WO2022021803A1 - 改进型双燃料发动机 - Google Patents

改进型双燃料发动机 Download PDF

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Publication number
WO2022021803A1
WO2022021803A1 PCT/CN2021/000020 CN2021000020W WO2022021803A1 WO 2022021803 A1 WO2022021803 A1 WO 2022021803A1 CN 2021000020 W CN2021000020 W CN 2021000020W WO 2022021803 A1 WO2022021803 A1 WO 2022021803A1
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Prior art keywords
combustion chamber
driving system
bumper
hollow
plate
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PCT/CN2021/000020
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English (en)
French (fr)
Inventor
陈小辉
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陈小辉
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Publication of WO2022021803A1 publication Critical patent/WO2022021803A1/zh

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B69/00—Internal-combustion engines convertible into other combustion-engine type, not provided for in F02B11/00; Internal-combustion engines of different types characterised by constructions facilitating use of same main engine-parts in different types
    • F02B69/02—Internal-combustion engines convertible into other combustion-engine type, not provided for in F02B11/00; Internal-combustion engines of different types characterised by constructions facilitating use of same main engine-parts in different types for different fuel types, other than engines indifferent to fuel consumed, e.g. convertible from light to heavy fuel
    • F02B69/04—Internal-combustion engines convertible into other combustion-engine type, not provided for in F02B11/00; Internal-combustion engines of different types characterised by constructions facilitating use of same main engine-parts in different types for different fuel types, other than engines indifferent to fuel consumed, e.g. convertible from light to heavy fuel for gaseous and non-gaseous fuels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/22—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being gaseous at standard temperature and pressure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/24—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being liquid at standard temperature and pressure

Definitions

  • the present invention relates to engine manufacturing technology.
  • An engine is a machine that can convert other forms of energy into mechanical energy, including internal combustion engines (gasoline engines, etc.), external combustion engines (Stirling engines, steam engines, etc.), electric motors, and the like.
  • internal combustion engines usually convert chemical energy into mechanical energy.
  • the engine applies to both the power generating device and the entire machine including the power device (eg gasoline engine, aero engine).
  • the purpose of the present invention is to provide an improved dual-fuel engine to solve the technical problems in the prior art that the structure is too complicated and the energy utilization rate is not high.
  • the improved dual-fuel engine is characterized in that: it comprises a first driving-engine system, a second driving-engine system, a third driving-engine system and a fourth driving-engine system; the first driving-engine system, the second driving-engine system, the The structures of the third driving system and the fourth driving system are exactly the same;
  • the first driving system includes a first driving device, a two-dimensional compressor, a fixed rod, a pressure bearing plate, an air outlet, a combustion chamber, and a fueling device , a gas filling device, a first safety device, a second safety device, an axial flow compressor, an electric ignition device;
  • the first drive device includes a first motor, a first gear, a first power transmission rod and a A first rack on a transmission rod; the first rack is meshed with the first gear;
  • the two-dimensional compressor includes an upper pressure plate, a first cylindrical plate, a second cylindrical plate, and a fixed rod , bearing plate, shell; the bottom of the first dowel rod is fixedly connected with the top
  • FIG. 1 is a schematic structural diagram of a first driving system.
  • FIG. 2 is a schematic structural diagram of a first driving device.
  • FIG. 3 is a schematic structural diagram of a second safety device.
  • FIG. 4 is a schematic structural diagram of the second driving device.
  • FIG. 5 is a schematic structural diagram of the first safety device.
  • the improved dual-fuel engine is characterized in that: it includes a first driving system 1 (as shown in FIG. 1 ), a second driving system 2, a third driving system 3 and a fourth driving system 4;
  • the structures of the first drive system 1, the second drive system 2, the third drive system 3, and the fourth drive system 4 are exactly the same;
  • the first drive system 1 includes a first drive device 5, a two-dimensional compressor Machine 6, fixed rod 38, pressure plate 39, air outlet 9, combustion chamber 40, refueling device 10, refueling device 11, first safety device 12, second safety device 36, axial compressor 34, electric ignition Device 35 ;
  • the first driving device 5 shown in FIG.
  • the two-dimensional compressor 6 (as shown in FIG. 1 ) includes an upper pressing plate 14, a first cylindrical plate 15, and a second cylindrical plate 16.
  • the axial flow compressor 34 is arranged on the left side of the air inlet 18; the air outlet of the axial flow compressor 34 communicates with the air inlet 18; the partial bottom 2301 of the casing 17 is downward
  • the protrusion forms the first groove 19; the bottom part 2302 of the casing 17 protrudes downward to form the second groove 20; the first cylindrical plate 15 can move up and down in the first groove 19; The two cylindrical plates 16 can move up and down in the second groove 20; the second air outlet 21 is opened on the part bottom
  • the fifth driving device 70 includes a safety ingot 28 , the first bumper 29, the second rack 30 and the second drive device 70 arranged on the first bumper 29; the interior of the bumper 28 is hollow; the interior of the first bumper 29 is hollow; The second driving device 70 (as shown in FIG.
  • the safety ingot 28 is arranged in the combustion chamber 40; the first bumper 29 passes through the The third opening 27 is fixedly connected with the insurance ingot 28; the second rack 30 on the first bumper 29 meshes with the second gear 3102 arranged outside the combustion chamber 40; the combustion chamber 40
  • the turbine 32 and the vortex shaft 33 are arranged in the end of the turbine; the interior of the turbine 32 and the vortex shaft 33 is hollow; the turbine 32 and the vortex shaft 33 are fixedly connected; the electric ignition device 35 is fixed at the lower part of the combustion chamber 40 On; the second safety device 36 (as shown in FIG.
  • the second safety device 36 is arranged on the right side of the first dowel rod 1303; the scroll shaft 33 in the first drive system 1 and the axial compressor in the second drive system 2 34 is connected to the rotating shaft; the scroll shaft 33 in the second driving system 2 is connected with the rotating shaft on the axial compressor 34 in the third driving system 3; the third driving system The scroll shaft 33 in 3 is connected with the rotating shaft on the axial compressor 34 in the fourth drive system 4; the scroll shaft 33 in the fourth drive system 4 is connected with the first drive system 1 The shafts on the axial compressor 34 are connected.
  • the concrete operation process of the present invention is:
  • the first motor 1301 in the first driving system 1 is activated to make the upper platen 14 move downward to compress the gas in the two-dimensional compressor 6 .
  • the fueling device 10 in the first drive system 1 starts to add gasoline into the combustion chamber 40 .
  • the electric ignition device 35 in the first drive system 1 makes gasoline and air combust.
  • the second motor 3101 in the first driving system 1 is activated to open the combustion chamber 40 in the first driving system 1 , and the gas in the combustion chamber 40 is ejected from the combustion chamber 40 .
  • the gas ejected from the combustion chamber 40 in the first driving system 1 acts on the turbine 32 in the first driving system 1, and the turbine 32 in the first driving system 1 drives the
  • the scroll shaft 33 rotates, and the scroll shaft 33 in the first driving system 1 drives the rotating shaft on the axial compressor 34 in the second driving system 2 to rotate together with it.
  • the first motor 1301 in the second driving system 2 is activated so that the upper platen 14 moves downward to compress the gas in the two-dimensional compressor 6 .
  • the fueling device 10 in the second driving system 2 starts to add gasoline into the combustion chamber 40 .
  • the electric ignition device 35 in the second drive system 2 causes the combustion of gasoline and air.
  • the second motor 3101 in the second driving system 2 is activated to open the combustion chamber 40 in the second driving system 2 , and the gas in the combustion chamber 40 is ejected from the combustion chamber 40 .
  • the gas ejected from the combustion chamber 40 in the second driving system 2 acts on the turbine 32 in the second driving system 2, and the turbine 32 in the second driving system 2 drives the turbine 32 in the second driving system 2.
  • the scroll shaft 33 rotates, and the scroll shaft 33 in the second driving system 2 drives the rotating shaft on the axial compressor 34 in the third driving system 3 to rotate together with it.
  • the first motor 1301 in the third driving system 3 is activated so that the upper platen 14 moves downward to compress the gas in the two-dimensional compressor 6 .
  • the fueling device 10 in the third driving system 3 starts to add gasoline into the combustion chamber 40 .
  • the electric ignition device 35 in the third drive system 3 causes the combustion of gasoline and air.
  • the second motor 3101 in the third driving system 3 is activated to open the combustion chamber 40 in the third driving system 3 , and the gas in the combustion chamber 40 is ejected from the combustion chamber 40 .
  • the gas ejected from the combustion chamber 40 in the third driving system 3 acts on the turbine 32 in the third driving system 3, and the turbine 32 in the third driving system 3 drives the turbine 32 in the third driving system 3.
  • the scroll shaft 33 rotates, and the scroll shaft 33 in the third driving system 3 drives the rotating shaft on the axial compressor 34 in the third driving system 4 to rotate together with it.
  • the first motor 1301 in the fourth driving system 4 is activated to make the upper platen 14 move downward to compress the gas in the two-dimensional compressor 6 .
  • the fueling device 10 in the fourth drive system 4 starts to add gasoline into the combustion chamber 40 .
  • the electric ignition device 35 in the fourth drive system 4 causes the combustion of gasoline and air.
  • the second motor 3101 in the fourth driving system 4 is activated to open the combustion chamber 40 in the fourth driving system 4 , and the gas in the combustion chamber 40 is ejected from the combustion chamber 40 .
  • the gas ejected from the combustion chamber 40 in the fourth driving system 4 acts on the turbine 32 in the fourth driving system 4, and the turbine 32 in the fourth driving system 4 drives the turbine 32 in the fourth driving system 4.
  • the scroll shaft 33 rotates, and the scroll shaft 33 in the fourth driving system 4 drives the rotating shaft on the axial compressor 34 in the first driving system 1 to rotate together with it.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

一种双燃料发动机，包括四个结构相同的驱发系统，驱发系统包括第一驱动装置（5）、双维压气机（6）、固定杆（38）、承压板（39）、出气管（9）、燃烧室（40）、加油装置（10）、加气装置（11）、第一保险装置（12）、第二保险装置（16）、轴流式压气机（34）和电点火装置（35），燃烧室内设置涡轮（32）和涡轴（33），涡轴与轴流式压气机的转轴相连。

Description

改进型双燃料发动机 技术领域
本发明涉及发动机制造技术。
背景技术
发动机是一种能够把其它形式的能转化为机械能的机器，包括如内燃机(汽油发动机等)、外燃机(斯特林发动机、蒸汽机等)、电动机等。如内燃机通常是把化学能转化为机械能。发动机既适用于动力发生装置，也可指包括动力装置的整个机器(如：汽油发动机、航空发动机)。
发明内容
本发明的目的是提供改进型双燃料发动机，解决现有技术中结构过于复杂、能量利用率不高的技术问题。
为解决上述问题，本发明所采取的技术方案是：
改进型双燃料发动机，其特征在于：包括第一驱发系统、第二驱发系统、第三驱发系统和第四驱发系统；所述的第一驱发系统、第二驱发系统、第三驱发系统、第四驱发系统的结构完全相同；所述的第一驱发系统包括第一驱动装置、双维压气机、固定杆、承压板、出气管、燃烧室、加油装置、加气装置、第一保险装置、第二保险装置、轴流式压气机、电点火装置；所述的第一驱动装置包括第一电机、第一齿轮、第一传力杆和设置在第一传力杆上的第一齿条；所述的第一齿条与第一齿轮相啮合；所述的双维压气机包括上压板、第一圆筒板、第二圆筒板、固定杆、承压板、外壳；所述的第一传力杆的底部与上压板的部分顶部固定连接；所述的上压板的内部中空；所述的第一圆筒板的顶部与上压板的部分底部固定连接；所述的第二圆筒板的顶部与上压板的部分底部固定连接；所述的外壳的上部开有进气口；所述的轴流式压气机设置在进气口的左侧；所述的轴流式压气机的出气口与进气口相通；所述的外壳的部分底部向下凸起形成第一凹槽；外壳的部分底部向下凸起形成第二凹槽；所述的第一圆筒板可以在第一凹槽内上下活动；所述的第二圆筒板可以在第二凹槽内上下活动；所述的外壳的部分底部开有第二出气口；所述的出气管的顶部与外壳的部分底部固定连接；所述的固定杆的顶部与上压板的部分底部固定连接；所述的固定杆的底部与承压板的部分顶部固定连接；所述的固定杆的内部中空；所述的承压板的内部中空；所述的第一圆筒板的内部中空；所述的第二圆筒板的内部中空；所述的外壳的内部中空；所述的承压板可在出气管内上下活动；所述的承压板的外侧可与出气管的内壁相贴合；所述的燃烧室的顶部与出气管的底部固定连接；所述的燃烧室的上部开有加气口；所述的加气口的右侧设置加气装置；所述的加气装置上设置喷气管；所述的喷气管与加气口相通；所述的燃烧室的中部开有加油口；所 述的加油口的左侧设置加油装置；所述的加油装置上设置喷油嘴；所述的喷油嘴与加油口相通；所述的燃烧室的下部开有第三开口；所述的第一保险装置包括保险锭、第一保险杠、设置在第一保险杠上的第二齿条、第二驱动装置；所述的保险锭的内部中空；所述的第一保险杠的内部中空；所述的第二驱动装置包括第二电机、第二齿轮；所述的保险锭设置在燃烧室内；所述的第一保险杠穿过所述的第三开口后与保险锭固定连接；所述的第一保险杠上的第二齿条与设置在燃烧室外的第二齿轮相啮合；所述的燃烧室的末端内设置涡轮和涡轴；所述的涡轮和涡轴的内部中空；所述的涡轮和涡轴固定连接；所述的电点火装置固定在燃烧室的下部上；所述的第二保险装置包括第三电机、第三齿轮、第三保险杠和设置在第三保险杠上的第三齿条；所述的第二保险装置设置在所述的第一传力杆的右侧；所述的第一驱发系统中的涡轴与第二驱发系统中的轴流式压气机上的转轴相连接；所述的第二驱发系统中的涡轴与第三驱发系统中的轴流式压气机上的转轴相连接；所述的第三驱发系统中的涡轴与第四驱发系统中的轴流式压气机上的转轴相连接；所述的第四驱发系统中的涡轴与第一驱发系统中的轴流式压气机上的转轴相连接。
附图说明
图1是第一驱发系统的结构示意图。
图2是第一驱动装置的结构示意图。
图3是第二保险装置的结构示意图。
图4是第二驱动装置的结构示意图。
图5是第一保险装置的结构示意图。
具体实施方式
下面结合附图对本发明的具体实施方式作进一步的说明。
改进型双燃料发动机，其特征在于：包括第一驱发系统1(如图1所示)、第二驱发系统2、第三驱发系统3和第四驱发系统4；所述的第一驱发系统1、第二驱发系统2、第三驱发系统3、第四驱发系统4的结构完全相同；所述的第一驱发系统1包括第一驱动装置5、双维压气机6、固定杆38、承压板39、出气管9、燃烧室40、加油装置10、加气装置11、第一保险装置12、第二保险装置36、轴流式压气机34、电点火装置35；所述的第一驱动装置5(如图2所示)包括第一电机1301、第一齿轮1302、第一传力杆1303和设置在第一传力杆1303上的第一齿条1304；所述的第一齿条1304与第一齿轮1302相啮合；所述的双维压气机6(如图1所示)包括上压板14、第一圆筒板15、第二圆筒板16、固定杆38、承压板39、外壳17；所述的第一传力杆1303的底部与上压板14的部分顶部固定连接；所述的上压板14的内部中空；所述的第一圆筒板15的顶部与上压板14的部分底部固定连接；所述的第二圆 筒板16的顶部与上压板14的部分底部固定连接；所述的外壳17的上部开有进气口18；所述的轴流式压气机34设置在进气口18的左侧；所述的轴流式压气机34的出气口与进气口18相通；所述的外壳17的部分底部2301向下凸起形成第一凹槽19；外壳17的部分底部2302向下凸起形成第二凹槽20；所述的第一圆筒板15可以在第一凹槽19内上下活动；所述的第二圆筒板16可以在第二凹槽20内上下活动；所述的外壳17的部分底部2303开有第二出气口21；所述的出气管9的顶部与外壳17的部分底部2304固定连接；所述的固定杆38的顶部与上压板14的部分底部固定连接；所述的固定杆38的底部与承压板39的部分顶部固定连接；所述的固定杆38的内部中空；所述的承压板39的内部中空；所述的第一圆筒板15的内部中空；所述的第二圆筒板16的内部中空；所述的外壳17的内部中空；所述的承压板39可在出气管9内上下活动；所述的承压板39的外侧可与出气管9的内壁相贴合；所述的燃烧室40的顶部与出气管9的底部固定连接；所述的燃烧室40的上部开有加气口22；所述的加气口22的右侧设置加气装置11；所述的加气装置11上设置喷气管24；所述的喷气管24与加气口22相通；所述的燃烧室40的中部开有加油口25；所述的加油口25的左侧设置加油装置10；所述的加油装置10上设置喷油嘴26；所述的喷油嘴26与加油口25相通；所述的燃烧室40的下部开有第三开口27；所述的第一保险装置12(如图5所示)包括保险锭28、第一保险杠29、设置在第一保险杠29上的第二齿条30、第二驱动装置70；所述的保险锭28的内部中空；所述的第一保险杠29的内部中空；所述的第二驱动装置70(如图4所示)包括第二电机3101、第二齿轮3102；所述的保险锭28设置在燃烧室40内；所述的第一保险杠29穿过所述的第三开口27后与保险锭28固定连接；所述的第一保险杠29上的第二齿条30与设置在燃烧室40外的第二齿轮3102相啮合；所述的燃烧室40的末端内设置涡轮32和涡轴33；所述的涡轮32和涡轴33的内部中空；所述的涡轮32和涡轴33固定连接；所述的电点火装置35固定在燃烧室40的下部上；所述的第二保险装置36(如图3所示)包括第三电机3701、第三齿轮3702、第三保险杠3703和设置在第三保险杠3703上的第三齿条3704；所述的第二保险装置36设置在所述的第一传力杆1303的右侧；所述的第一驱发系统1中的涡轴33与第二驱发系统2中的轴流式压气机34上的转轴相连接；所述的第二驱发系统2中的涡轴33与第三驱发系统3中的轴流式压气机34上的转轴相连接；所述的第三驱发系统3中的涡轴33与第四驱发系统4中的轴流式压气机34上的转轴相连接；所述的第四驱发系统4中的涡轴33与第一驱发系统1中的轴流式压气机34上的转轴相连接。
