and the deflector 58 is a ring-mounted structure, which is far away from the sideline of the contracted section of the storage chamber There are buffer fillets, and the liquid hydrocarbon fuel cracking gas entering the air inlet 57 acts on the guide table 58, and guides the flow through the guide table 58, so that the liquid hydrocarbon fuel cracking gas flows around the guide table 58, In this way, the cracking gas flow direction of the liquid hydrocarbon fuel is controlled, and the functions of shearing, entraining and mixing the solid fuel in the gas collection bin 56 are realized.

实施例4Example 4

在实施例2的基础上,本实施例中,所述进气孔57设置有三个,三个进气孔57沿前挡板周向均匀布置,从而增加集气仓56内气相分布均匀程度,保证狭缝处气体径向流动状态稳定,对固体燃料实现剪切携流的功能。On the basis of Embodiment 2, in this embodiment, there are three air inlets 57, and the three air inlets 57 are evenly arranged along the circumference of the front baffle, thereby increasing the uniformity of gas phase distribution in the gas collection bin 56, Ensure the stability of the gas radial flow state at the slit, and realize the function of shearing and entraining the solid fuel.

实施例5Example 5

在实施例1的基础上,本实施例中,所述活塞54上设置有活塞杆51,活塞杆51安装在电机6的输出端,并通过电机6驱动,通过控制电机6的转速可实现对固体燃料流量的控制,活塞54的外壁上开设有环形凹槽,环形凹槽与贮室直段内壁之间安装有密封圈,实现密封的功能,防止固体燃料自贮室直段内壁与活塞54之间渗出。On the basis of Embodiment 1, in this embodiment, the piston 54 is provided with a piston rod 51, the piston rod 51 is installed on the output end of the motor 6, and is driven by the motor 6. By controlling the speed of the motor 6, the To control the flow of solid fuel, an annular groove is formed on the outer wall of the piston 54, and a sealing ring is installed between the annular groove and the inner wall of the straight section of the storage chamber to realize the function of sealing and prevent the solid fuel from flowing from the inner wall of the straight section of the storage chamber to the piston 54. oozes between.

实施例6Example 6

在实施例2的基础上,本实施例中,所述贮室直段远离贮室收缩端的一端设置有圆台,圆台为环形薄片状,其远离贮室直段的一端安装有挡板,挡板为圆形薄片状,挡板与圆台通过螺栓相连接,挡板的中心位置开设有孔并铸有环形凸台,活塞杆51安装在环形凸台内,活塞杆51能够在环形凸台内自由滑动。On the basis of Embodiment 2, in this embodiment, the end of the straight section of the storage chamber away from the contracting end of the storage chamber is provided with a circular platform, the circular platform is in the shape of an annular sheet, and a baffle is installed at the end of the straight section of the storage chamber. It is in the shape of a circular sheet, and the baffle plate is connected with the round platform by bolts. A hole is opened in the center of the baffle plate and an annular boss is cast. The piston rod 51 is installed in the annular boss, and the piston rod 51 can move freely in the annular boss. slide.

实施例7Example 7

在实施例6的基础上,本实施例中,所述环形凸台与活塞杆51之间安装有滑动轴承,所述滑动轴承内测设置有滚珠,从而减小了活塞杆51与滑动轴承之间的摩擦力。On the basis of Embodiment 6, in this embodiment, a sliding bearing is installed between the annular boss and the piston rod 51, and the inside of the sliding bearing is provided with balls, thereby reducing the distance between the piston rod 51 and the sliding bearing. friction between them.

实施例8Example 8

在实施例3的基础上,本实施例中,所述后挡板与前挡板偏心位置设置有多个螺纹孔,后挡板前挡板通过螺栓相连接,从而实现后挡板的位置固定。On the basis of Embodiment 3, in this embodiment, the eccentric position of the rear baffle and the front baffle is provided with a plurality of threaded holes, and the front baffle of the rear baffle is connected by bolts, so that the position of the rear baffle is fixed .

实施例9Example 9

在实施例3的基础上,本实施例中所述后挡板上安装有掺混管59,利用掺混管59能够实现进入燃烧室的气固两相掺混均匀。On the basis of Embodiment 3, a mixing tube 59 is installed on the rear baffle in this embodiment, and the gas-solid two-phase mixing in the combustion chamber can be realized uniformly by using the mixing tube 59 .

实施例10Example 10

在实施例1的基础上,本实施例中,所述柱塞泵2的输出位置设置有流量调节阀3,利用流量调节阀3能够控制大分子液体碳氢燃料的流量,实现大分子液体碳氢燃料流量的调节,从而实现气固两相掺混固气比。On the basis of Embodiment 1, in this embodiment, the output position of the plunger pump 2 is provided with a flow regulating valve 3, and the flow regulating valve 3 can be used to control the flow rate of the macromolecular liquid hydrocarbon fuel to realize macromolecular liquid carbon fuel. The adjustment of the flow rate of hydrogen fuel realizes the solid-gas ratio of gas-solid two-phase blending.

当然,上述说明并非对本发明的限制,本发明也不仅限于上述举例,本技术领域的普通技术人员在本发明的实质范围内所做出的变化、改型、添加或替换,也属于本发明的保护范围。Of course, the above description is not a limitation of the present invention, and the present invention is not limited to the above examples. Changes, modifications, additions or replacements made by those skilled in the art within the scope of the present invention also belong to the scope of the present invention. protected range.

