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    Development of a New Factor for Hot Gas Ingestion Through Rim Seal

    Source: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 007::page 72501
    Author:
    Liu, Dongdong
    ,
    Tao, Zhi
    ,
    Luo, Xiang
    ,
    Wu, Hongwei
    ,
    Yu, Xiao
    DOI: 10.1115/1.4031758
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This article presents a further investigation on the mechanism of hot gas ingestion by exploring the ingress with complicated cavity generated by the rotormounted cylinder protrusion. During the experiment, a cavity with 32 cylinder protrusions circumferentially distributed in rotor that contained 59 blades is applied. The annulus Reynolds number and rotating Reynolds number are fixed to be 1.77 أ— 105 and 7.42 أ— 105, respectively, while the dimensionless sealing air flow rate ranges from 3047 to 8310. The measurement of CO2 concentration and pressure is conducted. Experimental results show that the sealing efficiency is improved with the introduction of the cylinder protrusions even the static pressure inside cavity is found to be reduced. The effect of the circumferentially nonuniform cavity pressure wave is considered and added into the orifice model, and the effect of some impact factors, i.e., the amplitude, initial phase angle difference, and frequency of the cavity pressure wave, on hot gas ingestion is theoretically discussed in detail. However, it is noted that the cavity pressure wave that was introduced by 32 cylinder rotormounted protrusions is found to have insignificant effect on improving the sealing efficiency. In the present study, a modified orifice model that takes the tangential velocity into account is proposed and a new factor H is introduced to well explain the mechanism of the ingress.
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      Development of a New Factor for Hot Gas Ingestion Through Rim Seal

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    http://yetl.yabesh.ir/yetl1/handle/yetl/161098
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    contributor authorLiu, Dongdong
    contributor authorTao, Zhi
    contributor authorLuo, Xiang
    contributor authorWu, Hongwei
    contributor authorYu, Xiao
    date accessioned2017-05-09T01:28:31Z
    date available2017-05-09T01:28:31Z
    date issued2016
    identifier issn1528-8919
    identifier othergtp_138_07_072501.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/161098
    description abstractThis article presents a further investigation on the mechanism of hot gas ingestion by exploring the ingress with complicated cavity generated by the rotormounted cylinder protrusion. During the experiment, a cavity with 32 cylinder protrusions circumferentially distributed in rotor that contained 59 blades is applied. The annulus Reynolds number and rotating Reynolds number are fixed to be 1.77 أ— 105 and 7.42 أ— 105, respectively, while the dimensionless sealing air flow rate ranges from 3047 to 8310. The measurement of CO2 concentration and pressure is conducted. Experimental results show that the sealing efficiency is improved with the introduction of the cylinder protrusions even the static pressure inside cavity is found to be reduced. The effect of the circumferentially nonuniform cavity pressure wave is considered and added into the orifice model, and the effect of some impact factors, i.e., the amplitude, initial phase angle difference, and frequency of the cavity pressure wave, on hot gas ingestion is theoretically discussed in detail. However, it is noted that the cavity pressure wave that was introduced by 32 cylinder rotormounted protrusions is found to have insignificant effect on improving the sealing efficiency. In the present study, a modified orifice model that takes the tangential velocity into account is proposed and a new factor H is introduced to well explain the mechanism of the ingress.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDevelopment of a New Factor for Hot Gas Ingestion Through Rim Seal
    typeJournal Paper
    journal volume138
    journal issue7
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4031758
    journal fristpage72501
    journal lastpage72501
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 007
    contenttypeFulltext
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