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A visual full-ring model combustion chamber with removable head structure

A combustion chamber and head technology, applied in the field of visual full-ring combustion chamber, can solve problems such as distortion, inability to adjust the size of the combustion chamber, and inability to observe the flow of the combustion chamber, etc., to achieve the effect of shortening the processing cycle and saving economic costs

Active Publication Date: 2021-08-06
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

Patent "diesel engine combustion chamber with visual window", patent number CN107023378B, its structure is: quartz cylinder liner and metal cylinder liner, the extended piston is placed in the quartz cylinder liner and metal cylinder liner, which solves the convection field of the traditional simplified combustion chamber Distortion and difficulty in obtaining the vertical flow field in the combustion chamber
Although these patents have achieved a lot of results, there are still some problems, such as the structure can be replaced, but the flow in the combustion chamber cannot be observed, or the flow field of the combustion chamber can be obtained, but the size of the combustion chamber cannot be adjusted

Method used

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  • A visual full-ring model combustion chamber with removable head structure
  • A visual full-ring model combustion chamber with removable head structure
  • A visual full-ring model combustion chamber with removable head structure

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Embodiment Construction

[0038] In order to clearly illustrate the technical characteristics of this patent, the following describes this patent in detail through specific implementation methods and in conjunction with the accompanying drawings.

[0039] The present invention as Figure 1-11 As shown, it includes an air intake casing, an oil inlet assembly, an annular head, a flame tube and an ignition assembly; the bottom of the air intake casing is provided with an air inlet, and the top is detachably connected with the annular head 27;

[0040] Described flame tube comprises inner flame tube 31 and the outer flame tube 29 that is made of transparent material, and described inner flame tube 31 and outer flame tube 29 all can be detachably connected on the top surface of annular head 27, and described inner The flame tube 31 is in the outer flame tube 29, and there is a distance between the two;

[0041]The annular head 27 is provided with several mounting holes 28 between the inner flame tube 31 an...

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Abstract

A visual full-ring model combustion chamber with a removable head structure. The invention relates to the field of aero-engine combustor structures. A visual full-ring model combustor with a short development period and low cost is proposed with a removable head structure. It includes an air intake casing, an oil inlet assembly, an annular head, a flame tube and an ignition assembly; the bottom of the air intake casing is provided with an air inlet, and the top is detachably connected to the annular head; the flame tube It includes an inner flame cylinder and an outer flame cylinder made of transparent material; a swirler is detachable in the installation hole; a nozzle is arranged in the swirler; the oil inlet assembly is arranged in the air intake casing , and is used to supply oil to several nozzles; the ignition assembly is fixedly connected to the flame cylinder, and the ignition assembly includes an ignition nozzle that passes through the outer flame cylinder. Through the ingenious design of the ring head, to replace different numbers of cyclones, only the corresponding ring head needs to be removed and installed. On the other hand, it is convenient to observe the whole field of view.

Description

technical field [0001] The invention relates to the field of aero-engine combustion chamber structures, in particular to a visual full-ring combustion chamber with a removable head structure. Background technique [0002] Internationally, NASA divides the research and development of combustor technology into multiple stages, including the proposal of the combustor design concept, the research and development of single-head combustors, the design of multi-head combustors, the full-ring and complete machine testing links, etc. Level 9, the test conditions, cycle, and funding required from low level to high level will increase by leaps and bounds. The single-head test piece has the characteristics of short cycle time, low test cost, convenient optical measurement, and easy determination of test parameters. It is often used as the object of preliminary test research and replacement research. The flame propagation characteristics under the flame interference state of one head, t...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F23R3/52
CPCF23R3/52
Inventor 金武汤朝伟李建中胡阁袁丽
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS