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    Feasibility Study of Rotorcraft Fire Fighting for High-Rise Buildings

    Source: Journal of Aerospace Engineering:;2010:;Volume ( 023 ):;issue: 003
    Author:
    Erminio Zanenga
    ,
    Domenico Leonello
    ,
    Carlo L. Bottasso
    DOI: 10.1061/(ASCE)AS.1943-5525.0000021
    Publisher: American Society of Civil Engineers
    Abstract: Fire risk in high-rise buildings is of special concern to the fire community, since it is crucial but still technically extremely challenging to significantly improve the current fire fighting capabilities when a calamity happens above the “seven story limit.” In fact, at the moment, there is a lack of effective means for fire fighting in this rare but potentially deadly and costly accidents. To address this problem, in this work we provide a preliminary exploration of a new concept for fire suppression: the use of rotorcraft vehicles for aerial fire fighting in high-rise buildings. If available, such system could effectively support fire fighting efforts conducted with conventional means; moreover, it could provide for one of the very few alternatives to classic systems in certain critical cases such as postearthquake fires. At first, we analyze the operative context with the help of a few reference realistic scenarios which allow for the estimation of some key physical parameters. Next, we evaluate two alternative fire extinguishing technologies, and we identify in the water impulse cannon the solution which seems to be the most effective and compatible with the use on-board a rotorcraft for the scopes considered in this work. The analysis leads us to the identification of a target vehicle as a possible candidate platform for the development of a fire fighting helicopter. Finally, we propose a preliminary design of the fire fighting kit, and we evaluate the handling qualities of the vehicle during operations with reference to the ADS-33 normative.
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      Feasibility Study of Rotorcraft Fire Fighting for High-Rise Buildings

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    contributor authorErminio Zanenga
    contributor authorDomenico Leonello
    contributor authorCarlo L. Bottasso
    date accessioned2017-05-08T21:33:38Z
    date available2017-05-08T21:33:38Z
    date copyrightJuly 2010
    date issued2010
    identifier other%28asce%29as%2E1943-5525%2E0000021.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/56159
    description abstractFire risk in high-rise buildings is of special concern to the fire community, since it is crucial but still technically extremely challenging to significantly improve the current fire fighting capabilities when a calamity happens above the “seven story limit.” In fact, at the moment, there is a lack of effective means for fire fighting in this rare but potentially deadly and costly accidents. To address this problem, in this work we provide a preliminary exploration of a new concept for fire suppression: the use of rotorcraft vehicles for aerial fire fighting in high-rise buildings. If available, such system could effectively support fire fighting efforts conducted with conventional means; moreover, it could provide for one of the very few alternatives to classic systems in certain critical cases such as postearthquake fires. At first, we analyze the operative context with the help of a few reference realistic scenarios which allow for the estimation of some key physical parameters. Next, we evaluate two alternative fire extinguishing technologies, and we identify in the water impulse cannon the solution which seems to be the most effective and compatible with the use on-board a rotorcraft for the scopes considered in this work. The analysis leads us to the identification of a target vehicle as a possible candidate platform for the development of a fire fighting helicopter. Finally, we propose a preliminary design of the fire fighting kit, and we evaluate the handling qualities of the vehicle during operations with reference to the ADS-33 normative.
    publisherAmerican Society of Civil Engineers
    titleFeasibility Study of Rotorcraft Fire Fighting for High-Rise Buildings
    typeJournal Paper
    journal volume23
    journal issue3
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000021
    treeJournal of Aerospace Engineering:;2010:;Volume ( 023 ):;issue: 003
    contenttypeFulltext
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