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公开(公告)号：US20170198590A1
公开(公告)日：2017-07-13
申请号：US14992672
申请日：2016-01-11
Applicant: United Technologies Corporation
Inventor： Jesse C. Meyer , Joseph Jalowka , John D. Riehl , Raymond P. Martina , James O. Hansen
CPC classification number: F01D5/282 , B32B15/043 , B32B2255/06 , B32B2255/26 , B32B2603/00 , C09J5/02 , C09J5/04 , C09J5/06 , C09J2201/36 , C09J2463/00 , C22C21/00 , F05D2300/603
Abstract: The present disclosure provides methods and systems for the bonding of dissimilar substrates. For example, a first substrate may be coupled to a second substrate by a composite joint between the first substrate and the second substrate. The composite joint may be comprised of a first adhesive material and a second adhesive material. The first adhesive material may be disposed on the first substrate, and the second adhesive material may be disposed to the first adhesive material. The composite joint between the first substrate and the second substrate may provide an isolation layer therebetween, preventing galvanic corrosion.
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公开(公告)号：US10221700B2
公开(公告)日：2019-03-05
申请号：US14992672
申请日：2016-01-11
Applicant: United Technologies Corporation
Inventor： Jesse C. Meyer , Joseph Jalowka , John D. Riehl , Raymond P. Martina , James O. Hansen
Abstract: The present disclosure provides methods and systems for the bonding of dissimilar substrates. For example, a first substrate may be coupled to a second substrate by a composite joint between the first substrate and the second substrate. The composite joint may be comprised of a first adhesive material and a second adhesive material. The first adhesive material may be disposed on the first substrate, and the second adhesive material may be disposed to the first adhesive material. The composite joint between the first substrate and the second substrate may provide an isolation layer therebetween, preventing galvanic corrosion.
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公开(公告)号：US20170023010A1
公开(公告)日：2017-01-26
申请号：US15039929
申请日：2014-11-25
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Lee Drozdenko , James O. Hansen , Jesse C. Meyer , Maria C. Kirejczyk , Scot A. Webb , Brandon A. Gates , Richard B. Bergethon
CPC classification number: F04D29/388 , B32B5/024 , B32B7/12 , B32B15/14 , B32B15/20 , B32B2262/101 , B32B2603/00 , F01D5/12 , F01D5/14 , F01D5/147 , F01D5/28 , F01D5/282 , F01D5/286 , F01D5/288 , F04D29/023 , F04D29/325 , F05D2220/36 , F05D2240/303 , F05D2300/121 , F05D2300/133 , F05D2300/6012
Abstract: A blade comprises an airfoil extending from a trailing edge to a leading edge. The airfoil includes a body formed of an aluminum containing material. A sheath is at the leading edge and is formed of a titanium containing material. A sandwich is positioned intermediate the sheath and the airfoil body, the sandwich including an outer adhesive layer adjacent the sheath, an intermediate fabric layer and an inner adhesive layer adjacent the body. A gas turbine engine is also disclosed.
Abstract translation: 叶片包括从后缘延伸到前缘的翼型件。 翼型件包括由含铝材料形成的主体。 护套位于前缘，由含钛材料形成。 三明治位于护套和翼型体之间，夹层包括邻近护套的外部粘合剂层，中间织物层和邻近身体的内部粘合剂层。 还公开了一种燃气涡轮发动机。
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公开(公告)号：US10458428B2
公开(公告)日：2019-10-29
申请号：US14917476
申请日：2014-08-04
Applicant: United Technologies Corporation
Inventor： Lee M. Drozdenko , James O. Hansen , Jesse C. Meyer , John J. Marcin, Jr. , Robert M. Shemenski , Scot A. Webb , Brandon A. Gates , Michael A. Morden
Abstract: An airfoil member (100) comprising has a substrate (120) along at least a portion of an airfoil (102) of the airfoil member. A sheath (122) has a channel (144) receiving a portion (160) of the substrate. A plurality of separate spacers (320; 380; 400) are between the sheath and the substrate and have a plurality of gaps between the spacers.
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公开(公告)号：US20160215784A1
公开(公告)日：2016-07-28
申请号：US14917485
申请日：2014-08-04
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Lee M. Drozdenko , James O. Hansen , Maria C. Kirejczyk , Scot A. Webb , Jesse C. Meyer , Brandon A. Gates , Richard B. Bergethon , Michael A. Morden
CPC classification number: F04D29/023 , F01D5/288 , F04D29/324 , F04D29/325 , F04D29/388 , F04D29/644 , F05D2240/303 , F05D2300/173 , F05D2300/174 , F05D2300/6033
Abstract: An airfoil member (100) comprising has a substrate (120) along at least a portion of an airfoil (102) of the airfoil member. A sheath (122) has a channel (144) receiving a portion (160) of the substrate. A scrim (200) is between the substrate and the sheath. A spacer (220) is between the sheath and the substrate and has a plurality of spaced-apart portions (232, 234) with gaps between the spaced-apart portions.
