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公开(公告)号：US10683761B1
公开(公告)日：2020-06-16
申请号：US15871392
申请日：2018-01-15
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： William R. Edwards , Stephen W. Milks , Steven J. Feigleson , Mark A. Stephens , Joseph C. Straccia
Abstract: A turbomachine airfoil element includes an airfoil that has pressure and suction sides spaced apart from one another in a thickness direction and joined to one another at leading and trailing edges. The airfoil extends in a radial direction a span that is in a range of 2.13-2.43 inch (54.2-61.8 mm). A chord length extends in a chordwise direction from the leading edge to the trailing edge at 50% span and is in a range of 3.56-3.86 inch (90.3-97.9 mm). The airfoil element includes at least one of a first mode with a frequency of 1049±10% Hz and a second mode with a frequency of 1271±10% Hz.
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公开(公告)号：US10767488B1
公开(公告)日：2020-09-08
申请号：US15871197
申请日：2018-01-15
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： William R. Edwards , Stephen W. Milks , Steven J. Feigleson , Mark A. Stephens , Joseph C. Straccia
Abstract: A turbomachine airfoil element includes an airfoil that has pressure and suction sides spaced apart from one another in a thickness direction and is joined to one another at leading and trailing edges. The airfoil extends in a radial direction a span that is in a range of 3.18-3.48 inch (80.7-88.4 mm). A chord length extends in a chordwise direction from the leading edge to the trailing edge at 50% span and is in a range of 1.17-1.47 inch (29.6-37.3 mm). The airfoil element includes at least two of a first mode with a frequency of 333±10% Hz, a second mode with a frequency of 1554±10% Hz, a third mode with a frequency of 2356±10% Hz, a fourth mode with a frequency of 2830±10% Hz, a fifth mode with a frequency of 4075±10% Hz and a sixth mode with a frequency of 5239±10% Hz.
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公开(公告)号：US10788049B1
公开(公告)日：2020-09-29
申请号：US15871347
申请日：2018-01-15
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： William R. Edwards , Stephen W. Milks , Steven J. Feigleson , Mark A. Stephens , Joseph C. Straccia
Abstract: A turbomachine airfoil element includes an airfoil that has pressure and suction sides spaced apart from one another in a thickness direction and joined to one another at leading and trailing edges. The airfoil extends in a radial direction a span that is in a range of 2.59-2.89 inch (65.7-73.3 mm). A chord length extends in a chordwise direction from the leading edge to the trailing edge at 50% span and is in a range of 1.46-1.76 inch (37.1-44.7 mm). The airfoil element includes at least two of a first mode with a frequency of 703±10% Hz, a second mode with a frequency of 3574±10% Hz, a third mode with a frequency of 8100±10% Hz, a fourth mode with a frequency of 9450±10% Hz, a fifth mode with a frequency of 11116±10% Hz and a sixth mode with a frequency of 11620±10% Hz.
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4.发明申请公开(公告)号：US20160108812A1
公开(公告)日：2016-04-21
申请号：US14855859
申请日：2015-09-16
Applicant: United Technologies Corporation
Inventor： Daniel S. Rogers , Stephen W. Milks , Steven J. Feigleson
CPC classification number: F02C7/06 , F01D25/246 , F02C3/04 , F02C7/20 , F05D2220/32 , F05D2240/50 , F05D2260/30 , F05D2260/36 , F05D2300/50212
Abstract: Conduits for guiding the motion of an inner diameter shroud of a low pressure compressor of a gas turbine engine are disclosed. The inner diameter shroud has at least three slots formed in one or more radially inwardly extending flanges. Each of the conduits are configured to assemble with a respective one of the at least three slots. Each conduit comprises a bushing having a first panel, and the first panel is capable of being inserted in a respective one of the slots of the inner diameter shroud. The conduit further comprises a bracket capable of being attached to a bearing support of a fan intermediate case of the gas turbine engine. The bushing is capable of being attached to the bracket. A contact between the first panel and the at least one slot of the inner diameter shroud restricts a circumferential rotation of the inner diameter shroud with respect to a central axis of the gas turbine engine when the first panel is inserted in the at least one slot, but allows a radial motion of the inner diameter shroud with respect to the central axis.
Abstract translation: 公开了用于引导燃气涡轮发动机的低压压缩机的内径护罩的运动的导管。 内径护罩具有形成在一个或多个径向向内延伸的凸缘中的至少三个槽。 每个导管被配置成与至少三个槽中的相应一个组合。 每个导管包括具有第一面板的衬套，并且第一面板能够插入内径护罩的相应的一个槽中。 导管还包括能够附接到燃气涡轮发动机的风扇中间壳体的轴承支撑件的支架。 套管能够连接到支架上。 第一面板和内径护罩的至少一个狭槽之间的接触限制当第一面板插入在至少一个狭槽中时，内径护罩相对于燃气涡轮发动机的中心轴线的周向旋转， 但允许内径护罩相对于中心轴线的径向运动。
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Patent Agency Ranking
公开(公告)号：US10794223B2
公开(公告)日：2020-10-06
申请号：US15840348
申请日：2017-12-13
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Daniel S. Rogers , Stephen W. Milks , Steven J. Feigleson
Abstract: A case assembly is provided. The case assembly comprises a first flange and a spot face in the first flange. The spot face has a D-shaped perimeter. A jacking insert is disposed in the spot face and has a D-shaped geometry. A threaded cylinder extends from the jacking insert into the first flange. A jacking insert is also provided. The jacking insert comprises a flat portion having a D-shaped geometry and a cylindrical portion having an internal thread configured to interface with a bolt.
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公开(公告)号：US10760447B1
公开(公告)日：2020-09-01
申请号：US15869312
申请日：2018-01-12
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： William R. Edwards , Stephen W. Milks , Steven J. Feigleson , Mark A. Stephens , Joseph C. Straccia
Abstract: A turbomachine airfoil element includes an airfoil that has pressure and suction sides spaced apart from one another in a thickness direction and joined to one another at leading and trailing edges. The airfoil extends in a radial direction a span that is in a range of 3.84-4.14 inch (97.5-105.1 mm). A chord length extends in a chordwise direction from the leading edge to the trailing edge at 50% span and is in a range of 1.16-1.46 inch (29.5-37.1 mm). The airfoil element includes at least two of a first mode with a frequency of 326±10% Hz, a second mode with a frequency of 1252±10% Hz, a third mode with a frequency of 2475±10% Hz, a fourth mode with a frequency of 2951±10% Hz, a fifth mode with a frequency of 4356±10% Hz and a sixth mode with a frequency of 6086±10% Hz.
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公开(公告)号：US10316749B2
公开(公告)日：2019-06-11
申请号：US14855859
申请日：2015-09-16
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Daniel S. Rogers , Stephen W. Milks , Steven J. Feigleson
Abstract: Conduits for guiding the motion of an inner diameter shroud of a low pressure compressor of a gas turbine engine are disclosed. The inner diameter shroud has at least three slots formed in one or more radially inwardly extending flanges. Each of the conduits are configured to assemble with a respective one of the at least three slots. Each conduit comprises a bushing having a first panel, and the first panel is capable of being inserted in a respective one of the slots of the inner diameter shroud. The conduit further comprises a bracket capable of being attached to a bearing support of a fan intermediate case of the gas turbine engine. The bushing is capable of being attached to the bracket. A contact between the first panel and the at least one slot of the inner diameter shroud restricts a circumferential rotation of the inner diameter shroud with respect to a central axis of the gas turbine engine when the first panel is inserted in the at least one slot, but allows a radial motion of the inner diameter shroud with respect to the central axis.
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公开(公告)号：US09879565B2
公开(公告)日：2018-01-30
申请号：US14600239
申请日：2015-01-20
Applicant: United Technologies Corporation
Inventor： Daniel S. Rogers , Stephen W. Milks , Steven J. Feigleson
CPC classification number: F01D25/243 , F01D9/042 , F01D25/246
Abstract: A case assembly is provided. The case assembly comprises a first flange and a spot face in the first flange. The spot face has a D-shaped perimeter. A jacking insert is disposed in the spot face and has a D-shaped geometry. A threaded cylinder extends from the jacking insert into the first flange. A jacking insert is also provided. The jacking insert comprises a flat portion having a D-shaped geometry and a cylindrical portion having an internal thread configured to interface with a bolt.
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公开(公告)号：US20160208652A1
公开(公告)日：2016-07-21
申请号：US14600239
申请日：2015-01-20
Applicant: United Technologies Corporation
Inventor： Daniel S. Rogers , Stephen W. Milks , Steven J. Feigleson
IPC: F01D25/24
CPC classification number: F01D25/243 , F01D9/042 , F01D25/246
Abstract: A case assembly is provided. The case assembly comprises a first flange and a spot face in the first flange. The spot face has a D-shaped perimeter. A jacking insert is disposed in the spot face and has a D-shaped geometry. A threaded cylinder extends from the jacking insert into the first flange. A jacking insert is also provided. The jacking insert comprises a flat portion having a D-shaped geometry and a cylindrical portion having an internal thread configured to interface with a bolt.
Abstract translation: 提供了一个壳体组件。 壳体组件包括第一凸缘和第一凸缘中的点面。 斑点具有D形周长。 顶针插入件设置在光斑面上并具有D形几何形状。 螺纹圆柱体从顶起插入件延伸到第一凸缘中。 还提供了顶升插入件。 顶起插入件包括具有D形几何形状的平坦部分和具有构造成与螺栓相接合的内螺纹的圆柱形部分。
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