阅读说明：本技术 冲压式反冲推进发动机及其应用 (Ram type recoil propulsion engine and application thereof ) 是由 李宏江 于 2019-11-01 设计创作，主要内容包括：本发明是冲压式反冲推进发动机及其应用,目的是改变传统的动力发动机配用模式,增加其使用范围和提高其节能环保性能、简化其工作原理和构造结构等优点。主要通过将飞机上使用的冲压式发动机移用于火箭、高铁、动车、航母舰艇、导弹炮弹上配套使用。另外将该发动机安装在转盘轮上构成与传统可调速的发动机配套各种汽车、坦克、装甲车使用,实现取代传统发动机的最终目的。(The invention relates to a ram recoil propulsion engine and application thereof, aiming at changing the matching mode of the traditional power engine, increasing the application range thereof, improving the energy-saving and environment-friendly performance thereof, simplifying the working principle and the structural structure thereof and the like. The stamping engine used on the airplane is mainly used for matching rocket, high-speed rail, bullet train, aircraft carrier and missile cannonball. In addition, the engine is arranged on a turntable wheel to form a complete set with the traditional speed-adjustable engine for various automobiles, tanks and armored vehicles, thereby realizing the final purpose of replacing the traditional engine.)

1. The ram recoil propulsion engine and its application characteristic are: the invention relates to a ram engine, also called a propeller, which is an engine for pushing a machine device to move forwards or backwards as the name suggests, compared with a jet engine in an airplane, the ram engine is the most similar engine and is also one of the ram engines, the ram engine comprises an engine shell 1, a fuel storage tank 2, an air suction cylinder port 3, a combustion chamber 4, an air jet port 5, a remote control fuel nozzle 6, a remote control electronic igniter 7, a fuel switch 8 and a one-way air inlet valve 9, and the structure connection relationship is characterized in that: the front end of a shell (1) is provided with an air suction cylinder opening (3), the middle or the front end of the air suction cylinder opening (3) is provided with a fuel tank (2), the bottom of the fuel tank (2) is provided with a remote control fuel switch (8), the top end of the fuel tank (2) is provided with a one-way stamping air inlet valve (9) for air inlet and fuel compression to be discharged into a combustion chamber for continuous combustion, the rear pipe orifice of the fuel switch (8) is connected with a spiral-shaped rotary fuel heating gas fuel nozzle (6) and extends into the middle lower part of the combustion chamber (4) (used for burning and heating diesel oil and gas in a spiral pipe to be mixed with oxygen-containing air and stamped in for full combustion through electronic ignition, high-temperature and high-pressure gas is sprayed out to a gas nozzle at the rear end to generate recoil thrust to push the whole engine cylinder to fly forwards, but if the adopted fuel is oxygen-containing gunpowder or gas, the spiral-shaped fuel heating gas fuel nozzle is not necessarily, ) Then a remote control type electronic igniter (7) is arranged at the mixing space position of a fuel nozzle opening and an air inlet of the combustion chamber (4), namely the space position of a mixing area of fuel and oxygen-containing air to form a ram type recoil propulsion engine (used for igniting mixed gas to continuously combust to generate a large amount of high-temperature high-pressure gas to be sprayed out to a nozzle opening and generate strong recoil thrust to push the whole engine cylinder to fly forwards! ).

2. The ram recoil propulsion engine and its application characteristic are: embodiment two: the disc wheel four-stamping engine combined engine comprises stamping engines 1, 2, 3 and 4, a disc wheel 5, a driving wheel 6, a main shaft 7, a movable support 8, a shell fixing seat 9, a disc wheel shell 10, a shell counter flow plate 11, an exhaust pipe ball 12, a neutralization and purification liquid medicine box or a steam storage box 13 and a main bearing 14, and is characterized in that the device is specifically assembled and connected with the following components: a stamping type recoil engine of a scheme I is respectively arranged on the surface or four-way side edges of a disk wheel (5), namely 4 stamping type engines (1), (2), (3) and (4) of a scheme II are totally arranged, a main bearing (14) is arranged at the center of the disk wheel (5), then a main shaft (7) is sleeved in the main shaft, the main shaft (7) can be horizontal type or vertical type, generally horizontal type better fixed transmission is convenient, a transmission wheel (6) is fixed in the middle of the disk wheel (5) and used for outward transmission, a movable support (8) is used for supporting the disk wheel (5) to reduce bounce when the disk wheel rotates at high speed, the bounce is reduced because the weight and the installation size of the 1, 2, 3 and 4 stamping type engines arranged on the wheel surface are not necessarily symmetrical, the bounce can be generated when the disk wheel rotates at high speed, a shell shaking fixing seat (9) is used for fixing a shell (10) on a foundation base or a frame, because the shell baffle plate (11) is arranged in the shell of the shell (10) and is specially used for resisting the high-speed airflow sprayed from the tail part of the ram-type recoil propulsion engine, and the shell can also have recoil thrust, if the shell is not fixed, the shell can also rotate, in addition, the top of the shell (10) is provided with an exhaust pipe ball (12) by a perforation, and harmful substances such as carbon dioxide, sulfur monoxide, sulfur dioxide and the like are discharged by using a dispersed porous ball, the liquid medicine passing through the neutralization purification box (13) is neutralized and purified to generate two states of chemical sediment and water vapor, the chemical sediment is left in the liquid to be concentrated, the water vapor is stored in a cooling box or exchanged by a heat exchanger to generate heating for heating or directly supplying the steam to a turbonator for generating electricity, and the invention also discloses two using modes of the device.

The technical field is as follows: the invention relates to a ram recoil propulsion engine and application thereof, belonging to the field of jet engines.

Background art: the most similar to the invention is the jet engine used on the airplane, the working principle of the jet engine and the jet engine are basically similar, but the jet engine is not matched with the airplane to be used as a power machine, but is matched with the automobile, the train and the motor vehicle or the competitive motor vehicle or used on the boat, the ballistic missile, the fire-fighting missile, the cannon shell or the novel rocket. The engine is a main engine, and the matching combination application of the engine and the various vehicles, ships, missiles and the like will be respectively described in detail.

The invention content is as follows: the invention is characterized in that a jet engine in the jet plane is reformed to be suitable for various ram engines which need to be used on devices matched with the jet engine, and then the ram engines are assembled into various new products according to the matched structure of a single device, such as rocket boosters, ballistic missile propellers or fire-fighting missile transmitters, remote cannonball propellers, train motor train unit propellers or tank armored car engines or boosters of aircraft carriers, in particular to booster or main-boost propeller engines matched with devices such as aircrafts flying in the air, aircrafts sailing on the water surface and the like.

Description of the drawings:

1. FIG. 1 is a schematic diagram of a first embodiment of the present invention.

2. FIG. 2 is a schematic diagram of the second embodiment.

The first embodiment is as follows: the invention relates to a ram engine, also called a propeller, which is an engine for pushing a machine device to move forwards or backwards as the name suggests, compared with a jet engine in an airplane, the ram engine is the most similar engine and is also one of the ram engines, the ram engine comprises an engine shell 1, a fuel storage tank 2, an air suction cylinder port 3, a combustion chamber 4, an air jet port 5, a remote control fuel nozzle 6, a remote control electronic igniter 7, a fuel switch 8 and a one-way air inlet valve 9, and the structure connection relationship is characterized in that: the front end of the shell (1) is provided with an air suction tube opening (3), the middle or the front end of the air suction tube opening (3) is provided with a fuel tank (2), the bottom of the fuel tank (2) is provided with a remote control type fuel switch (8), and the top end of the fuel tank (2) is provided with a one-way stamping air inlet valve (9) for air inlet and fuel compression to be discharged into a combustion chamber for continuous combustion. A screw-shaped rotary fuel-heated gas fuel nozzle (6) is connected to the rear pipe orifice of a fuel switch (8) and extends into the middle-lower part of a combustion chamber (4) (used for burning and heating diesel oil in the screw pipe into oil gas for being mixed and punched to contain oxygen-containing air, the oxygen-containing air is fully combusted through electronic ignition and is changed into high-temperature and high-pressure gas to be sprayed out to a gas nozzle at the rear end, and recoil thrust is generated to push the whole engine cylinder to fly forwards, but if the fuel is oxygen-containing powder or gas, a spiral fuel-heated gas fuel nozzle does not need to be installed), and then a remote control electronic igniter (7) is installed at the mixing space position of the fuel nozzle and the air inlet of the combustion chamber (4), namely the space position of the mixing area of the fuel and the oxygen-containing air, so as to form the ram type recoil propulsion engine. (for igniting the mixed gas to continuously burn and produce a large amount of high-temperature high-pressure gas to spray out to the gas nozzle, and produce strong recoil thrust to push the whole engine cylinder to rapidly advance forward!)