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公开(公告)号：US20130193270A1
公开(公告)日：2013-08-01
申请号：US13788266
申请日：2013-03-07
Applicant: The Boeing Company
Inventor： Diane C. Rawlings , James D. McLean , Mary J. Mathews
CPC classification number: B64C21/10 , B29C65/4855 , B64C2230/26 , F15D1/12 , Y02T50/166 , Y10T156/1039
Abstract: An array of aerodynamic riblets is formed with a surface layer for adhering to an aerodynamic surface and a plurality of riblet tips having a parabolic cross section extending from the surface layer.
Abstract translation: 空气动力肋阵列形成有用于粘附到空气动力学表面的表面层和具有从表面层延伸的抛物线横截面的多个肋尖。
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公开(公告)号：US09714083B2
公开(公告)日：2017-07-25
申请号：US14705564
申请日：2015-05-06
Applicant: The Boeing Company
Inventor： Diane C. Rawlings
IPC: B64C1/38 , B64C21/10 , B05D5/06 , B44F1/02 , B64C23/00 , B64D45/00 , G09F19/00 , B42D25/324 , B41F15/00 , B44B5/00 , G09F19/12 , G09F21/08
CPC classification number: B64C21/10 , B05D1/28 , B05D3/12 , B05D5/06 , B05D5/063 , B05D5/065 , B41F15/00 , B41F15/0872 , B42D25/324 , B44B5/0047 , B44B5/0095 , B44F1/02 , B64C23/00 , B64C2230/26 , B64D45/00 , F15D1/00 , G09F19/00 , G09F19/12 , G09F21/08
Abstract: Color applications for aerodynamic microstructures are disclosed herein. One disclosed example apparatus includes an aerodynamic microstructure of a vehicle, sub-microstructures superimposed on the aerodynamic microstructure, and a color application defined on or within the microstructure.
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公开(公告)号：US20160318603A1
公开(公告)日：2016-11-03
申请号：US15212218
申请日：2016-07-16
Applicant: The Boeing Company
Inventor： Diane C. Rawlings , Kevin R. Malone
CPC classification number: B64C21/10 , B32B3/30 , B32B15/08 , B32B25/08 , B32B27/283 , B32B27/288 , B32B27/34 , B32B27/38 , B32B27/40 , B32B2250/02 , B32B2307/416 , B32B2307/50 , B32B2307/702 , B32B2605/18 , B64C1/38 , B64C2230/26 , F15D1/0035 , F15D1/004 , Y02T50/166 , Y10T428/24612
Abstract: A multilayer construction for aerodynamic riblets includes a first layer composed of a material with protuberances, the first layer material exhibiting a first characteristic having long-term durability and a second layer composed of a material, exhibiting a second characteristic with capability for adherence to a surface.
Abstract translation: 用于空气动力学肋的多层结构包括由具有突起的材料构成的第一层，第一层材料具有长期耐久性的第一特性和由材料构成的第二层，具有粘附于表面的能力的第二特性 。
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公开(公告)号：US10946559B2
公开(公告)日：2021-03-16
申请号：US16148760
申请日：2018-10-01
Applicant: The Boeing Company
Inventor： Diane C. Rawlings , Bruce K. Keough , Larry K. Olli , Alan G. Burg , James M. Kestner , George Michael Granger , James Charles McGarvey
IPC: B29C39/12 , B32B27/28 , B32B3/30 , B64C21/10 , B32B37/20 , B32B37/10 , B32B37/00 , B32B37/02 , B32B37/24 , B29C39/14 , B29C39/18 , B29C39/38 , B32B33/00 , B29C41/30 , B29C41/32 , B29C41/46 , B29C39/16 , B29C65/78 , B29L7/00 , B29L31/00 , B29L9/00 , B29K101/12 , B29L31/30
Abstract: Multilayer riblet applique and methods of producing the same are described herein. One disclosed example method includes applying a first high elongation polymer material to a web tool, where the web tool is to be provided from a first roll, and heating, via a first heating process, the first high elongation polymer material. The disclosed example method also includes applying a second high elongation polymer material to the first high elongation polymer material, and heating, via a second heating process, the second high elongation polymer material. The disclosed example method also includes applying, via a laminating roller, a support layer to the second high elongation polymer material.
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公开(公告)号：US20190030764A1
公开(公告)日：2019-01-31
申请号：US16148760
申请日：2018-10-01
Applicant: The Boeing Company
Inventor： Diane C. Rawlings , Bruce K. Keough , Larry K. Olli , Alan G. Burg , James M. Kestner , George Michael Granger , James Charles McGarvey
IPC: B29C39/14 , B64C21/10 , B29C39/16 , B29C39/18 , B29C39/38 , B29C41/30 , B29C41/32 , B29C41/46 , B29C65/78 , B32B3/30 , B32B27/28 , B32B37/10 , B32B37/20 , B29K101/12 , B32B37/00 , B32B37/02 , B29L7/00 , B29L9/00 , B32B37/24 , B29L31/30 , B29L31/00
Abstract: Multilayer riblet applique and methods of producing the same are described herein. One disclosed example method includes applying a first high elongation polymer material to a web tool, where the web tool is to be provided from a first roll, and heating, via a first heating process, the first high elongation polymer material. The disclosed example method also includes applying a second high elongation polymer material to the first high elongation polymer material, and heating, via a second heating process, the second high elongation polymer material. The disclosed example method also includes applying, via a laminating roller, a support layer to the second high elongation polymer material.