Claims (10)

1. The mixed fuel supply device of the cracking gas carrying flow solid fuel is characterized in that: the device comprises a plunger pump for pushing macromolecular liquid hydrocarbon fuel, a regeneration cooling channel for cracking the macromolecular liquid hydrocarbon fuel, and a fuel supply device for carrying and mixing solid fuel;
the fuel supply device comprises a fuel storage chamber, a piston for pushing solid fuel is slidably arranged in the fuel storage chamber, and the fuel storage chamber is communicated with a gas collecting bin.
2. The pyrolysis gas entrained flow solid fuel mixed fuel supply device according to claim 1, characterized in that: the fuel reservoir is divided into three parts, namely a reservoir straight section, a reservoir contracted section and a thin straight section.
3. The pyrolysis gas stream-carrying solid fuel mixed fuel supply device according to claim 2, characterized in that: the two ends of the gas collection bin are respectively provided with a front baffle and a rear baffle, an air inlet is arranged at the eccentric position of the front baffle, a flow guide table is arranged at one end of the thin straight section of the storage chamber, which is far away from the contraction section of the storage chamber, and a slit is formed between the flow guide table and the rear baffle.
4. The pyrolysis gas stream-carrying solid fuel mixed fuel supply device according to claim 2, characterized in that: the air inlet holes are three.
5. The pyrolysis gas entrained flow solid fuel mixed fuel supply device according to claim 1, characterized in that: the piston is provided with a piston rod, and the piston rod is arranged at the output end of the motor.
6. The pyrolysis gas stream-carrying solid fuel mixed fuel supply device according to claim 2, characterized in that: the end of the straight section of the storage chamber, which is far away from the contraction end of the storage chamber, is provided with a round table, the end of the straight section of the storage chamber, which is far away from the straight section of the storage chamber, is provided with a baffle, and a piston rod is slidably arranged on the baffle.
7. The pyrolysis gas stream-carrying solid fuel mixed fuel supply apparatus according to claim 6, wherein: and a sliding bearing is arranged between the baffle and the piston rod.
8. The mixed fuel supply apparatus for a pyrolysis gas entrained flow solid fuel according to claim 3, wherein: the rear baffle is connected with the front baffle through bolts.
9. The mixed fuel supply apparatus for a pyrolysis gas entrained flow solid fuel according to claim 3, wherein: the rear baffle is provided with a mixing pipe.
10. The pyrolysis gas stream-carrying solid fuel mixed fuel supply device according to claim 2, characterized in that: and a flow regulating valve is arranged at the output position of the plunger pump.
CN202310094666.7A 2023-02-10 2023-02-10 Mixed fuel supply device for liquid hydrocarbon fuel cracking gas carrying flow solid fuel Pending CN116066257A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202310094666.7A CN116066257A (en) 2023-02-10 2023-02-10 Mixed fuel supply device for liquid hydrocarbon fuel cracking gas carrying flow solid fuel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202310094666.7A CN116066257A (en) 2023-02-10 2023-02-10 Mixed fuel supply device for liquid hydrocarbon fuel cracking gas carrying flow solid fuel

Publications (1)

Publication Number Publication Date
CN116066257A true CN116066257A (en) 2023-05-05

Family

ID=86181708

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202310094666.7A Pending CN116066257A (en) 2023-02-10 2023-02-10 Mixed fuel supply device for liquid hydrocarbon fuel cracking gas carrying flow solid fuel

Country Status (1)

Country Link
CN (1) CN116066257A (en)

Similar Documents

Publication Publication Date Title
US7980056B2 (en) Methods and apparatus for controlling air flow within a pulse detonation engine
CN1892011A (en) Booster rocket engine using gaseous hydrocarbon in catalytically enhanced gas generator cycle
RU2004125487A (en) EJECTIVE AIR-REACTIVE ENGINE
CN110219751B (en) Multiple starting system and starting method for recyclable liquid rocket engine
CN114688561A (en) High-capacity thermal-strength gas generator taking air and alcohol as propellant
CN110469871A (en) A kind of Compound cooling rotation detonation combustor based on Stirling cycle
CN105003357A (en) Pasty propellant fuel gas generator ignition device based on solid rocket engine
CN107701331A (en) A kind of solid-liquid hybrid rocket engine and its method of work
CN116066257A (en) Mixed fuel supply device for liquid hydrocarbon fuel cracking gas carrying flow solid fuel
CN116771548A (en) A chemical-arc combined power thruster for space and its application method
CN103104934A (en) Combustor and method for supplying fuel to combustor
CN219242064U (en) Mixed fuel supply device for liquid hydrocarbon fuel cracking gas carrying solid fuel
Wickman In-situ Mars rocket and jet engines burning carbon dioxide
CN112814807B (en) Phase-change ramjet engine containing paraffin fuel
CN106134391B (en) RBCC engine integration fuel service system based on anhydrous hydrazine
US20220333530A1 (en) Regenerative cooling and adjustable throat for rotating detonation engine
US3942320A (en) Solid boron fuel burner for ramjet
CN210289938U (en) Hydraulic drive type powdered fuel conveying device
CN110778415A (en) Aircraft engine
CN111712624A (en) Pulse driving device
CN116181485A (en) High Mach number ramjet engine with afterburner
CN116025484A (en) Continuous detonation solid rocket engine system based on solid powder
Ostrander et al. Air Turbo-Rocket solid propellant development and testing
CN211650223U (en) Multipurpose air injection system capable of generating speed and temperature controllable air flow
CN114408145A (en) Preheating type water inlet ramjet engine structure and control method

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination