WO2011160602A1 - 一种气流收集装置、风力发动机及机动车 - Google Patents

一种气流收集装置、风力发动机及机动车 Download PDF

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Publication number
WO2011160602A1
WO2011160602A1 PCT/CN2011/076343 CN2011076343W WO2011160602A1 WO 2011160602 A1 WO2011160602 A1 WO 2011160602A1 CN 2011076343 W CN2011076343 W CN 2011076343W WO 2011160602 A1 WO2011160602 A1 WO 2011160602A1
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Prior art keywords
airflow
impeller
impeller chamber
passage
stage
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PCT/CN2011/076343
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English (en)
French (fr)
Inventor
丛洋
Original Assignee
Cong Yang
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Publication of WO2011160602A1 publication Critical patent/WO2011160602A1/zh

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D1/00Wind motors with rotation axis substantially parallel to the air flow entering the rotor 
    • F03D1/04Wind motors with rotation axis substantially parallel to the air flow entering the rotor  having stationary wind-guiding means, e.g. with shrouds or channels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D9/00Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
    • F03D9/30Wind motors specially adapted for installation in particular locations
    • F03D9/32Wind motors specially adapted for installation in particular locations on moving objects, e.g. vehicles
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/728Onshore wind turbines

Definitions

  • the invention relates to an air flow collecting device and an engine, which are particularly suitable for various motor vehicles.
  • An engine that uses fuel as an energy source consumes a large amount of fuel, and emits a large amount of exhaust gas, hot gas, and pollutes the environment.
  • human beings are more eager to eliminate emissions, hot air emissions, and pollution-free launches without fuel consumption.
  • the applicant of the present invention has proposed the patent number 200580044218.6, and the invention name is "the wind engine is the wind power.
  • the invention discloses a blast engine and a motor vehicle, comprising at least one impeller chamber, an impeller installed in the impeller chamber, and a jet system for injecting compressed gas into the impeller chamber.
  • the main feature of the invention is that the impeller chamber is arranged A jet system and an air inlet for receiving an external airflow are provided.
  • the inventive ventilating engine is installed on a power-driven mechanical machine (especially a motor vehicle).
  • compressed gas is used as a main power, no fuel consumption, no exhaust gas, hot gas discharge, and no pollution.
  • the air inlet for receiving the external wind resistance airflow By setting the air inlet for receiving the external wind resistance airflow, the wind resistance airflow encountered by the power machinery during the running process can be directly utilized, and the resistance is the power.
  • the above invention firstly proposes a ventilating engine that directly utilizes the wind resistance airflow as the auxiliary power and simultaneously uses the compressed gas as the main power, and the motor vehicle using the same, it is not necessary to convert the wind resistance airflow into electric energy, and thus there is no complicated Electromechanical energy conversion systems and circuit control systems greatly simplify the structure of power machinery, especially motor vehicles, and provide a new way to save energy and find environmentally friendly fuel substitutes.
  • the inventor in order to make better use of the wind resistance airflow and the compressed gas, to make the best cooperation between the main power and the auxiliary power, and to improve the use efficiency of the main power, the inventor has proposed an application number of 200780030483.8, and the invention name is Invention patent application for combined air-fuel engines and motor vehicles.
  • the main feature of the invention is that a separate structure of a compressed gas (compressed gas) engine and a windage (wind) engine are respectively provided, which can be characterized according to the high and relatively concentrated flow rate of the compressed gas, and the flow velocity of the wind-resistant airflow is low and relatively dispersed, respectively.
  • Optimized design of the impeller in a targeted manner for example, the impeller blade surface design of the wind resistance engine is small, and the impeller blade surface of the wind resistance engine is designed to be large) to improve the energy conversion efficiency.
  • the motor vehicle adopting the combined air-fuel engine adopts compressed gas as the main power, and directly adopts the wind-resistance airflow encountered by the power machinery during driving as an auxiliary power, and can also make the compressed gas and the wind-resistant airflow better cooperate. .
  • the main technical problem to be solved by the present invention is to further optimize the airflow collecting device to make the collected airflow more concentrated, so that the wind turbine can more effectively utilize the collected airflow to generate stronger power.
  • An airflow collecting device includes an airflow collecting passage having a large outer port and a small inner port, and a fluid guiding body is disposed in the airflow collecting passage.
  • a wind power engine comprising an airflow collecting device, at least one impeller chamber, at least one impeller installed in the impeller chamber through a power output shaft, the airflow collecting device comprising an airflow collecting passage having a large outer port and a small inner opening, a gas guide is disposed in the airflow collecting passage, and a vane is fixed on an outer circumferential surface of the impeller, and an air flow passage formed between the fluid guide and the airflow collecting passage communicates with the vane, so that the airflow passage The internally collected gas stream acts directly on the blade.
