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Trapped Vortex Combustion Chamber: Design and Experimental Investigations Using Hydrogen as Fuel

Kulshreshtha, D. B. / Channiwala, S. A.

Abstract The design of trapped vortex combustion chamber was undertaken as a part of ongoing research on micro combustion chamber using hydrogen as fuel. The reacting experimental studies were then carried out on the designed chamber. The fuel was injected directly into the cavity. The combustion was first initiated in the cavity with 3 % of the main flow air supplied in reverse direction to the fuel flow. The combustion in cavity was of rich type. Temperature levels in the range of 900 K were encountered in the cavity. Thereafter, diffusion combustion was initiated using the flame generated in the cavity. The temperature levels in this stage were in the range of 1,800 K. The overall pressure drop for a trapped vortex combustor was less than 5 % at all operating parameters.

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Trapped Vortex Combustion Chamber: Design and Experimental Investigations Using Hydrogen as Fuel

Kulshreshtha, D. B. / Channiwala, S. A.

Abstract The design of trapped vortex combustion chamber was undertaken as a part of ongoing research on micro combustion chamber using hydrogen as fuel. The reacting experimental studies were then carried out on the designed chamber. The fuel was injected directly into the cavity. The combustion was first initiated in the cavity with 3 % of the main flow air supplied in reverse direction to the fuel flow. The combustion in cavity was of rich type. Temperature levels in the range of 900 K were encountered in the cavity. Thereafter, diffusion combustion was initiated using the flame generated in the cavity. The temperature levels in this stage were in the range of 1,800 K. The overall pressure drop for a trapped vortex combustor was less than 5 % at all operating parameters.

Trapped Vortex Combustion Chamber: Design and Experimental Investigations Using Hydrogen as Fuel

Kulshreshtha, D. B. / Channiwala, S. A.

Abstract The design of trapped vortex combustion chamber was undertaken as a part of ongoing research on micro combustion chamber using hydrogen as fuel. The reacting experimental studies were then carried out on the designed chamber. The fuel was injected directly into the cavity. The combustion was first initiated in the cavity with 3 % of the main flow air supplied in reverse direction to the fuel flow. The combustion in cavity was of rich type. Temperature levels in the range of 900 K were encountered in the cavity. Thereafter, diffusion combustion was initiated using the flame generated in the cavity. The temperature levels in this stage were in the range of 1,800 K. The overall pressure drop for a trapped vortex combustor was less than 5 % at all operating parameters.

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Title:

Trapped Vortex Combustion Chamber: Design and Experimental Investigations Using Hydrogen as Fuel

Contributors:

Kulshreshtha, D. B. (author) / Channiwala, S. A. (author)

Published in:

Journal of The Institution of Engineers (India): Series C ; 95 ; 69-75

Publication date:

2014-01-01

Size:

7 pages

ISSN:

2250-0553 , 2250-0545

DOI:

https://doi.org/10.1007/s40032-014-0102-8

Type of media:

Article (Journal)

Type of material:

Electronic Resource

Language:

English

Keywords:

Trapped vortex combustion chamber , Hydrogen fuel Engineering , Aerospace Technology and Astronautics , Mechanical Engineering , Industrial and Production Engineering

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