Multipurpose engine

Abstract

The invention discloses a multi-purpose engine, which utilizes a distortion space mechanism to distort and absorb surrounding fluid to generate strong thrust, does not reflect radar waves during operation and has excellent stealth, and the loading capacity of the multi-purpose engine is determined by the size and the rotating speed of an internal rotating part. A twisted light cone design is adopted, rotation reaches a specific speed and can suspend by means of space compression reaction force, and a middle cockpit design enables the aircraft to have an underwater take-off capability; when the device is applied to an aircraft, a cockpit and an engine body are arranged in the middle, an external bent duct guides airflow to provide lift force, an aero-engine is installed at the tail, and when the air pressure is too large, wrapping cyclone is formed to achieve active defense; the internal dragon tail structure twists a compression space, and a curve speed engine is formed during gradient superposition; the keel provides structural support, the space compression duct achieves efficient space movement, the center blade duct optimizes airflow, the energy conversion efficiency and thrust are improved, and the system can be applied to the fields of aerospace, water traffic, defense and the like.

Description

Technical Field

[0001] The present invention relates to the technical field of engines, and particularly to a multi-purpose engine that can be applied to multiple fields such as aerospace, water transportation, and special defense. Background Art

[0002] Traditional engines have many limitations in terms of thrust, stealth performance, multi-purpose capabilities, etc. In the aerospace field, traditional engines are difficult to meet the requirements for higher thrust and more flexible flight modes; in the water transportation field, engines are difficult to balance efficient operation in different environments above and below the water surface; in terms of defense, traditional engines lack effective active defense mechanisms. In addition, there is also room for improvement in the space utilization and energy conversion efficiency of traditional engines, and they cannot adapt to the increasingly complex and diverse application scenarios. Therefore, it is of great practical significance to develop a new type of engine with greater thrust, better stealth performance, and stronger multi-purpose capabilities. Summary of the Invention

[0003] The purpose of the present invention is to provide a multi-purpose engine that has greater thrust than traditional engines, has good stealth performance, can operate efficiently in various environments and applications, and has a certain active defense ability to overcome the deficiencies of existing engine technologies.

[0004] To achieve the above purpose, the present invention is realized through the following technical solutions:

[0005] A multi-purpose engine twists space in a specific way, twists and absorbs the surrounding fluid to generate thrust, and has the stealth characteristic of not reflecting radar waves in the operating state.

[0006] Furthermore, the load capacity of the engine is jointly determined by its own size and the rotational speed of the internal rotating components, and different loads can be effectively carried by adjusting the size and rotational speed.

[0007] Furthermore, the design concept of twisting the light cone is adopted, the expanded space is restored and compressed to the starting point as the supporting force, and when the rotational speed of the engine reaches the preset threshold, suspension is achieved by means of the reaction force generated by the space compression; and the middle area of the engine is designed as a cockpit, enabling the engine to have the special ability to take off in water.

[0008] Furthermore, it has the function of gradient rotation superposition. When applied to an aircraft, the aircraft is structurally designed with this engine as the core. A cockpit and an engine main body are arranged in the middle of the engine, and curved ducts are equipped outside. The curved ducts are used to guide the airflow to provide lift for the aircraft.

[0009] Furthermore, an aeroengine is installed at the tail of the curved duct. When the aeroengine operates, the airflow generated wraps the engine body. When the tail air pressure exceeds the set value, a wrapping air vortex is formed. This air vortex constitutes a rotating air wall that wraps the central area of the engine and can deflect approaching objects, achieving active defense.

[0010] Furthermore, the engine internally includes a "dragon tail" structure and a "dragon head" structure. The dragon tail is located below the dragon head and is used to realize the functions of twisting, coiling, folding, and compressing space. When the engine adopts a gradient superposition design, it forms a warp drive engine as a whole, achieving a more efficient power output and operation mode.