  • the fluid guiding body is substantially fixed on a central axis of the airflow collecting passage near the inner port, and the conducting fluid is substantially a projection extending from the inner port in the direction of the outer port.
  • the guiding fluid is substantially a cone extending from the inner port in the direction of the outer port, and the airflow collecting passage forms an annular airflow passage with the fluid guiding body, and the annular airflow passage and the outer circumferential surface of the impeller The vanes corresponding to the annular arrangement are communicated such that the annular airflow collected in the air passage directly acts on the annularly disposed vanes on the outer peripheral surface of the impeller to drive the impeller to rotate.
  • a side of the impeller is fixed with a shroud for guiding the airflow onto the surrounding blades.
  • the at least one impeller chamber is at least two stages of impeller chambers, and the impellers of the impellers are installed in the impeller chambers of each stage, and the blades are fixed on the outer peripheral surface of the impellers in the radial direction of the impellers.
  • the airflow flowing out of the impeller chamber acts on the blades in the inner impeller chamber through the airflow passage.
  • a wind energy collecting device comprising the foregoing wind power engine, a gas compression device and a gas storage tank, the power transmission gas compression device output by the wind power engine, and the compressed gas generated by the gas compression device is input into a gas storage tank for storage.
  • each stage of the compressed gas engine comprising at least one impeller chamber, at least one impeller installed in the impeller chamber through a rotating shaft, and at least one intake air is provided in each stage of the impeller chamber The port and the at least one exhaust port, wherein the exhaust port on the impeller chamber of the first stage communicates with the air inlet on the impeller chamber of the rear stage, and each stage of the impeller outputs power through a drive shaft of the rotating shaft motor vehicle.
  • the size and shape of the fluid guide can be flexibly changed as needed, so that the collected airflow is more concentrated and more directional.
  • airflow when applied to an engine, airflow (windage) can be directed to the blades at the end of the impeller, resulting in greater torque output.
  • the airflow windage resistance
  • the airflow is directly guided to the blades at the end of the impeller, which avoids the disorder of the airflow caused by the airflow encountering when the airflow flows through the central portion of the impeller blade, thereby improving the utilization rate of the wind energy of the engine.
  • FIG. 1 is a schematic structural view of a wind turbine according to the present invention.
  • FIG. 2 is a schematic structural view of a wind energy collecting device.
  • Fig. 3 is a schematic structural view of a motor vehicle.
  • FIG. 4 is a schematic structural view of the first stage compressed gas engine of FIG.
  • Fig. 5 is an enlarged schematic partial view showing the structure of an impeller chamber of the first stage compressed gas engine of Fig. 3.
  • a wind power engine as shown in FIG. 1, includes an air flow collecting device, an impeller chamber 4, an impeller 6 installed in the impeller chamber 4 through the power output shaft 7, and a blade is fixedly fixed on the outer peripheral surface of the impeller 6 in the radial direction. 5.
  • a shroud 9 for guiding the airflow to the outer peripheral blades 5 is fixed to the side of the impeller 6.
  • the airflow collecting device includes an airflow collecting passage 1 having a large outer port and a small inner port, and a fluid guiding body 2.
  • a fluid guide 2 is disposed in the airflow collecting passage 1, and the fluid guide 2 is fixed on a central axis of the airflow collecting passage 1 near the inner port, and the fluid guide 2 is substantially a cone extending from the inner port in the direction of the outer port, and the airflow collecting passage
  • An annular air flow passage 3 is formed between the first airflow passage 3 and the annular air flow passage 3, and the annular air flow passage 3 communicates with the annularly disposed vane 5 on the outer circumferential surface of the impeller 6, so that the annular air flow collected in the air flow passage 3 directly acts on the outer circumferential surface of the impeller 6.
  • the blades 5 are arranged to drive the impeller 6 to rotate.
  • the power generated by the wind turbine is outputted outward by the power output shaft 7 via the clutch 8.
  • the engine of the present invention can be installed as a wind resistance engine on a blast engine motor vehicle (application number 200780030483.8), receiving the moving wind resistance of the motor vehicle during driving, changing the resistance to power, and installing the wind resource.
  • a wind resistance engine on a blast engine motor vehicle (application number 200780030483.8)
  • receiving the moving wind resistance of the motor vehicle during driving changing the resistance to power
  • installing the wind resource In the rich natural environment, the wind is received by nature, and the power output is generated.
  • the power output can be used to convert the air compressor into compressed air for storage, or directly to drive the generator output power.
  • a wind energy collecting device as shown in FIG. 2, comprises a wind power engine, a gas compression device 10 and a gas storage tank 11.
  • the structure of the wind power engine is the same as that of the first embodiment, and the power output from the wind turbine output shaft 7 is driven by the clutch 8 to compress the air compression device. 10.
  • the compressed air generated by the air compressing device 10 is input to the gas storage tank 11 for storage.
  • a motor vehicle as shown in FIGS. 3 to 5, includes a windshield engine 100, a compressed gas engine 200, and a drive shaft 300 of a motor vehicle. among them:
  • the damper engine 100 includes an airflow collecting device and a two-stage damper engine.
  • the airflow collecting device includes an airflow collecting passage 101 having a large outer port, a small inner port, and a fluid guiding body 102.
  • a fluid guide 102 is disposed in the airflow collecting passage 101, and the fluid guide 102 is fixed on a central axis of the airflow collecting passage 101 near the inner port.
  • the fluid guide 102 is substantially a cone extending from the inner port in the direction of the outer port, and the airflow collecting passage is provided.
  • An annular air flow passage 103 is formed between the 101 and the cone 102.
  • the two-stage windage engine includes an impeller chamber (104, 106), and the two-stage impeller (113, 110) common power output shaft 109 is installed in the impeller chamber (104, 106) in the radial direction of the two-stage impeller (113, 110).
  • Two stages of blades (105, 111) are equally divided on the outer peripheral surface, and the airflow flowing out from the front stage impeller chamber 104 acts on the blades 111 in the latter stage impeller chamber 106 through the next stage air flow passage 112.
  • a shroud (114, 108) for guiding the airflow to the outer peripheral blades (105, 111) is fixed to the side of the impeller (113, 110).
  • the first-stage annular airflow passage 103 communicates with the annularly disposed blades 105 on the outer circumferential surface of the impeller 113, so that the annular airflow collected in the airflow passage 103 directly acts on the annularly disposed blades 105 on the outer circumferential surface of the impeller 113, thereby driving the first The stage impeller 113 rotates.
  • the second-stage annular airflow passage 112 communicates with the annularly disposed blades 111 on the outer circumferential surface of the impeller 110, so that the annular airflow collected from the first-stage impeller chamber 104 collected in the second-stage annular airflow passage 112 acts on the impeller again.
  • the second stage impeller 110 is driven to rotate.
  • the power generated by the two-pole impeller is output by the power output shaft 109.
  • the compressed gas engine 200 includes a left side compressed gas engine, a right side compressed gas engine, and a transmission shaft 19, and the left and right compressed gas engines have a bilaterally symmetrical structure.
  • the left compressed gas engine includes a first stage compressed gas engine 210 and a second stage compressed gas engine 220, and the first stage compressed gas engine 210 and the second stage compressed gas engine 220 are coaxially mounted.
  • the power generated by the compressed gas engines on the left and right sides drives the drive shaft 300 of the motor vehicle via the rotating shaft 203.
  • the first stage compressed gas engine 210 has the same structure as the second stage compressed gas engine 220.
  • the first stage compressed gas engine 210 includes an impeller chamber 215, an impeller 220 mounted in the impeller chamber 215 through the rotating shaft 203, and the impeller 219 has a plurality of equally spaced vanes 216 thereon.
  • the impeller chamber 215 is provided with a plurality of air inlets 211 and exhaust ports 212.
  • the air inlets 211 are provided with nozzles 217, the exhaust ports 212 on the first stage impeller chamber 215 and the second stage impeller chambers 225.
  • the air inlets 221 are in communication.
  • a jet introduction groove 213 provided in the rotating peripheral surface and communicating with the intake port 211 is opened on the inner surface of the impeller chamber 215, and when approaching the intake port 211
  • the air introduction slot 213 is deep and wide, and the air introduction slot 213 when the air inlet 211 is away from the air inlet 211 is shallow and narrow (FIG. 5), and the length of the air introduction slot 213 is greater than the distance L between two adjacent leaf teeth 216 (reference numeral 218).
  • the compressed gas which is led out from the air introducing groove 213 can simultaneously act on two or more of the blade teeth 216, and the second can be applied to the desired leaf tooth portion according to a preset derivation path to generate a stronger one.
  • the thrust Further, in order to increase the jet force, two nozzles 217 are provided in the same jet introduction groove 213 in this embodiment.
  • An exhaust groove 214 parallel to the axis of the rotating shaft is opened on the inner surface of the impeller chamber 215, and the exhaust groove 214 communicates with the exhaust port 212.
  • the width of the venting groove 214 is substantially the same as the width of the impeller 220.
  • the first stage compressed gas engine 210 has a small impeller diameter
  • the second stage compressed gas engine 220 has a large impeller diameter.
  • the diameter of the first-stage exhaust port 212 is 2-10 times that of the first-stage air inlet 211
  • the diameter of the second-stage exhaust port 222 is 2-10 times that of the second-stage air inlet 221. , can be flexibly set as needed.
  • the gas just injected is prevented from being directly discharged from the exhaust groove 214, and the distance between the end of the jet introduction groove 213 and the nearest exhaust groove 214 should be greater than the distance L between two adjacent blade teeth.
  • a compressed gas is injected into the first-stage compressed gas engine 210 through the nozzle 217 through a jet system (not shown) of the motor vehicle, and is depressurized and stabilized by the first-stage compressed gas engine 210 to enter the second-stage compression.
  • Gas engine 220 The first stage compressed gas engine 210 takes both the decompression and the stabilizing effect, and fully utilizes the energy generated during the release of the compressed gas.
  • the first stage compressed gas engine 210 simultaneously provides partial power.
  • the second stage compressed gas engine 220 provides primary power. When the motor vehicle reaches a certain speed, the wind resistance airflow enters the wind resistance engine 100 through the airflow collecting device to generate auxiliary power.

