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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
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국제특허분류(IPC7판) |
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출원번호 | US-0014298 (2008-01-15) |
등록번호 | US-8469656 (2013-06-25) |
발명자 / 주소 |
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출원인 / 주소 |
|
인용정보 | 피인용 횟수 : 1 인용 특허 : 21 |
A turbine airfoil seal system of a turbine engine having a seal base with a plurality of seal strips extending therefrom for sealing gaps between rotational airfoils and adjacent stationary components. The seal strips may overlap each other and may be generally aligned with each other. The seal stri
1. An airfoil seal system for airfoils of a gas turbine engine, comprising: a seal base configured to be received within a channel of a rotational airfoil proximate to a platform extending from the airfoil, wherein the seal base is generally an arcuate segment and wherein the seal base is configured
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