[0011] Furthermore, a keel and a space compression duct are provided inside the engine. The keel provides stable structural support for the engine, and the space compression duct realizes the efficient movement of the engine in space through a space distortion mechanism. The two work together to ensure the stable operation of the engine.

[0012] Furthermore, a central vane duct is provided inside the space compression duct. Through the design of specific shapes and angles, the central vane duct optimizes the flow state of the airflow in the duct, improving the energy conversion efficiency and thrust output of the engine.

[0013] Furthermore, the active defense function automatically adjusts the operating parameters of the aeroengine by the control system according to the threat level, precisely controls the tail air pressure, and thus adjusts the intensity and range of the wrapping air vortex to achieve different levels of defense effects.

[0014] Furthermore, the ability to take off in water is achieved through the space distortion and suspension principle of the engine, combined with the structural design of the middle cockpit of the engine and the special action mode of the engine on water flow. After the engine starts in water, it reaches the critical state of suspension and takeoff through specific rotational speed control.

[0015] Compared with the prior art, the beneficial effects of the present invention are as follows:

[0016] 1. Thrust improvement: Through unique space distortion and fluid absorption mechanisms, the multi-purpose engine of the present invention can generate greater thrust than traditional engines, providing stronger power support for large aircraft in the fields of aerospace, etc., and helping to achieve faster flight speeds and greater payload capabilities.

[0017] 2. Excellent stealth performance: The engine does not reflect radar waves during operation, greatly reducing the probability of being detected, which has important strategic significance in both military and civilian fields; in military applications, it can improve the survivability and penetration ability of aircraft; in civilian fields, it helps to reduce interference and impact on the surrounding environment.

[0018] 3. Strong versatility: This engine is not only applicable to the aerospace field, but also can be used in multiple fields such as water transportation and special defense; its ability to take off in water provides new ideas for the design and research and development of water vehicles, while the active defense function enhances the safety of aircraft in complex environments and broadens the application scope of the engine.

[0019] 4. Efficient space utilization and energy conversion: Through ingenious space compression and distortion design, the engine can utilize space more efficiently and achieve efficient energy conversion; with the same volume and weight, it can output greater power, improve energy utilization efficiency, and reduce operating costs. Brief Description of the Drawings

[0020] Figure 1 It is a structural diagram of a multi-purpose engine of the present invention.

[0021] Among them, 1. Engine, 2. Keel, 3. Central blade duct. Detailed Embodiment

[0022] To make the objectives, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are some, but not all, of the embodiments of the present invention. Usually, the components of the embodiments of the present invention described and shown in the drawings here can be arranged and designed in various different configurations.

[0023] In the description of the embodiments of the present invention, it should be noted that if terms such as "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. are used to indicate the orientation or positional relationship, it is based on the orientation or positional relationship shown in the drawings, or the orientation or positional relationship in which the product of the invention is usually placed when in use. It is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation of the present invention. In addition, terms such as "first", "second", "third", etc. are only used for distinguishing descriptions and cannot be understood as indicating or implying relative importance.

[0024] In addition, if terms such as "horizontal", "vertical", "overhanging", etc. are used, it does not mean that the component is required to be absolutely horizontal or overhanging, but can be slightly inclined. For example, "horizontal" only means that its direction is more horizontal relative to "vertical", and does not mean that the structure must be completely horizontal, but can be slightly inclined.

[0025] In the description of the embodiments of the present invention, "a plurality of" represents at least 2.

[0026] In the description of the embodiments of the present invention, it should also be noted that unless otherwise clearly specified and defined, if the terms "set", "installed", "connected", and "connected" appear, they should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be directly connected, or indirectly connected through an intermediate medium, and it can be the communication inside two components. For those of ordinary skill in the art, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.

[0027] Embodiment:

[0028] A multi-purpose engine provided by the present invention

[0029] Basic structure and principle

[0030] The core design of the multi-purpose engine of the present invention is based on the unique principle of space distortion and energy conversion. It distorts space in a specific way, absorbs and distorts the surrounding fluid, thereby generating a powerful thrust. This space distortion mechanism enables the engine not to reflect radar waves during operation and has excellent stealth performance.

