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公开(公告)号：WO2013188722A1
公开(公告)日：2013-12-19
申请号：PCT/US2013/045765
申请日：2013-06-14
Applicant: UNITED TECHNOLOGIES CORPORATION , GKN AEROSPACE SWEDEN AB
Inventor： MOUNTZ, Daryl B. , KAPUSTKA, Theodore W. , LEVASSEUR, Glenn , BORG, Marcus , BERGLUND, Joakim , SVAHN, Anders , OCKBORN, Johan , PETTERSSON, Bengt
CPC classification number: F01D25/005 , F01D21/045 , F01D25/162 , F01D25/24 , F01D25/30 , F02C9/18 , F02K1/386 , F05D2220/32 , F05D2230/21 , F05D2230/232 , F05D2230/25 , F05D2230/54 , F05D2260/941 , F05D2300/175 , F05D2300/176 , F05D2300/177 , F05D2300/502
Abstract: A turbine exhaust case has an outer housing to be secured within a gas turbine engine and a central hub. Struts extend between the outer housing and the central hub. The struts are formed at least in part of a first material. The central hub is formed at least in part of a second material.
Abstract translation: 涡轮机排气箱具有固定在燃气涡轮发动机和中心毂内的外壳。 支柱在外壳和中心轮毂之间延伸。 支柱至少部分地由第一材料形成。 中心毂至少部分地由第二材料形成。
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Patent Agency Ranking
公开(公告)号：WO2013126471A1
公开(公告)日：2013-08-29
申请号：PCT/US2013/026969
申请日：2013-02-21
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： FARAH, Jorge I. , KAPUSTKA, Theodore W. , BURT, Jonathan P. , JAKIEL, Jonathan J. , STEWART, Dana P.
CPC classification number: F01D25/162 , B23K1/0018 , B23K2201/001 , F01D9/04 , F01D9/044 , F01D9/065 , F01D25/246 , F05D2230/237
Abstract: A static structure of a gas turbine engine includes a multiple of airfoil segments and at least one structural reinforcement ring mounted to the multiple of airfoil segments.
Abstract translation: 燃气涡轮发动机的静态结构包括多个翼型段和安装到多个翼型段的至少一个结构加强环。
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公开(公告)号：EP2817496B1
公开(公告)日：2017-07-05
申请号：EP13751563.1
申请日：2013-02-21
Applicant: United Technologies Corporation
Inventor： FARAH, Jorge I. , KAPUSTKA, Theodore W. , BURT, Jonathan P. , JAKIEL, Jonathan J. , STEWART, Dana P.
CPC classification number: F01D25/162 , B23K1/0018 , B23K2201/001 , F01D9/04 , F01D9/044 , F01D9/065 , F01D25/246 , F05D2230/237
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公开(公告)号：EP2861847B1
公开(公告)日：2020-03-25
申请号：EP13804715.4
申请日：2013-06-14
Applicant: United Technologies Corporation , GKN Aerospace Sweden AB
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公开(公告)号：EP2861847A1
公开(公告)日：2015-04-22
申请号：EP13804715.4
申请日：2013-06-14
Applicant: United Technologies Corporation , GKN Aerospace Sweden AB
Inventor： MOUNTZ, Daryl B. , KAPUSTKA, Theodore W. , LEVASSEUR, Glenn , BORG, Marcus , BERGLUND, Joakim , SVAHN, Anders , OCKBORN, Johan , PETTERSSON, Bengt
CPC classification number: F01D25/005 , F01D21/045 , F01D25/162 , F01D25/24 , F01D25/30 , F02C9/18 , F02K1/386 , F05D2220/32 , F05D2230/21 , F05D2230/232 , F05D2230/25 , F05D2230/54 , F05D2260/941 , F05D2300/175 , F05D2300/176 , F05D2300/177 , F05D2300/502
Abstract: A turbine exhaust case has an outer housing to be secured within a gas turbine engine and a central hub. Struts extend between the outer housing and the central hub. The struts are formed at least in part of a first material. The central hub is formed at least in part of a second material.
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6.发明公开TURBINE FRAME FAIRING FOR A GAS TURBINE ENGINE 有权TURBINENRAHMENVERKLEIDUNGFÜREINEN GASTURBINENMOTOR
公开(公告)号：EP2817496A1
公开(公告)日：2014-12-31
申请号：EP13751563.1
申请日：2013-02-21
Applicant: United Technologies Corporation
Inventor： FARAH, Jorge I. , KAPUSTKA, Theodore W. , BURT, Jonathan P. , JAKIEL, Jonathan J. , STEWART, Dana P.
CPC classification number: F01D25/162 , B23K1/0018 , B23K2201/001 , F01D9/04 , F01D9/044 , F01D9/065 , F01D25/246 , F05D2230/237
Abstract: A static structure of a gas turbine engine includes a multiple of airfoil segments and at least one structural reinforcement ring mounted to the multiple of airfoil segments.
Abstract translation: 燃气涡轮发动机的静态结构包括多个翼型段和至少一个安装到多个翼型段的结构加强环。
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