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Development of Pulse Detonation Engine Initiator Using Conic Shape Reflector for Large Bore and High thrust Combustor

Research Project

Project/Area Number 21760646
Research Category

Grant-in-Aid for Young Scientists (B)

Allocation TypeSingle-year Grants
Research Field Aerospace engineering
Research InstitutionHokkaido University

Principal Investigator

WAKITA Masashi  北海道大学, 大学院・工学研究院, 助教 (80451441)

Project Period (FY) 2009 – 2011
Project Status Completed (Fiscal Year 2011)
Budget Amount *help
¥4,420,000 (Direct Cost: ¥3,400,000、Indirect Cost: ¥1,020,000)
Fiscal Year 2011: ¥910,000 (Direct Cost: ¥700,000、Indirect Cost: ¥210,000)
Fiscal Year 2010: ¥2,080,000 (Direct Cost: ¥1,600,000、Indirect Cost: ¥480,000)
Fiscal Year 2009: ¥1,430,000 (Direct Cost: ¥1,100,000、Indirect Cost: ¥330,000)
Keywordsパルスデトネーションエンジン / デトネーション / 円錐形状反射板 / 超音速燃焼 / デトネーションの伝播 / 水素-空気混合気 / ドライバーガス過供給
Research Abstract

To develop a pulse detonation engine(PDE) with large diameter and small L/D, a new PDE initiator using a conic shape reflector have been proposed. The promotion effect of the transition of detonation wave obtained by the conical body of 15°is extremely high. This is because transverse waves in a detonation wave can reach the sidewall of the conical body, when the conical angle is sufficiently smaller than the angle of the triple point trajectory of the detonation wave. The large diameter cylindrical combustor experiments reveal that the necessary overfilling radius of the driver gas mixture is more than 100 mm to initiate the detonation wave, and this radius is less than 1% of the driver gas usage rate over the whole section of the PDE system.

Report

(4 results)
  • 2011 Annual Research Report   Final Research Report ( PDF )
  • 2010 Annual Research Report
  • 2009 Annual Research Report
  • Research Products

    (18 results)

All 2012 2011 2010 2009

All Journal Article (4 results) (of which Peer Reviewed: 2 results) Presentation (14 results)

  • [Journal Article] Development of Pulse Detonation Engine Initiator Using Reflector for Large Bore Combustor2012

    • Author(s)
      Masashi WAKITA, Masayoshi TAMURA, Akihiro TERASAKA, Kazuya SAJIKI, Tsuyoshi TOTANI and Harunori NAGATA
    • Journal Title

      TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN

      Volume: Vol.10, No.ists28 Pages: 31-36

    • NAID

      130002137028

    • Related Report
      2011 Final Research Report
  • [Journal Article] Development of Pulse Detonation Engine Initiator Using Reflector for Large Bore Combustor2012

    • Author(s)
      Masashi Wakita
    • Journal Title

      TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN

      Volume: 10 Issue: ists28 Pages: Pa_31-Pa_36

    • DOI

      10.2322/tastj.10.Pa_31

    • NAID

      130002137028

    • ISSN
      1884-0485
    • Related Report
      2011 Annual Research Report
    • Peer Reviewed
  • [Journal Article] Driver Gas Reduction Effect of Pulse-Detonation-Engine Initiator Using Reflecting Board2011

    • Author(s)
      Masashi Wakita, Ryusuke Numakura, Takatoshi Asada, Masayoshi Tamura, Tsuyoshi Totani and Harunori Nagata
    • Journal Title

      Journal of Propulsion and Power

      Volume: Vol.27, No.1 Pages: 162-170

    • Related Report
      2011 Final Research Report
  • [Journal Article] Driver Gas Reduction Effect of Pulse-Detonation-Engine Initiator Using Reflecting Boar2011

    • Author(s)
      Masashi Wakita
    • Journal Title

      JOURNAL OF PROPULSION AND POWER

      Volume: 27 Pages: 162-170

    • Related Report
      2010 Annual Research Report
    • Peer Reviewed
  • [Presentation] Development effort of pulse detonation engine initiator using reflector at Hokkaido university2011

    • Author(s)
      Masashi Wakita
    • Organizer
      International Workshop on Detonation for Propulsion 2011
    • Place of Presentation
      パラダイスホテル,(釜山,韓国)(招待講演)
    • Year and Date
      2011-11-15
    • Related Report
      2011 Annual Research Report
  • [Presentation] Planar toroidal detonation propagation through gradual expanding channel2011

    • Author(s)
      Masashi Wakita
    • Organizer
      23rd International Colloquium on Dynamics of Explosion and Reactive Systems (23rd ICDERS)
    • Place of Presentation
      カリフォルニア大学アーバイン校,(アーバイン,米国)
    • Year and Date
      2011-07-18
    • Related Report
      2011 Annual Research Report
  • [Presentation] 大口径平板燃焼器を伝播する円筒デトネーション波に関する研究2011