本发明的具体操作过程为：
1.第一驱发系统1中的第一电机1301启动使得上压板14向下运动以压缩双维压气机6内的气体。
1.第一驱发系统1中的加油装置10启动往燃烧室40内加入汽油。
2.第一驱发系统1中的电点火装置35使得汽油和空气发生燃烧。
3.第一驱发系统1中的第二电机3101启动以打开第一驱发系统1中的燃烧室40，燃烧室40内的气体从燃烧室40喷出。
4.从第一驱发系统1中的燃烧室40喷出的气体作用于第一驱发系统1中的涡轮32，第一驱发系统1中的涡轮32带动第一驱发系统1中的涡轴33旋转，第一驱发系统1中的涡轴33带动第二驱发系统2中的轴流式压气机34上的转轴与之一起旋转。
6.第二驱发系统2中的第一电机1301启动使得上压板14向下运动以压缩双维压气机6内的气体。
7.第二驱发系统2中的加油装置10启动往燃烧室40内加入汽油。
8.第二驱发系统2中的电点火装置35使得汽油和空气发生燃烧。
9.第二驱发系统2中的第二电机3101启动以打开第二驱发系统2中的燃烧室40，燃烧室40内的气体从燃烧室40喷出。
10.从第二驱发系统2中的燃烧室40喷出的气体作用于第二驱发系统2中的涡轮32，第二驱发系统2中的涡轮32带动第二驱发系统2中的涡轴33旋转，第二驱发系统2中的涡轴33带动第三驱发系统3中的轴流式压气机34上的转轴与之一起旋转。
11.第三驱发系统3中的第一电机1301启动使得上压板14向下运动以压缩双维压气机6内的气体。
12.第三驱发系统3中的加油装置10启动往燃烧室40内加入汽油。
13.第三驱发系统3中的电点火装置35使得汽油和空气发生燃烧。
14.第三驱发系统3中的第二电机3101启动以打开第三驱发系统3中的燃烧室40，燃烧室40内的气体从燃烧室40喷出。
15.从第三驱发系统3中的燃烧室40喷出的气体作用于第三驱发系统3中的涡轮32，第三驱发系统3中的涡轮32带动第三驱发系统3中的涡轴33旋转，第三驱发系统3中的涡轴33带动第三驱发系统4中的轴流式压气机34上的转轴与之一起旋转。
16.第四驱发系统4中的第一电机1301启动使得上压板14向下运动以压缩双维压气机6内的气体。
17.第四驱发系统4中的加油装置10启动往燃烧室40内加入汽油。
18.第四驱发系统4中的电点火装置35使得汽油和空气发生燃烧。
19.第四驱发系统4中的第二电机3101启动以打开第四驱发系统4中的燃烧室40，燃烧室40内的气体从燃烧室40喷出。
20.从第四驱发系统4中的燃烧室40喷出的气体作用于第四驱发系统4中的涡轮32，第四驱发系统4中的涡轮32带动第四驱发系统4中的涡轴33旋转，第四驱发系统4中的涡轴33带动第一驱发系统1中的轴流式压气机34上的转轴与之一起旋转。
当把汽油换成可燃气体时，操作过程如上述一样。
以上说明书中未作特别说明的部分均为现有技术，或者通过现有技术即能实现。凡依本发明申请专利范围的内容所作的等效变化与修饰都应作为本发明的技术范畴。

Claims (1)

  1. 改进型双燃料发动机，其特征在于：包括第一驱发系统(1)、第二驱发系统(2)、第三驱发系统(3)和第四驱发系统(4)；所述的第一驱发系统(1)、第二驱发系统(2)、第三驱发系统(3)、第四驱发系统(4)的结构完全相同；所述的第一驱发系统(1)包括第一驱动装置(5)、双维压气机(6)、固定杆(38)、承压板(39)、出气管(9)、燃烧室(40)、加油装置(10)、加气装置(11)、第一保险装置(12)、第二保险装置(36)、轴流式压气机(34)、电点火装置(35)；所述的第一驱动装置(5)包括第一电机(1301)、第一齿轮(1302)、第一传力杆(1303)和设置在第一传力杆(1303)上的第一齿条(1304)；所述的第一齿条(1304)与第一齿轮(1302)相啮合；所述的双维压气机(6)包括上压板(14)、第一圆筒板(15)、第二圆筒板(16)、固定杆(38)、承压板(39)、外壳(17)；所述的第一传力杆(1303)的底部与上压板(14)的部分顶部固定连接；所述的