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  • Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
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Description

一种气流收集装置、风力发动机及机动车 技术领域
本发明涉及一种气流收集装置及发动机,特别适合于各种机动车。
背景技术
用燃料作为能源的发动机需要消耗大量的燃料,且又排放大量的废气、热气,污染环境。为了节省燃料能源,保护地球环境,人类更渴望一种无需燃料消耗,杜绝废气、热气排放、无污染的发动。
为了能更直接地利用风能,特别是为了能够将动力机械在行驶过程中所遇到的风阻气流直接加以利用,本发明的申请人提出了专利号为200580044218.6、发明名称为“风气发动机即采用风力气压取代燃料能源的发动机”的中国专利。该发明公开了一种风气发动机及机动车,包括至少一个叶轮室、装设在叶轮室内的叶轮和用于将压缩气体喷入叶轮室的喷气系统,该发明的主要特点在于在叶轮室上设置了设置喷气系统和用于接收外部风阻气流的进风口。使用时,该发明的风气发动机安装在能够行驶的动力机械上(特别是机动车),通过设置喷气系统,采用压缩气体作为主动力,无燃料消耗,无废气、热气排放、无污染。通过设置接收外部风阻气流的进风口,可以将动力机械在行驶过程中所遇到的风阻气流直接加以利用,变阻力为动力。
虽然,上述发明首创性地提出了直接利用风阻气流作为辅助动力以及同时采用压缩气体作为主动力的风气发动机及采用该风气发动机的机动车,不但不需要将风阻气流转换成电能,因而没有复杂的机电能量转换系统和电路控制系统,大大简化了动力机械、特别是机动车的结构,而且为节约能源和寻找环保型的燃油代用品提供了一个新的途径。但是,为了能够更好地利用风阻气流和压缩气体,使主动力和辅助动力之间产生最佳的配合,提高主动力的使用效率,发明人又提出了一种申请号为200780030483.8、发明名称为组合式风气发动机及机动车的发明专利申请。该发明的主要特点是分别设置独立结构的压缩气体(压缩气体)发动机和风阻(风力)发动机,可根据压缩气体的流速高、相对集中,而风阻气流的流速低、相对分散的特点,分别有针对性地对叶轮进行优化设计(如:风阻发动机的叶轮叶面设计得要小,风阻发动机的叶轮叶面设计得要大),以提高能量转换效率。采用该组合式风气发动机的机动车既采用压缩气体作为主动力,又直接采用动力机械在行驶过程中所遇到的风阻气流作为辅助动力,还可以使压缩气体和风阻气流能够更好地配合使用。
但是,上述新型的以压缩空气作为主动力、以接收利用风阻气流作为辅助动力的新能源汽车,仍还有大量的技术工作要做。
技术问题
本发明要解决的主要技术问题是,进一步优化气流收集的装置,使收集的气流更集中,使风力发动机更有效地利用收集的气流产生更强的动力。
技术解决方案
解决上述技术问题的技术方案:
一种气流收集装置,包括外口大、内口小的气流收集通道,在所述气流收集通道内设置有导流体。
一种风力发动机,包括气流收集装置、至少一个叶轮室、通过动力输出轴装设于所述叶轮室内的至少一个叶轮,所述气流收集装置包括外口大、内口小的气流收集通道,在所述气流收集通道内设置有导流体,在所述叶轮径向的外周面上固定有叶片,所述导流体与所述气流收集通道之间形成的气流通道与所述叶片相通,使得气流通道内收集的气流直接作用于所述叶片上。
进一步地,所述导流体基本固定在靠近内口处的气流收集通道的中轴线上,所述导流体基本呈从内口沿外口方向延伸的凸出部。
进一步地,所述导流体基本呈从内口沿外口方向延伸的锥形体,所述气流收集通道与所述导流体之间形成环形气流通道,所述环形气流通道与所述叶轮外周面上对应呈环形设置的叶片相通,使得气流通道内收集的环形气流直接作用于所述叶轮外周面上环形设置的叶片上,从而驱动叶轮旋转。
