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公开(公告)号:US11840986B2
公开(公告)日:2023-12-12
申请号:US16857487
申请日:2020-04-24
Applicant: The Boeing Company
Inventor: Kevin O'Brien Gaw , Dylan E. Jones , Michael H. Larson , Belur N. Shivashankara , Randy J. Grove , David John Barene , Jeston Lingelbach , Kory Shaffer , David W. Foutch
IPC: F02K1/62 , F02K1/70 , B29C43/18 , B29C65/02 , B29C65/48 , B29C65/00 , B29K101/12 , F02K1/72 , B29L31/00
CPC classification number: F02K1/70 , B29C43/18 , B29C65/02 , B29C65/48 , B29C66/7254 , B29C2043/189 , B29K2101/12 , B29L2031/7504 , F02K1/625 , F02K1/72 , F05D2220/32 , F05D2230/23 , F05D2230/60 , F05D2250/283 , F05D2260/96 , F05D2300/43 , F05D2300/432 , F05D2300/433 , F05D2300/434 , F05D2300/436
Abstract: A blocker door assembly for use in a gas turbine includes a panel, a core integrally formed with the panel, and a plurality of mounting structures extending from at least one of the panel and the core. The plurality of mounting structures are integrally formed with the core and the panel such that the panel, the core, and the mounting structures are co-molded from a thermoplastic material.
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公开(公告)号:US20180058373A1
公开(公告)日:2018-03-01
申请号:US15250253
申请日:2016-08-29
Applicant: THE BOEING COMPANY
Inventor: Kevin O'Brien Gaw , Dylan E. Jones , Michael H. Larson , Belur N. Shivashankara , Randy J. Grove , David John Barene , Jeston Lingelbach , Kory Shaffer , David W. Foutch
Abstract: A blocker door assembly for use in a gas turbine engine includes a facesheet including a plurality of openings to facilitate noise attenuation and a body portion coupled to the facesheet. The body portion includes a backsheet integrally formed with a honeycomb core, wherein the body portion is molded from a thermoplastic material.
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公开(公告)号:US10794326B2
公开(公告)日:2020-10-06
申请号:US15250253
申请日:2016-08-29
Applicant: THE BOEING COMPANY
Inventor: Kevin O'Brien Gaw , Dylan E. Jones , Michael H. Larson , Belur N. Shivashankara , Randy J. Grove , David John Barene , Jeston Lingelbach , Kory Shaffer , David W. Foutch
Abstract: A blocker door assembly for use in a gas turbine engine includes a facesheet including a plurality of openings to facilitate noise attenuation and a body portion coupled to the facesheet. The body portion includes a backsheet integrally formed with a honeycomb core, wherein the body portion is molded from a thermoplastic material.
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公开(公告)号:US20200291892A1
公开(公告)日:2020-09-17
申请号:US16857487
申请日:2020-04-24
Applicant: The Boeing Company
Inventor: Kevin O'Brien Gaw , Dylan E. Jones , Michael H. Larson , Belur N. Shivashankara , Randy J. Grove , David John Barene , Jeston Lingelbach , Kory Shaffer , David W. Foutch
Abstract: A blocker door assembly for use in a gas turbine includes a panel, a core integrally formed with the panel, and a plurality of mounting structures extending from at least one of the panel and the core. The plurality of mounting structures are integrally formed with the core and the panel such that the panel, the core, and the mounting structures are co-molded from a thermoplastic material.
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