Pulse turbine engine

By designing multiple annular combustion chamber components and U-tube structures, a simple design and low-cost production of pulse turbine engines are realized, which solves the complex problems of traditional engine combustion accessories and achieves jet stability.

CN222576760UActive Publication Date: 2025-03-07杨辉
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Patent Information

Application Number
CN202322982608.6
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2023-11-06
Publication Date
2025-03-07
Estimated Expiration
2033-11-06

AI Technical Summary

Technical Problem

The combustion accessories of the pulse engine are complex, which increases the difficulty of making it.

Method used

A pulse turbine engine is designed, using multiple annular combustion chamber components, a tail exhaust pipe is arranged at the bottom of the combustion chamber body, an intake pipe is arranged at the top, and a tail exhaust pipe is connected to an exhaust main pipe. Two U-shaped pipes are arranged at the top of the combustion chamber body to replace traditional blades or pistons to achieve the simultaneous operation of compressed air and exhaust.

Benefits of technology

A simple jet design is realized, without moving parts, low production costs and stable jets, solving the problem of complex combustion accessories of traditional engines.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model discloses a pulse turbine engine which comprises a plurality of combustion chamber assemblies, the combustion chamber assemblies are arranged in a ring shape in the circumferential direction, each combustion chamber assembly comprises a combustion chamber body, a tail exhaust pipe is arranged at the bottom of each combustion chamber body, an air inlet pipe is arranged at the top of each combustion chamber body, and each tail exhaust pipe is connected to an exhaust main pipe. Two U-shaped pipes are further arranged at the top of the combustion chamber body, a simple jet can be formed through the multiple annularly-arranged combustion set assemblies, no movable part is arranged, production is easy, the cost is low, traditional blades or pistons are replaced by the U-shaped pipes in the combustion chamber, air compression and air exhaust are conducted at the same time, and the combustion efficiency is improved. The multiple combustion chambers spray air to do work in a pulse mode, and air spraying is stable.
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Description

Technical Field

[0001] The utility model relates to the technical field of engines, in particular to a pulse turbine engine. Background Art

[0002] The pulse engine is an air-breathing engine that uses pulsed deflagration to generate thrust. The unique working principle of the pulse engine determines that it has advantages that other engines cannot match, mainly in the following aspects: since there are no rotating parts such as compressors and turbines, it is light in weight, has a high thrust-to-weight ratio, and unlike ramjet engines, it can be started statically on the ground. However, the combustion accessories of the pulse engine are complex, which increases its difficulty in production. Utility Model Content

[0003] In order to solve the above technical problems, the technical solution provided by the utility model is: a pulse turbine engine, comprising a plurality of combustion chamber assemblies, wherein the plurality of combustion chamber assemblies are arranged circumferentially in a ring, the combustion chamber assembly comprising a combustion chamber body, a tail exhaust pipe is arranged at the bottom of the combustion chamber body, an intake pipe is arranged at the top, the tail exhaust pipe is connected to an exhaust main pipe, and two U-shaped tubes are also arranged on the top of the combustion chamber body, one of the U-shaped tubes is connected to the intake pipe on the current combustion chamber body, and the other U-shaped tube is connected to the intake pipe on the combustion chamber body behind the current combustion chamber body in a clockwise direction.

[0004] The advantages of the present invention over the prior art are as follows: the present invention can form a simple jet through a plurality of annularly arranged combustion group components, has no moving parts, is easy to produce and has low cost; in the present solution, a U-shaped tube is used in the combustion chamber to replace the traditional blades or pistons, so that compression and exhaust are carried out simultaneously; and a plurality of combustion chambers jet in the form of pulses to make the jet stable. BRIEF DESCRIPTION OF THE DRAWINGS

[0005] Figure 1 The utility model is a schematic structural diagram of a pulse turbine engine.

[0006] Figure 2 The utility model is a schematic structural diagram of a U-shaped tube in a pulse turbine engine.

[0007] Figure 3 It is a schematic diagram of the top structure of a pulse turbine engine of the utility model. DETAILED DESCRIPTION

[0008] In order to make the purpose, technical scheme and advantages of the embodiments of the utility model clearer, the technical scheme in the embodiments of the utility model will be clearly and completely described below in conjunction with the drawings in the embodiments of the utility model. Obviously, the described embodiments are part of the embodiments of the utility model, not all of the embodiments. Generally, the components of the embodiments of the utility model described and shown in the drawings here can be arranged and designed in various different configurations.