进一步地,所述叶轮的侧面固定有用于将气流引导至周围叶片上的导流罩。
进一步地,所述至少一个叶轮室为至少两级叶轮室,各级叶轮共用动力输出轴装设于各级叶轮室内,在所述各级叶轮径向的外周面上固定有叶片,从前一级叶轮室流出的气流经气流通道作用于后一级叶轮室内的叶片上。
一种风能收集装置,包括前述风力发动机、气体压缩装置和储气罐,所述风力发动机输出的动力传动气体压缩装置,所述气体压缩装置产生的压缩气体输入储气罐储存。
一种装有前述风力发动机的机动车,风力发动机通过动力输出轴向机动车的传动轴输出动力。
进一步地,还包括至少两级压缩气体发动机,每一级压缩气体发动机包括至少一个叶轮室、通过转轴装设于所述叶轮室内的至少一个叶轮,每一级叶轮室上开设有至少一个进气口和至少一个排气口,其中前一级叶轮室上的排气口与后一级叶轮室上的进气口相通,每一级叶轮通过转轴向机动车的传动轴输出动力。
有益效果
采用上述技术方案,本发明有益的技术效果在于:
通过在气流收集通道内设置导流体,能够根据需要,灵活地改变导流体的大小和形状,使收集的气流更集中、更具有方向性。特别是,当应用于发动机时,可以将气流(风阻)直接导流到叶轮端部的叶片,产生更大的扭矩输出。另外,将气流(风阻)直接导流到叶轮端部的叶片上,避免了当气流流经叶轮叶片中心部位时因气流遇阻所产生的气流紊乱现象,提高发动机对风能的利用率。
附图说明
图1为本发明一种风力发动机的结构示意图。
图2是一种风能收集装置的结构示意图。
图3是一种机动车的结构示意图。
图4是图3中第一级压缩气体发动机的结构示意图。
图5是图3中第一级压缩气体发动机的叶轮室的局部结构放大示意图。
本发明的实施方式
下面通过具体实施方式,结合附图对本发明作进一步详细说明。
实施例一
一种风力发动机,如图1所示,包括气流收集装置、叶轮室4、通过动力输出轴7装设于叶轮室4内的叶轮6,在叶轮6径向的外周面上均分固定有叶片5,在叶轮6的侧面固定有用于将气流引导至外侧周围叶片5上的导流罩9。 气流收集装置包括外口大、内口小的气流收集通道1和导流体2。在气流收集通道1内设置导流体2,导流体2固定在靠近内口处的气流收集通道1的中轴线上,导流体2基本呈从内口沿外口方向延伸的锥形体,气流收集通道1与锥形2之间形成环形气流通道3,环形气流通道3与叶轮6外周面上对应呈环形设置的叶片5相通,使得气流通道3内收集的环形气流直接作用于叶轮6外周面上环形设置的叶片5上,从而驱动叶轮6旋转。风力发动机产生的动力由动力输出轴7经离合器8向外输出。
需要说明的是,本发明的发动机,既可以作为风阻发动机安装在风气发动机机动车上(申请号200780030483.8),接收机动车在行驶过程中的运动风阻,变阻力为动力;又可以安装在风力资源丰富的自然环境中,接收大自然的风力,产生动力输出,该动力输出既可以带动空气压缩机转化为压缩空气储存起来,也可以直接带动发电机输出电力。
实施例二
一种风能收集装置,如图2所示,包括风力发动机、气体压缩装置10和储气罐11,风力发动机的结构同实施例一,风力发动机输出轴7输出的动力经离合器8传动空气压缩装置10,空气压缩装置10产生的压缩空气输入储气罐11储存。
实施例三
一种机动车,如图3至图5所示,包括风阻发动机100、压缩气体发动机200和机动车的传动轴300。其中:
风阻发动机100,包括气流收集装置和两级风阻发动机。
气流收集装置包括外口大、内口小的气流收集通道101和导流体102。在气流收集通道101内设置导流体102,导流体102固定在靠近内口处的气流收集通道101的中轴线上,导流体102基本呈从内口沿外口方向延伸的锥形体,气流收集通道101与锥形102之间形成环形气流通道103。
