Double-turbine coaxially-connected device

A twin-turbo, coaxial technology, used in machines/engines, internal combustion piston engines, mechanical equipment, etc., can solve the problems of complex structure of the supercharging system, and achieve the effect of simple structure and reasonable design.

CN102926859AInactive Publication Date: 2013-02-13SHANGHAI JIAO TONG UNIV
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Publication Date
2013-02-13
Estimated Expiration
Not applicable · inactive patent

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Abstract

The invention relates to a double-turbine coaxially-connected device which belongs to the technical field of internal-combustion engines. The double-turbine coaxially-connected device comprises air compressors, an air inlet pipe, an engine, an air exhaust pipe, turbines, a volume cavity, a connecting pipe, a movable body, a spring and through tubes, wherein the movable body is arranged in the volume cavity and is hermetically contact with the inner wall surface of the volume cavity; the first through tube and the second through tube both penetrate through the upper wall surface and the lower wall surface of the movable body; and the right wall surface of the movable body is connected with the right wall surface of the volume cavity through the spring. When the engine is under a high-speed working condition, the movable body moves towards right, the first air compressor, the second air compressor, the first turbine and the second turbine work simultaneously, and the engine is lower in pumping loss, so that the engine is better in overall machine performance; when the engine is under a low-speed working condition, the movable body moves towards left, only the first air compressor and the first turbine work, pulse energy is sufficiently utilized, and the engine is higher in inlet pressure, so that the engine is better in overall machine performance. The double-turbine coaxially-connected device is reasonable in design, simple in structure and suitable for a turbocharging system with double turbines and double air compressors.
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Description

technical field

[0001] The invention relates to a turbocharger system in the field of internal combustion engines, in particular to a twin-turbine coaxial connection device. Background technique

[0002] With the development of society and the improvement of environmental protection requirements, the application of engine supercharging technology is becoming more and more extensive. Most of the engines with medium and high power adopt turbocharging technology to improve power and reduce fuel consumption. The two basic types of turbocharging systems are constant pressure supercharging system and pulse supercharging system. Constant-pressure supercharging system, each cylinder shares a large-volume exhaust pipe, the structure of the exhaust pipe system is relatively simple, the equivalent flow area of ​​the turbine is relatively large, the pressure in the exhaust pipe is basically kept constant, and the pressure is only related to the load of the engine It is related to the r...

Examples

Embodiment

[0014] Such as figure 1 and figure 2 As shown, the present invention includes: a first air suction pipe 1, a first air compressor 2, a first air outlet pipe 3, a first turbine 4, a second air suction pipe 5, a second air compressor 6, a second air outlet pipe 7, Second turbine 8, engine intake pipe 9, engine 10, engine exhaust pipe 11, connecting shaft 12, volume cavity 13, volume cavity upper wall 14, volume cavity lower wall 15, volume cavity left wall 16, volume cavity right wall 17 , volume chamber front wall 18, volume chamber rear wall 19, moving body 20, spring 21, first connecting pipe 22, second connecting pipe 23, third connecting pipe 24, fourth connecting pipe 25, fifth connecting pipe 26, The first through pipe 27 and the second through pipe 28, the air inlet and outlet of the first compressor 2 are respectively connected with the air outlet of the first suction pipe 1 and the air inlet of the engine intake pipe 9, and the inlet of the second air compressor 6 T...