基本信息:
- 专利标题： 굴곡진 가스 터빈 엔진 구성요소 상의 써모커플
- 专利标题（英）：A thermocouple on a contoured gas turbine engine component
- 专利标题（中）：一个轮廓燃气涡轮发动机部件上的热电偶
- 申请号：KR1020137027076 申请日：2012-03-13
- 公开(公告)号：KR1020130133292A 公开(公告)日：2013-12-06
- 发明人： 서브라마니안,라메쉬 , 쿨카르니,애넌드에이. , 쉬한,케빈씨.
- 申请人： 지멘스 에너지, 인코포레이티드
- 申请人地址： **** Alafaya Trail, Orlando, FL *****-****, U.S.A.
- 专利权人： 지멘스 에너지, 인코포레이티드
- 当前专利权人： 지멘스 에너지, 인코포레이티드
- 当前专利权人地址： **** Alafaya Trail, Orlando, FL *****-****, U.S.A.
- 代理人： 특허법인 남앤드남; 정현주; 이시용
- 优先权： US13/417,448 2012-03-12; US61/452,735 2011-03-15
- 国际申请： PCT/US2012/028858 2012-03-13
- 国际公布： WO2012145095 2012-10-26
- 主分类号： G01K1/14
- IPC分类号： G01K1/14 ; G01K7/02 ; F01D17/08 ; G01K11/12
To form a first material phase, the pattern 50 on the component 10 to stack on the component (10) to a method of forming, forming a first leg 14 of the thermocouple 12 a step of laminating the second material through the mask 30, the pattern 50 is first that contains separate lead ends of the plurality of separate second leg junction end 20 and the second leg (16) 2 and form a continuous patch 52 of material, each of the second legs junction end 20 is in the range of up to a continuous patch 52 from the respective intersections (18) with a first leg 14, the depositing a second material, and the second leg (16) separate from the lead end portion (22) comprising: a laser to remove the continuous patch 52 to form, respectively, of the lead end 22 is each intersection of It is electrically connected to the end 20, so that by forming a separate second leg 16, and a step of removing the laser continuous patch 52.
公开/授权文献:
- KR101599789B1 굴곡진 가스 터빈 엔진 구성요소 상의 써모커플 公开/授权日：2016-03-07
信息查询:
EspacenetIPC结构图谱:
| G | 物理 |
| --G01 | 测量；测试 |
| ----G01K | 温度测量；热量测量；未列入其他类目的热敏元件 |
| ------G01K1/00 | 非专用于特殊类型温度计的零部件 |
| --------G01K1/14 | .支撑；固定装置；在特殊位置安装温度计 |