两级风阻发动机包括叶轮室(104、106),两级叶轮(113、110)共用动力输出轴109装设于叶轮室(104、106)内,在两级叶轮(113、110)径向的外周面上均分固定有两级叶片(105、111),从前一级叶轮室104流出的气流经下一级气流通道112作用于后一级叶轮室106内的叶片111上。在叶轮(113、110)的侧面固定有用于将气流引导至外侧周围叶片(105、111)上的导流罩(114、108)。
第一级环形气流通道103与叶轮113外周面上对应呈环形设置的叶片105相通,使得气流通道103内收集的环形气流直接作用于叶轮113外周面上环形设置的叶片105上,从而驱动第一级叶轮113旋转。
第二级环形气流通道112与叶轮110外周面上对应呈环形设置的叶片111相通,使得第二级环形气流通道112内收集的、来自前一级叶轮室104流出的环形气流再一次作用于叶轮110外周面上环形设置的叶片111上,驱动第二级叶轮110旋转。
两极叶轮产生的动力由动力输出轴109输出。
压缩气体发动机200包括左侧压缩气体发动机、右侧压缩气体发动机和传动轴19,左右两侧压缩气体发动机呈左右对称结构。以左侧压缩气体发动机为例,左侧压缩气体发动机包括第一级压缩气体发动机210和第二级压缩气体发动机220,第一级压缩气体发动机210与第二级压缩气体发动机220共轴装设在同一转轴203上,左右两侧压缩气体发动机产生的动力经转轴203传动机动车的传动轴300。第一级压缩气体发动机210与第二级压缩气体发动机220的结构相同。
以第一级压缩气体发动机210为例,第一级压缩气体发动机210包括叶轮室215、通过转轴203装设于叶轮室215内的叶轮220,叶轮219上具有多个等分设置的叶齿216,叶轮室215上开设有多个进气口211和排气口212,进气口211上装设有喷嘴217,第一级叶轮室215上的排气口212与第二级叶轮室225上的进气口221相通。
如图4和图5所示,为了提高动力性能,在叶轮室215的内表面上开设有沿转动周面设置的、与进气口211相通的喷气导入槽213,接近进气口211时的喷气导入槽213深而宽,远离进气口211时的喷气导入槽213浅而窄(图5),喷气导入槽213的长度大于两个相邻叶齿216之间的距离L(标号218),使得从喷气导入槽213导出的压缩气体一是能够同时作用于二个或两个以上的叶齿216上,二是能够按照预设的导出路径作用在希望的叶齿部位,以产生更强的推力。另外,为了加大喷气力度,本实施例同一喷气导入槽213上装设两个喷嘴217。
在叶轮室215的内表面上开设有与转轴轴线平行的排气槽214,排气槽214与排气口212相通。为了更好的排气,排气槽214的宽度与叶轮220的宽度基本相一致。
第一级压缩气体发动机210的叶轮直径小,第二级压缩气体发动机220的叶轮直径大。为了使气体顺畅,第一级排气口212的直径是第一级进气口211的2—10倍,第二级排气口222的直径是第二级进气口221的2-10倍,可根据需要灵活设置。
为了防止漏气,避免刚喷入的气体直接从排气槽214排出,喷气导入槽213末端与最近的排气槽214之间的距离应大于两个相邻叶齿之间的距离L。
工作时,首先通过机动车的喷气系统(未画)经喷嘴217向第一级压缩气体发动机210内喷入压缩气体,经第一级压缩气体发动机210减压、稳压后进入第二级压缩气体发动机220。第一级压缩气体发动机210既起减压、稳压作用,又将释放压缩气体过程中产生的能量充分利用起来,第一级压缩气体发动机210同时提供部分动力。第二级压缩气体发动机220提供主动力。当机动车达到一定速度时,风阻气流经气流收集装置进入风阻发动机100产生辅助动力。
以上内容是结合具体的实施方式对本发明所作的进一步详细说明,不能认定本发明的具体实施只局限于这些说明。对于本发明所属技术领域的普通技术人员来说,在不脱离本发明构思的前提下,还可以做出若干简单推演或替换,都应当视为属于本发明的保护范围。

