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1. 发明授权

KR101363975B1 버너 결합구조를 구비하는 마이크로 가스터빈 및 그 조립방법 失效
标题翻译：微型燃气轮机，包括燃烧器组合结构及其组装方法
公开(公告)号：KR101363975B1
公开(公告)日：2014-02-18
申请号：KR1020120133031
申请日：2012-11-22
申请人： 에스티엑스중공업 주식회사
发明人： 박필제 , 박재석 , 김종훈 , 우타관
IPC分类号： F02C3/14 , F02C7/00 , F23R3/42
摘要： The present invention relates to a micro gas turbine having a burner joining structure and an assembling method thereof and more specifically, to a micro gas turbine having a burner joining structure and an assembling method thereof which prevents a decrease in the efficiency of the micro gas turbine by preventing a leakage of mixed gas of compressed air and fuel as the airtightness between a liner and a burner guide is maintained by screw-joining the burner guide and a joining member by forming the joining screw on one side of the outer circumference of the burner guide and rotating a burner assembly after mounting the joining member having a screw corresponding to the joining screw on the liner. The present invention includes a burner; the burner guide which is joined to the burner and which includes the joining screw on the outer circumference of the end; and the joining member which is mounted on the liner of a combustor and which includes the screw corresponding to the joining screw on the inner circumference.
摘要翻译：本发明涉及具有燃烧器接合结构及其组装方法的微型燃气轮机，更具体地说，涉及一种具有燃烧器接合结构的微型燃气轮机及其组装方法，其防止微型燃气轮机的效率降低通过在燃烧器的外周的一侧形成接合螺钉，通过将燃烧器引导件和接合部件螺接连接来防止压缩空气和燃料的混合气体的泄漏，因为衬套和燃烧器引导件之间的气密性在将具有对应于接合螺钉的螺钉的接合构件安装在衬套上之后引导和旋转燃烧器组件。本发明包括燃烧器; 燃烧器引导件，其连接到燃烧器并且包括在端部的外周上的接合螺钉; 以及安装在燃烧器的衬套上并且包括对应于内圆周上的接合螺钉的螺钉的接合构件。

2. 发明授权

KR101265883B1 점화기 결합구조를 구비하는 마이크로 가스터빈 및 그 조립방법 失效
标题翻译：微型气体涡轮机，包括点火器组合结构及其组装方法
公开(公告)号：KR101265883B1
公开(公告)日：2013-05-20
申请号：KR1020120133033
申请日：2012-11-22
申请人： 에스티엑스중공업 주식회사
发明人： 박정민 , 박재석 , 이상민 , 우타관
IPC分类号： F02C7/264 , F02C3/14 , F02C7/00
CPC分类号： F02C7/20 , F02C3/14 , F02C7/26 , F02C7/264 , F05D2250/82 , F23C2900/03001 , F23R2900/00001 , F23R2900/00012 , Y10T29/4932
摘要： PURPOSE: A micro gas turbine having a structure for coupling an igniter and an assembling method thereof are provided to thread-couple an igniter flange and a coupling member by rotating an igniter assembly in order to seal a gap between a liner casing and the igniter flange, thereby preventing the leakage of mixture gas of compressed air and fuel. CONSTITUTION: A micro gas turbine having a structure for coupling an igniter includes an igniter(121), an igniter flange(122), a coupling member(124), and a bellows(140). The coupling member has a first part(124a) inserted inside a liner casing and a second part(124b) curved against the first part and mounted on the liner casing. The bellows is stuck to the second part. The igniter is coupled to one side of the igniter flange. A circumferential groove(128) is formed on the other side of the igniter flange so that a space part can be formed between the igniter flange and the coupling member.
摘要翻译：目的：提供具有用于联接点火器的结构的微型燃气涡轮机及其组装方法，以通过旋转点火器组件来使点火器凸缘和联接构件螺纹连接，以便密封衬套和点火器凸缘之间的间隙，从而防止压缩空气和燃料的混合气体的泄漏。构造：具有用于联接点火器的结构的微型燃气轮机包括点火器（121），点火器法兰（122），联接构件（124）和波纹管（140）。联接构件具有插入衬套内部的第一部分（124a）和与第一部分弯曲并安装在衬套上的第二部分（124b）。波纹管卡在第二部分。点火器联接到点火器法兰的一侧。在点火器凸缘的另一侧上形成周向槽（128），使得可以在点火器凸缘和联接构件之间形成空间部分。

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