[0031] The size and rotational speed of the engine are the key factors determining its load capacity. By precisely controlling the size of the engine and the rotational speed of the internal rotating components, effective loading of different loads can be achieved to meet the power requirements in various application scenarios.

[0032] Space compression and suspension principle

[0033] The engine adopts the design concept of a twisted light cone, which can restore and compress the expanding space to the starting point as a supporting force; when the engine reaches a certain rotational speed, using the reaction force generated by this space compression, the engine can achieve a suspension effect.

[0034] In terms of the appearance design, the middle part of the engine is designed as a cockpit; when the engine is applied to the water environment, this design combines its space distortion and suspension principles, enabling the engine to have the ability to take off in water, breaking the limitations of traditional engines in water application scenarios.

[0035] Multi-purpose aircraft design

[0036] This engine has the function of gradient rotation superposition and can be applied to aircraft design; the overall structure of the aircraft is centered around the engine, with a cockpit and the engine main body in the middle, and curved ducts are equipped outside; the design of the curved ducts can skillfully guide the airflow to provide lift for the aircraft and ensure the stable flight of the aircraft.

[0037] Install an aero-engine at the tail of a curved duct. When the aero-engine operates, the generated airflow will wrap around the engine core (i.e., the main part of the engine). When the air pressure at the tail is too high, a wrapped air vortex will be formed. This rotating air wall can wrap the central area. When an object approaches, the powerful airflow generated by the air vortex will deflect the object, thus realizing the active defense function and effectively protecting the safety of the aircraft and the personnel and equipment carried on it.

[0038] Space Compression and Distortion Structure

[0039] The engine contains "dragon tail" and "dragon head" structures inside. The dragon tail is located below the dragon head. The dragon tail plays the role of distorting, spiraling, folding, and compressing space. Through this complex space operation, the performance of the engine is further enhanced.

[0040] When the engine adopts a gradient superposition design, the overall composition forms a warp drive engine, which can utilize the space distortion principle more efficiently, achieve more powerful power output and more flexible operation modes.

[0041] The keel works in coordination with the space compression duct. The keel provides stable structural support for the engine, and the space compression duct realizes the efficient movement of the engine in space through the space distortion mechanism. As one of the key components of the engine, the central blade duct optimizes the airflow by reasonably designing its shape and angle, improving the energy conversion efficiency and thrust output of the engine.

[0042] Application Scenarios and Operation Methods

[0043] Aerospace Field

[0044] Aircraft Design: When applying a multi-purpose engine to an aircraft, according to the design requirements of the aircraft, reasonably determine the installation position and quantity of the engine. The middle cockpit is designed according to ergonomic principles, providing a comfortable and safe operation environment for the pilot. The installation position and angle of the curved duct and the aero-engine need to be accurately calculated to ensure that the aircraft can obtain the best lift and defense effects during flight.

[0045] Flight Operation: During flight, the pilot precisely adjusts the rotation speed and rotation direction of the engine through the control system to achieve actions such as takeoff, cruise, and landing of the aircraft. When it is necessary to enhance the defense ability, by adjusting the working parameters of the aero-engine, the air pressure at the tail is adjusted to an appropriate level to form a wrapped air vortex for active defense against approaching objects.

[0046] Water Transportation Field

[0047] Watercraft Design: For watercraft, the engine is designed to have a structure adaptable to the aquatic environment. The engine housing is made of waterproof and corrosion-resistant materials to ensure normal operation in different underwater and waterborne environments. The middle cockpit has good visibility and sealing performance, facilitating the operation of the driver.

[0048] Waterborne Operation: During takeoff on water, the driver uses the control system to make the engine reach a certain rotational speed and utilizes the levitation force generated by spatial compression to achieve takeoff. During the waterborne navigation process, the power output of the engine is reasonably adjusted according to the navigation speed and load conditions to ensure the stable navigation of the watercraft.