Claims (13)

  1. 一种气流收集装置,包括外口大、内口小的气流收集通道,其特征在于:在所述气流收集通道内设置有导流体。
  2. 根据权利要求1所述的气流收集装置,其特征在于:所述导流体固定在靠近内口处的气流收集通道的中轴线上,所述导流体基本呈从内口沿外口方向延伸的凸出部。
  3. 根据权利要求2所述的气流收集装置,其特征在于:所述导流体基本呈锥形体。
  4. 一种风力发动机,包括气流收集装置、至少一个叶轮室、通过动力输出轴装设于所述叶轮室内的至少一个叶轮,所述气流收集装置包括外口大、内口小的气流收集通道,其特征在于:在所述气流收集通道内设置有导流体,在所述叶轮径向的外周面上固定有叶片,所述导流体与所述气流收集通道之间形成的气流通道与所述叶片相通,使得气流通道内收集的气流直接作用于所述叶片上。
  5. 根据权利要求4所述的风力发动机,其特征在于:所述导流体固定在靠近内口处的气流收集通道的中轴线上,所述导流体基本呈从内口沿外口方向延伸的锥形体,所述气流收集通道与所述导流体之间形成环形气流通道,所述环形气流通道与所述叶轮外周面上对应呈环形设置的叶片相通,使得气流通道内收集的环形气流直接作用于所述叶轮外周面上环形设置的叶片上,从而驱动叶轮旋转。
  6. 根据权利要求4或5所述的风力发动机,其特征在于:所述叶轮的侧面固定有用于将气流引导至周围叶片上的导流罩。
  7. 根据权利要求4或5所述的风力发动机,其特征在于:所述至少一个叶轮室为至少两级叶轮室,各级叶轮共用动力输出轴装设于各级叶轮室内,在所述各级叶轮径向的外周面上固定有叶片,从前一级叶轮室流出的气流经气流通道作用于后一级叶轮室内的叶片上。
  8. 一种风能收集装置,包括权利要求4或5所述的风力发动机、气体压缩装置和储气罐,所述风力发动机输出的动力传动气体压缩装置,所述气体压缩装置产生的压缩气体输入储气罐储存。
  9. 一种风能收集装置,包括权利要求7所述的风力发动机、气体压缩装置和储气罐,所述风力发动机输出的动力传动气体压缩装置,所述气体压缩装置产生的压缩气体输入储气罐储存。
  10. 一种装有权利要求8所述风能收集装置的机动车,所述风能收集装置通过动力输出轴向机动车的传动轴输出动力。
  11. 一种装有权利要求9所述风能收集装置的机动车,所述风能收集装置通过动力输出轴向机动车的传动轴输出动力。
  12. 根据权利要求10所述的机动车,其特征在于:还包括至少两级压缩气体发动机,每一级压缩气体发动机包括至少一个叶轮室、通过转轴装设于所述叶轮室内的至少一个叶轮,每一级叶轮室上开设有至少一个进气口和至少一个排气口,其中前一级叶轮室上的排气口与后一级叶轮室上的进气口相通,每一级叶轮通过转轴向机动车的传动轴输出动力。
  13. 根据权利要求11所述的机动车,其特征在于:还包括至少两级压缩气体发动机,每一级压缩气体发动机包括至少一个叶轮室、通过转轴装设于所述叶轮室内的至少一个叶轮,每一级叶轮室上开设有至少一个进气口和至少一个排气口,其中前一级叶轮室上的排气口与后一级叶轮室上的进气口相通,每一级叶轮通过转轴向机动车的传动轴输出动力。
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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9802492B2 (en) 2015-12-07 2017-10-31 Smart Auto Labs Inc. Vehicle drag reduction and electricity generation system
US10500963B2 (en) 2015-12-07 2019-12-10 Smart Auto Labs Inc. Vehicle drag reduction and electricity generation system

