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    과수류, 또는 묘목에서 발생하는 파이토프토라속 균주를 검출하기 위한 중합효소연쇄반응의 프라이머, 이를 이용한 검출키트 및 방법
    3.
    发明公开
    과수류, 또는 묘목에서 발생하는 파이토프토라속 균주를 검출하기 위한 중합효소연쇄반응의 프라이머, 이를 이용한 검출키트 및 방법 有权
    用于检测水果种子或种子的种类的检测物质的聚合酶链反应的引物，以及检测试剂盒及其方法

    公开(公告)号：KR1020130100090A

    公开(公告)日：2013-09-09

    申请号：KR1020130103654

    申请日：2013-08-30

    Applicant: 충남대학교산학협력단

    Inventor： 김홍기 ,  송정영 ,  최유리 ,  나상권 ,  임현섭 ,  전낙범 ,  서문원 ,  장찬용 ,  이지현 ,  양슬기

    IPC: C12N15/11 ,  C12Q1/68

    CPC classification number: C12N15/11 ,  C12Q1/6851 ,  C12Q1/689

    Abstract: PURPOSE: A primer set for detecting Phytophthora sp. strains is provided to quickly and accurately detect and quantitate a very low concentration of the strains and to determine the kind of the strains. CONSTITUTION: An oligonucleotide has one base sequence among sequence numbers 22-26. A primer set for detecting Phytophthora siringae contains the nucleotide. A kit for detecting Phytophthora sp. strain contains the primer set and a reagent for polymerase chain reaction (PCR) or real-time PCR. A method for detecting Phytophthora sp. strain comprises the step of: isolating genome DNA from diseased plant tissues; performing PCR or real-time PCR using the DNA as a template; and amplifying and quantitating DAN fragments.

    Abstract translation: 目的：用于检测疫霉疫苗的引物组 提供菌株以快速且准确地检测和定量非常低浓度的菌株并确定菌株的种类。 构成：序列号22-26中的寡核苷酸具有一个碱基序列。 用于检测疫霉的引物组含有该核苷酸。 用于检测疫霉疫苗的试剂盒 菌株含有引物组和聚合酶链反应（PCR）或实时PCR的试剂。 一种检测疫霉疫霉的方法 菌株包括从病害植物组织分离基因组DNA的步骤; 使用DNA作为模板进行PCR或实时PCR; 并扩增和定量DAN片段。

    이원 추진제 로켓 엔진의 막냉각 장치 및 그 시험 방법
    4.
    发明公开
    이원 추진제 로켓 엔진의 막냉각 장치 및 그 시험 방법 无效
    BIPROPELLANT ROCKET发动机的薄膜冷却装置及其测试方法

    公开(公告)号：KR1020120080005A

    公开(公告)日：2012-07-16

    申请号：KR1020110001413

    申请日：2011-01-06

    Applicant: 충남대학교산학협력단

    Inventor： 고영성 ,  김선진 ,  이양석 ,  전준수 ,  김보연 ,  최유리

    IPC: F02K9/64 ,  F02K9/52 ,  F02K9/44

    CPC classification number: F02K9/64 ,  F02K9/44 ,  F02K9/52 ,  F02K9/96

    Abstract: PURPOSE: A film cooling apparatus of a bi-propellant rocket engine and a testing method thereof are provided to simplify a system using hydrogen peroxide instead of cooling agents. CONSTITUTION: A film cooling apparatus(300) of a bi-propellant rocket engine comprises a body unit(310) and a distributing unit(320). A front end of the body unit is connected to a rear part of an injector, and an inflow path is formed on a side part of the body unit. Cooling agents are flow through the inflow path. The front end of the distributing unit is connected to the rear part of the body unit, and one end of the distributing unit is connected to the other end of the inflow path. A plurality of distribution passages are formed in the other end of the distributing unit. The distribution passages are radially formed on a circumference of the distributing unit.

    Abstract translation: 目的：提供双推进剂火箭发动机的薄膜冷却装置及其测试方法，以简化使用过氧化氢代替冷却剂的系统。 构成：双推进剂火箭发动机的薄膜冷却装置（300）包括主体单元（310）和分配单元（320）。 主体单元的前端连接到喷射器的后部，并且流体通道形成在主体单元的侧部。 冷却剂流过流入路径。 分配单元的前端连接到主体单元的后部，并且分配单元的一端连接到流入路径的另一端。 多个分配通道形成在分配单元的另一端。 分配通道径向地形成在分配单元的圆周上。

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