    • Author(s)
      桟敷和弥
    • Organizer
      第43回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム
    • Place of Presentation
      早稲田大学,(東京都)
    • Year and Date
      2011-07-07
    • Related Report
      2011 Annual Research Report
  • [Presentation] Development of Pulse Detonation Engine Initiator using Reflector for Large Bore Combustor2011

    • Author(s)
      Masashi Wakita
    • Organizer
      28th International Symposium on Space Technology and Science (ISTS)
    • Place of Presentation
      沖縄コンベンションセンター,(宜野湾市)
    • Year and Date
      2011-06-11
    • Related Report
      2011 Annual Research Report
  • [Presentation] Development effort of pulse detonation engine initiator using reflector at Hokkaido university2011

    • Author(s)
      Masashi Wakita
    • Organizer
      International Workshop on Detonation for Propulsion 2011
    • Place of Presentation
      Paradise Hotel, Busan, Korea
    • Related Report
      2011 Final Research Report
  • [Presentation] Planar toroidal detonation propagation through gradual expanding channel2011

    • Author(s)
      Masashi Wakita, Masayoshi Tamura, Akihiro Terasaka, Kazuya Sajiki, Tsuyoshi Totani and Harunori Nagata
    • Organizer
      Proc. 23rd International Colloquium on Dynamics of Explosion and Reactive Systems(23rd ICDERS)
    • Place of Presentation
      Irvine, USA
    • Related Report
      2011 Final Research Report
  • [Presentation] Development of Pulse Detonation Engine Initiator using Reflector for Large Bore Combustor2011

    • Author(s)
      Masashi Wakita, Masayosi Tamura, Akihiro Terasaka, Kazuya Sajiki, Tsuyoshi Totani and Harunori Nagata
    • Organizer
      Proc. 28th International Symposium on Space Technology and Science(ISTS)
    • Place of Presentation
      Naha, Japan
    • Related Report
      2011 Final Research Report
  • [Presentation] 流路幅とセルサイズが円環デトネーション波から平面デトネーション波への遷移過程に与える影響2010

    • Author(s)
      田村正佳
    • Organizer
      第49回燃焼シンポジウム
    • Place of Presentation
      福岡ガーデンパレス 福岡
    • Year and Date
      2010-12-03
    • Related Report
      2010 Annual Research Report
  • [Presentation] Effects of flow passage shape around reflector on detonation transition2010

    • Author(s)
      Masashi Wakita
    • Organizer
      Eighth International Symposium on Hazards, Prevention, and Mitigation of Industrial Explosions
    • Place of Presentation
      慶應義塾大学 日吉キャンパス 横浜
    • Year and Date
      2010-09-07
    • Related Report
      2010 Annual Research Report
  • [Presentation] 流路幅と流路傾斜角が円環デトネーション波の伝播に与える影響2010

    • Author(s)
      寺坂昭宏
    • Organizer
      第42回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2010
    • Place of Presentation
      米子コンベンションセンターBiG ShiP、米子
    • Year and Date
      2010-06-24
    • Related Report
      2010 Annual Research Report
  • [Presentation] Effects of flow passage shape around reflector on detonetion transition2010

    • Author(s)
      Masashi Wakita, Masayoshi Tamura, Akihiro Terasaka, Tsuyoshi Totani and Harunori Nagata
    • Organizer
      Proc. 8th International Sympoium on Hazards, Prevention, and Mitigation of Industrial Explosions(8th ISHPMIE)
    • Place of Presentation
      Yokohama, Japan
    • Related Report
      2011 Final Research Report
  • [Presentation] 拡大する流路内を伝播する円環デトネーション波の挙動2009

    • Author(s)
      田村正佳
    • Organizer
      第47回燃焼シンポジウム
    • Place of Presentation
      札幌コンベンションセンター(札幌)
    • Year and Date
      2009-12-02
    • Related Report
      2009 Annual Research Report
  • [Presentation] PDE燃焼器内の円環流路部を通過するデトネーション波の伝播挙動2009

    • Author(s)
      脇田督司
    • Organizer
      第53回宇宙科学技術連合講演会
    • Place of Presentation
      京都大学 吉田南構内(京都)
    • Year and Date
      2009-09-10
    • Related Report
      2009 Annual Research Report
  • [Presentation] 環状流路を有するPDEイニシエーター内のデトネーション波の挙動2009

    • Author(s)
      田村正佳
    • Organizer
      第41回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2009
    • Place of Presentation
      JAXA調布航空宇宙センター(調布)
    • Year and Date
      2009-06-19
    • Related Report
      2009 Annual Research Report

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Published: 2009-04-01   Modified: 2016-04-21  

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