[0049] Special Defense Field

[0050] Defense System Integration: The multi-purpose engine is integrated into the special defense system as the core component of active defense. According to the requirements of the defense scenario, the quantity and position of the engines are reasonably arranged to ensure all-round protection of the target area.

[0051] Defense Operation: When a threatening object is detected approaching, the defense system automatically starts the engine. By adjusting the operating state of the aviation engine, a powerful enveloping air vortex is formed at the tail. The airflow generated by the air vortex deflects the approaching object to achieve effective defense of the target.

[0052] The above describes the present invention and its implementation manners. Such description is not restrictive. What is shown in the drawings is only one of the implementation manners of the present invention, and the actual structure is not limited thereto. In short, if those of ordinary skill in the art are inspired by it and, without departing from the gist of the present invention, creatively design a structural manner and an embodiment similar to the technical solution, they shall fall within the protection scope of the present invention.

Claims

1. A multi-purpose engine, characterized in that: Distort space in a specific way, distort and absorb the surrounding fluid to generate thrust, and have the stealth characteristic of not reflecting radar waves in the operating state.

2. The multi-purpose engine according to claim 1, characterized in that: The load capacity of the engine is jointly determined by its own size and the rotational speed of the internal rotating components, and different loads can be effectively carried by adjusting the size and rotational speed.

3. The multi-purpose engine according to claim 1, characterized in that: Adopt the design concept of a distorted light cone, restore and compress the expanding space to the starting point as the supporting force. When the engine rotation speed reaches the preset threshold, suspension is achieved by means of the reaction force generated by this space compression; and the middle area of the engine is designed as a cockpit, enabling the engine to have the special ability to take off in water.

4. A multi-purpose engine according to claim 1, characterized in that: It has the function of gradient rotation superposition. When applied to an aircraft, the aircraft is structurally designed with this engine as the core. A cockpit and an engine main body are arranged in the middle of the engine, and curved ducts are equipped outside. The curved ducts are used to guide the airflow to provide lift for the aircraft.

5. A multi-purpose engine according to claim 4, wherein: An aeroengine is installed at the tail of the curved duct. The airflow generated when the aeroengine works wraps the engine main body; when the tail air pressure exceeds the set value, a wrapped air vortex is formed. This air vortex constitutes a rotating air wall that wraps the central area of the engine and can deflect approaching objects to achieve active defense.

6. A multi-purpose engine according to claim 1, characterized in that: The engine interior contains a "dragon tail" structure and a "dragon head" structure. The dragon tail is located below the dragon head and is used to achieve the functions of distorting, coiling, folding, and compressing space; when the engine adopts a gradient superposition design, the whole forms a warp engine to achieve a more efficient power output and operating mode.

7. A multi-purpose engine according to claim 1, characterized in that: The engine interior is provided with a keel and a space compression duct. The keel provides stable structural support for the engine, and the space compression duct realizes the efficient movement of the engine in space through a space distortion mechanism. The two work together to ensure the stable operation of the engine.

8. A multi-purpose engine according to claim 7, characterized in that: The space compression duct is internally provided with a central vane duct. The central vane duct is designed with a specific shape and angle to optimize the flow state of the airflow in the duct and improve the energy conversion efficiency and thrust output of the engine.

9. A multi-purpose engine according to claim 5, characterized in that: The active defense function automatically adjusts the working parameters of the aeroengine by the control system according to the threat level, accurately controls the tail air pressure, and thus adjusts the intensity and range of the wrapped air vortex to achieve different levels of defense effects.

10. A multi-purpose engine according to claim 3, characterized in that: The ability to take off in water is achieved through the space distortion and suspension principle of the engine, combined with the structural design of the middle cockpit of the engine and the special action mode of the engine on water flow. After the engine starts in water, the critical state of suspension and takeoff is reached through specific rotational speed control.

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