[0009] In the description of the embodiments of the present utility model, it should be noted that if the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inside", "outside", etc. indicate an orientation or position relationship based on the orientation or position relationship shown in the accompanying drawings, or the orientation or position relationship in which the utility model product is usually placed when in use, it is only for the convenience of describing the utility model and simplifying the description, and does not indicate or imply 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 on the present utility model. In addition, the terms "first", "second", "third", etc. are only used to distinguish the description, and cannot be understood as indicating or implying relative importance.

[0010] In addition, the terms "horizontal", "vertical", "overhanging" and the like do not mean that the components must be absolutely horizontal or overhanging, but can be slightly tilted. For example, "horizontal" only means that its direction is more horizontal than "vertical", and does not mean that the structure must be completely horizontal, but can be slightly tilted.

[0011] In the description of the embodiments of the present invention, "multiple" means at least 2.

[0012] In the description of the embodiments of the present utility model, it is also necessary to explain that, unless otherwise clearly specified and limited, the terms "set", "install", "connect", and "connect" 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 a direct connection, or it can be indirectly connected through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in the present utility model can be understood according to specific circumstances.

[0013] Example:

[0014] Combined with Figure 1-3The present embodiment discloses a pulse turbine engine, comprising a plurality of combustion chamber assemblies 1, which are arranged circumferentially in a ring, the combustion chamber assembly 1 comprising a combustion chamber body 101, a tail exhaust pipe 102 is arranged at the bottom of the combustion chamber body 101, an intake pipe 103 is arranged at the top, the tail exhaust pipe 102 is connected to an exhaust main pipe 2, two U-shaped tubes 104 are also arranged at the top of the combustion chamber body 101, one of the U-shaped tubes 104 is connected to the intake pipe 103 on the current combustion chamber body 101, and the other U-shaped tube 104 is connected to the intake pipe 103 on the next combustion chamber body 101 behind the current combustion chamber body 101 in a clockwise direction; the intake pipe 103 is a conical wide mouth with an opening gradually increasing from bottom to top; an ignition device 106 is arranged on the outside of the combustion chamber body 101; and a fuel port 105 is arranged on the U-shaped tube 104.

[0015] In this embodiment, multiple combustion chamber assemblies form a ring, and the tail exhaust pipes are connected to the same exhaust main pipe. A turbine may or may not be installed in the exhaust main pipe. The intake pipe is configured to have a conical wide mouth, which can have a stamping effect. This embodiment forms a simple jet, which mainly has no moving parts and is easy to produce at a low cost. The combustion chamber uses a U-shaped tube instead of a blade or a piston, and compression and exhaust are carried out simultaneously. Multiple combustion chambers work by jetting in the form of pulses to make the jet stable.

[0016] The above description of the utility model and its implementation methods is not restrictive. The drawings show only one implementation method of the utility model, and the actual structure is not limited thereto. In short, if ordinary technicians in this field are inspired by it and design structural methods and embodiments similar to the technical solution without creativity without departing from the purpose of the invention of the utility model, they should all fall within the protection scope of the utility model.

Claims

1. A pulse turbine engine, characterized in that: It includes multiple combustion chamber assemblies, which are arranged circumferentially in a ring. The combustion chamber assembly includes a combustion chamber body. A tail exhaust pipe is arranged at the bottom of the combustion chamber body, and an intake pipe is arranged at the top. The tail exhaust pipe is connected to an exhaust main pipe. Two U-shaped tubes are also arranged on the top of the combustion chamber body, one of which is connected to the intake pipe on the current combustion chamber body, and the other U-shaped tube is connected to the intake pipe on the combustion chamber body behind the current combustion chamber body in a clockwise direction.

2. A pulse turbine engine according to claim 1, characterized in that: The air inlet pipe is a conical wide opening with the opening gradually increasing from bottom to top.

3. A pulse turbine engine according to claim 1, characterized in that: An ignition device is arranged outside the combustion chamber body.

4. A pulse turbine engine according to claim 1, characterized in that: The U-shaped tube is provided with a fuel port.