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TWI709689B (zh) 2017-05-22 2020-11-11 李受勳 交通載具的風力發電設備
CN108979948B (zh) * 2018-07-24 2019-07-30 李素梅 一种电动汽车用空气放大器

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080170941A1 (en) * 2006-08-01 2008-07-17 Ghosh Dwipen N Wind turbine
CN101506524A (zh) * 2006-08-16 2009-08-12 丛洋 组合式风气发动机及机动车
CN201428560Y (zh) * 2009-05-19 2010-03-24 何幸华 储能风力发电装置
CN101725479A (zh) * 2008-10-27 2010-06-09 李泉洞 自升塔架导流体风力发电设备
CN201763511U (zh) * 2010-07-02 2011-03-16 丛洋 气流收集装置、风力发动机、风能收集装置及风力发电装置
CN201771672U (zh) * 2010-07-02 2011-03-23 丛洋 一种气流收集装置、风力发动机及机动车
CN201874623U (zh) * 2010-06-13 2011-06-22 丛洋 压缩空气发动机及机动车

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3812912A1 (de) * 1988-04-18 1988-12-01 Josef Klaus Windkraftanlage
CN101550915B (zh) * 2004-11-22 2013-10-16 丛洋 风气发动机的起动加速喷气系统
CN2825998Y (zh) * 2005-07-18 2006-10-11 崨豹科技有限公司 风力发电装置
CN101619703A (zh) * 2008-06-30 2010-01-06 李泉洞 高速风力涡轮发电设备
JP2009287545A (ja) * 2008-04-28 2009-12-10 Tomoyasu Yutaka 隔壁付定電圧風力発電機
CN201513202U (zh) * 2009-04-30 2010-06-23 丛洋 压缩气体发动机及机动车
CN201460992U (zh) * 2009-05-07 2010-05-12 丛洋 喷气嘴、喷气系统及机动车
CN201461001U (zh) * 2009-05-07 2010-05-12 丛洋 压缩气体供气系统及压缩气体机动车制冷系统

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080170941A1 (en) * 2006-08-01 2008-07-17 Ghosh Dwipen N Wind turbine
CN101506524A (zh) * 2006-08-16 2009-08-12 丛洋 组合式风气发动机及机动车
CN101725479A (zh) * 2008-10-27 2010-06-09 李泉洞 自升塔架导流体风力发电设备
CN201428560Y (zh) * 2009-05-19 2010-03-24 何幸华 储能风力发电装置
CN201874623U (zh) * 2010-06-13 2011-06-22 丛洋 压缩空气发动机及机动车
CN201763511U (zh) * 2010-07-02 2011-03-16 丛洋 气流收集装置、风力发动机、风能收集装置及风力发电装置
CN201771672U (zh) * 2010-07-02 2011-03-23 丛洋 一种气流收集装置、风力发动机及机动车

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9802492B2 (en) 2015-12-07 2017-10-31 Smart Auto Labs Inc. Vehicle drag reduction and electricity generation system
US10500963B2 (en) 2015-12-07 2019-12-10 Smart Auto Labs Inc. Vehicle drag reduction and electricity generation system

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