上压板(14)的内部中空；所述的第一圆筒板(15)的顶部与上压板(14)的部分底部固定连接；所述的第二圆筒板(16)的顶部与上压板(14)的部分底部固定连接；所述的外壳(17)的上部开有进气口(18)；所述的轴流式压气机(34)设置在进气口(18)的左侧；所述的轴流式压气机(34)的出气口与进气口(18)相通；所述的外壳(17)的部分底部(2301)向下凸起形成第一凹槽(19)；外壳(17)的部分底部(2302)向下凸起形成第二凹槽(20)；所述的第一圆筒板(15)可以在第一凹槽(19)内上下活动；所述的第二圆筒板(16)可以在第二凹槽(20)内上下活动；所述的外壳(17)的部分底部(2303)开有第二出气口(21)；所述的出气管(9)的顶部与外壳(17)的部分底部(2304)固定连接；所述的固定杆(38)的顶部与上压板(14)的部分底部固定连接；所述的固定杆(38)的底部与承压板(39)的部分顶部固定连接；所述的固定杆(38)的内部中空；所述的承压板(39)的内部中空；所述的第一圆筒板(15)的内部中空；所述的第二圆筒板(16)的内部中空；所述的外壳(17)的内部中空；所述的承压板(39)可在出气管(9)内上下活动；所述的承压板(39)的外侧可与出气管(9)的内壁相贴合；所述的燃烧室(40)的顶部与出气管(9)的底部固定连接；所述的燃烧室(40)的上部开有加气口(22)；所述的加气口(22)的右侧设置加气装置(11)；所述的加气装置(11)上设置喷气管(24)；所述的喷气管(24)与加气口(22)相通；所述的燃烧室(40)的中部开有加油口(25)；所述的加油口(25)的左侧设置加油装置(10)；所述的加油装置(10)上设置喷油嘴(26)；所述的喷油嘴(26)与加油口(25)相通；所述的燃烧室(40)的下部开有第三开口(27)；所述的第一保险装置(12)包括保险锭(28)、第一保险杠(29)、设置在第一保险杠(29)上的第二齿条(30)、第二驱动装置(70)；所述的保险锭(28)的内部中空；所述的第一保险杠(29)的内部中空；所述的第二驱动装置(70)包括第二电机(3101)、第二齿轮(3102)；所述的保险锭(28)设置在燃烧室(40)内；所述的第一保险杠(29)穿过所 述的第三开口(27)后与保险锭(28)固定连接；所述的第一保险杠(29)上的第二齿条(30)与设置在燃烧室(40)外的第二齿轮(3102)相啮合；所述的燃烧室(40)的末端内设置涡轮(32)和涡轴(33)；所述的涡轮(32)和涡轴(33)的内部中空；所述的涡轮(32)和涡轴(33)固定连接；所述的电点火装置(35)固定在燃烧室(40)的下部上；所述的第二保险装置(36)包括第三电机(3701)、第三齿轮(3702)、第三保险杠(3703)和设置在第三保险杠(3703)上的第三齿条(3704)；所述的第二保险装置(36)设置在所述的第一传力杆(1303)的右侧；所述的第一驱发系统(1)中的涡轴(33)与第二驱发系统(2)中的轴流式压气机(34)上的转轴相连接；所述的第二驱发系统(2)中的涡轴(33)与第三驱发系统(3)中的轴流式压气机(34)上的转轴相连接；所述的第三驱发系统(3)中的涡轴(33)与第四驱发系统(4)中的轴流式压气机(34)上的转轴相连接；所述的第四驱发系统(4)中的涡轴(33)与第一驱发系统(1)中的轴流式压气机(34)上的转轴相连接。
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EP1801386A1 (en) * 2005-12-20 2007-06-27 Ford Global Technologies, LLC An arrangement at an internal combustion engine
US20160084149A1 (en) * 2013-06-14 2016-03-24 Jaguar Land Rover Limited Supercharger Assembly
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CN107288750A (zh) * 2016-03-30 2017-10-24 陈小辉 涡轮增压双燃料发动机

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