Experimental study of research of centrifugal-compressor-radial-turbine type rotating detonation engine

Chikara Ishiyama, Koji Miyazaki, Soma Nakagami, Ken Matsuoka, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki

Research output: Chapter in Book/Report/Conference proceedingConference contribution

9 Citations (Scopus)

Abstract

Rotating detonation engines (RDEs) can get thrust or work by keeping detonation waves propagating in circumferential direction. Our objective is to apply rotating detonation engines (RDEs) to aircraft engines since we expect that the aircraft such as airplanes is to fly longer range by more simple structure. In this study, we designed a rotating detonation turbine engine (RDTE) with a single stage centrifugal compressor and a single stage radial flow turbine. The outer diameter of RDTE is about 200 mm. The revolution speed is 110000 rpm and rated air mass flow rate was 0.610 kg/s. We made two-parallel-plane rotating detonation combustor. We performed hot test with ethylene and oxygen. We analyzed several combustion modes with streak pictures and pressure time history. We observed the number of detonation waves, quenching and re-ignition phenomena by streak pictures.

Original languageEnglish
Title of host publication52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624104060
Publication statusPublished - 2016
Event52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016 - Salt Lake City, United States
Duration: 2016 Jul 252016 Jul 27

Other

Other52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
CountryUnited States
CitySalt Lake City
Period16/7/2516/7/27

Fingerprint

Centrifugal compressors
Detonation
Turbines
Engines
Aircraft
Radial flow
Aircraft engines
Combustors
Ignition
Quenching
Ethylene
Flow rate
Oxygen
Air

Keywords

  • Aircraft engine
  • Detonatin wave
  • Rotating detonation engine

ASJC Scopus subject areas

  • Engineering(all)

Cite this

Ishiyama, C., Miyazaki, K., Nakagami, S., Matsuoka, K., Kasahara, J., Matsuo, A., & Funaki, I. (2016). Experimental study of research of centrifugal-compressor-radial-turbine type rotating detonation engine. In 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016 American Institute of Aeronautics and Astronautics Inc, AIAA.

Experimental study of research of centrifugal-compressor-radial-turbine type rotating detonation engine. / Ishiyama, Chikara; Miyazaki, Koji; Nakagami, Soma; Matsuoka, Ken; Kasahara, Jiro; Matsuo, Akiko; Funaki, Ikkoh.

52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016. American Institute of Aeronautics and Astronautics Inc, AIAA, 2016.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Ishiyama, C, Miyazaki, K, Nakagami, S, Matsuoka, K, Kasahara, J, Matsuo, A & Funaki, I 2016, Experimental study of research of centrifugal-compressor-radial-turbine type rotating detonation engine. in 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016. American Institute of Aeronautics and Astronautics Inc, AIAA, 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016, Salt Lake City, United States, 16/7/25.
Ishiyama C, Miyazaki K, Nakagami S, Matsuoka K, Kasahara J, Matsuo A et al. Experimental study of research of centrifugal-compressor-radial-turbine type rotating detonation engine. In 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016. American Institute of Aeronautics and Astronautics Inc, AIAA. 2016
Ishiyama, Chikara ; Miyazaki, Koji ; Nakagami, Soma ; Matsuoka, Ken ; Kasahara, Jiro ; Matsuo, Akiko ; Funaki, Ikkoh. / Experimental study of research of centrifugal-compressor-radial-turbine type rotating detonation engine. 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016. American Institute of Aeronautics and Astronautics Inc, AIAA, 2016.
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