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A kind of internal combustion wave rotor with movable end cover and sealing method thereof

A technology of internal combustion wave rotor and mobile end, which is applied in the direction of gas turbine devices, machines/engines, jet propulsion devices, etc. It can solve the problems of rotor jamming, poor sealing effect between the end face and end cover of internal combustion wave rotors, etc., so as to ensure reliability , to avoid the rotor stuck, the effect of simple structure

Active Publication Date: 2018-05-04
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

[0004] Purpose of the invention: Based on the deficiencies of the prior art, the present invention provides a sealing method for the moving end cover of the internal combustion wave rotor, which is used to solve the poor sealing effect between the end face and the end cover of the internal combustion wave rotor and the technology that is likely to cause bad consequences of rotor jamming question

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  • A kind of internal combustion wave rotor with movable end cover and sealing method thereof
  • A kind of internal combustion wave rotor with movable end cover and sealing method thereof
  • A kind of internal combustion wave rotor with movable end cover and sealing method thereof

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Embodiment Construction

[0024] The present invention will be further explained below in conjunction with the drawings.

[0025] Aiming at the problem of internal combustion wave rotor leakage, the present invention proposes a mobile end cover sealing device and method. The specific implementation process is as follows:

[0026] It mainly includes the wave rotor 1, the fixed end cover 2 and the movable end cover 3. The wave rotor 1 includes the wave rotor main body 1a and the friction plate 1b. The wave rotor main body 1a channel is arranged at both ends of the wave rotor main body connecting flange 5, the friction plate 1b The friction plate connecting flange 4 is arranged on the periphery, the threaded holes 7 are evenly arranged on the wave rotor main body connecting flange 5, and the counterbore 6 corresponding to the threaded holes 7 is evenly arranged on the friction plate flange 4. The rotor body 1a and the friction plate 1b are connected to form an integral structure of the wave rotor 1, and the he...

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Abstract

The invention provides an internal combustion wave rotor with a movable end cover and a sealing method, and belongs to the technical field of aero-engine combustion chamber sealing. An internal combustion wave rotor movable end cover sealing device mainly comprises the wave rotor, a fixed end cover, the movable end cover and other structures. The fixed end cover and a positioning assembly arranged on the fixed end cover achieve a function of limiting the stroke of the movable end cover. Under the action of a spring on the positioning assembly, the movable end cover always makes contact with a friction piece on a wave rotor channel, and radial and circumferential sealing of the internal combustion wave rotor is achieved. Movement of the movable end cover can contain system heat expansion, and the effect that the rotor is not stuck is ensured. By adopting the internal combustion wave rotor movable end cover sealing device, the performance loss and the working instability caused by leakage in the working process of the internal combustion wave rotor can be greatly reduced; and meanwhile, the sealing method can be used for sealing of other rotating systems in the aviation field.

Description

Technical field [0001] The invention belongs to the field of aeroengines, in particular to a sealing method for a movable end cover of an internal combustion wave rotor. Background technique [0002] The internal combustion wave rotor is a new type of unsteady combustion device, which has the potential advantage of greatly improving the performance of the propulsion system. However, because the main part of the wave rotor is rotating during the working process, the leakage problem becomes its inherent technical obstacle. Moreover, its working process usually adopts the rapid pressurized combustion mode of knock or deflagration. The pressure generated during the combustion process is very high, which particularly highlights the impact of leakage. Data show that ABB's internal combustion wave rotor project was forced to terminate in the 1960s, and the impact of leakage is an important reason. [0003] From the above analysis, it can be known that in order to carry out research on th...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F02C3/14F02C7/28
CPCF02C3/14F02C7/28
Inventor 李建中巩二磊
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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