Abstract translation: 翼型件（100）包括沿翼型件的翼型（102）的至少一部分具有基底（120）。 护套（122）具有容纳衬底的一部分（160）的通道（144）。 稀松布（200）在基材和护套之间。 间隔物（220）位于护套和衬底之间并且具有多个间隔开的部分（232,234），其间隔开间隔开的部分。
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Patent Agency Ranking
公开(公告)号：US20160201482A1
公开(公告)日：2016-07-14
申请号：US14915964
申请日：2014-09-02
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Joseph Parkos, Jr. , James O. Hansen , Jesse C. Meyer
CPC classification number: F01D5/286 , C23F1/00 , F01D5/28 , F01D5/288 , F04D29/324 , F05D2220/32 , F05D2220/36 , F05D2230/20 , F05D2240/30 , F05D2240/303 , F05D2240/305 , F05D2240/306 , F05D2300/121 , F05D2300/133 , Y02T50/672 , Y02T50/673
Abstract: An airfoil includes an aluminum airfoil body with a pressure side, suction side, leading edge and trailing edge; and a titanium foil layer covering at least part of one of the pressure side and the suction side.
Abstract translation: 机翼包括具有压力侧的铝翼型本体，吸力侧，前缘和后缘; 以及覆盖压力侧和吸入侧中的一方的至少一部分的钛箔层。
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公开(公告)号：US11156104B2
公开(公告)日：2021-10-26
申请号：US16255976
申请日：2019-01-24
Applicant: United Technologies Corporation
Inventor： Jesse C. Meyer , Joseph Jalowka , John D. Riehl , Raymond P. Martina , James O. Hansen
Abstract: The present disclosure provides methods and systems for the bonding of dissimilar substrates. For example, a first substrate may be coupled to a second substrate by a composite joint between the first substrate and the second substrate. The composite joint may be comprised of a first adhesive material and a second adhesive material. The first adhesive material may be disposed on the first substrate, and the second adhesive material may be disposed to the first adhesive material. The composite joint between the first substrate and the second substrate may provide an isolation layer therebetween, preventing galvanic corrosion.
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公开(公告)号：US10982683B2
公开(公告)日：2021-04-20
申请号：US15039929
申请日：2014-11-25
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Lee Drozdenko , James O. Hansen , Jesse C. Meyer , Maria C. Kirejczyk , Scot A. Webb , Brandon A. Gates , Richard B. Bergethon
IPC: F04D29/38 , B32B7/12 , F01D5/28 , F01D5/14 , F01D5/12 , B32B5/02 , B32B15/14 , B32B15/20 , F04D29/02 , F04D29/32
Abstract: A blade comprises an airfoil extending from a trailing edge to a leading edge. The airfoil includes a body formed of an aluminum containing material. A sheath is at the leading edge and is formed of a titanium containing material. A sandwich is positioned intermediate the sheath and the airfoil body, the sandwich including an outer adhesive layer adjacent the sheath, an intermediate fabric layer and an inner adhesive layer adjacent the body. A gas turbine engine is also disclosed.
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公开(公告)号：US20190153878A1
公开(公告)日：2019-05-23
申请号：US16255976
申请日：2019-01-24
Applicant: United Technologies Corporation
Inventor： Jesse C. Meyer , Joseph Jalowka , John D. Riehl , Raymond P. Martina , James O. Hansen
Abstract: The present disclosure provides methods and systems for the bonding of dissimilar substrates. For example, a first substrate may be coupled to a second substrate by a composite joint between the first substrate and the second substrate. The composite joint may be comprised of a first adhesive material and a second adhesive material. The first adhesive material may be disposed on the first substrate, and the second adhesive material may be disposed to the first adhesive material. The composite joint between the first substrate and the second substrate may provide an isolation layer therebetween, preventing galvanic corrosion.
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公开(公告)号：US10106712B2
公开(公告)日：2018-10-23
申请号：US15106044
申请日：2014-11-12
Applicant: United Technologies Corporation
Inventor： John H. Vontell , Jesse C. Meyer , Charles R. Watson
IPC: C09J183/04 , C09J5/02 , C08G77/20
Abstract: A method of adhering a first structure to a second structure using a primer, containing a primer fugitive inhibitor, and a film adhesive by removing the primer fugitive inhibitor under vacuum at room temperature conditions.
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