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Patent Agency Ranking
公开(公告)号：US10105877B2
公开(公告)日：2018-10-23
申请号：US15205460
申请日：2016-07-08
Applicant: The Boeing Company
Inventor： Diane C. Rawlings , Bruce K. Keough , Larry K. Olli , Alan G. Burg , James M. Kestner , George Michael Granger , James Charles McGarvey
IPC: B29C39/14 , B29C39/16 , B29C65/78 , B32B37/10 , B29C39/18 , B29C39/38 , B29C41/30 , B29C41/32 , B29C41/46 , B32B27/28 , B32B3/30 , B64C21/10 , B32B37/20 , B29K101/12 , B29L31/30 , B32B37/24 , B29L7/00 , B29L31/00 , B32B37/00 , B29L9/00 , B32B37/02
Abstract: Multilayer riblet applique and methods of producing the same are described herein. One disclosed example method includes applying a first high elongation polymer material to a web tool, where the web tool is to be provided from a first roll, and heating, via a first heating process, the first high elongation polymer material. The disclosed example method also includes applying a second high elongation polymer material to the first high elongation polymer material, and heating, via a second heating process, the second high elongation polymer material. The disclosed example method also includes applying, via a laminating roller, a support layer to the second high elongation polymer material.
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公开(公告)号：US09751618B2
公开(公告)日：2017-09-05
申请号：US14705547
申请日：2015-05-06
Applicant: The Boeing Company
Inventor： Diane C. Rawlings , Timothy Leroy Williams , James C. McGarvey , James M. Kestner , Alan G. Burg
IPC: B64C1/38 , B64C21/10 , B44F1/02 , B64C23/00 , B64D45/00 , G09F19/12 , G09F19/14 , B42D25/324 , G09F21/08 , B41M3/00
CPC classification number: B64C21/10 , B32B3/30 , B41M3/00 , B42D25/324 , B44B5/0047 , B44B5/0095 , B44F1/02 , B64C23/00 , B64C2230/26 , B64D45/00 , F15D1/00 , G09F19/12 , G09F19/14 , G09F21/08 , Y02T50/166
Abstract: Aerodynamic microstructures having sub-microstructure are disclosed herein. One disclosed example apparatus includes an aerodynamic microstructure defining an external surface of a vehicle, and a pattern of sub-microstructures superimposed on the microstructure to convey a representation of an image.
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公开(公告)号：US09635715B1
公开(公告)日：2017-04-25
申请号：US13889657
申请日：2013-05-08
Applicant: The Boeing Company
Inventor： Robert James Miller , Marc R. Matsen , Diane C. Rawlings
CPC classification number: H05B6/105 , H05B2206/023
Abstract: A radiant heater having a ferromagnetic element includes a high emissivity surface and an induction coil operatively coupled with the ferromagnetic element. The induction coil may be energized to create eddy currents heating the ferromagnetic element until the element reaches its Curie temperature. At the Curie temperature the ferromagnetic element becomes substantially nonmagnetic and the temperature of the element remains relatively constant. The high emissivity surface of the heater provides a substantially uniform radiant heat to an object in close proximity to the high emissivity surface. The object may be thermally coupled with the high emissivity surface of the radiant heater. The radiant heater having a high emissivity surface may be used to heat temperature sensitive objects such as thin films. Multiple radiant heaters having different Curie temperatures may be used to ramp up a temperature, ramp down a temperature, or provide different temperatures required during a process.
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公开(公告)号：US20160297515A9
公开(公告)日：2016-10-13
申请号：US14070183
申请日：2013-11-01
Applicant: The Boeing Company
Inventor： Diane C. Rawlings , Stephen Christensen
CPC classification number: B64C21/10 , B32B3/08 , B32B3/30 , B32B7/12 , B32B15/08 , B32B15/20 , B32B25/08 , B32B27/283 , B32B27/288 , B32B27/34 , B32B27/38 , B32B27/40 , B32B2250/02 , B32B2307/416 , B32B2307/50 , B32B2307/702 , B32B2605/18 , B64C1/38 , B64C2230/26 , F15D1/0035 , F15D1/004 , Y02T50/166 , Y10T428/24355 , Y10T428/24612
Abstract: An array of aerodynamic riblets is created by a plurality of high stiffness tips with a layer supporting the tips in predetermined spaced relation and adhering the tips to a vehicle surface.
Abstract translation: 空气动力肋的阵列由多个高刚度尖端产生，其具有以预定的间隔关系支撑尖端的层并且将尖端附接到车辆表面。
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公开(公告)号：US11452178B2
公开(公告)日：2022-09-20
申请号：US14937511
申请日：2015-11-10
Applicant: The Boeing Company
Inventor： Robert J. Miller , John F. Spalding, Jr. , Diane C. Rawlings , Darrell M. Storvick , Christopher J. Hottes
Abstract: A heating blanket is disclosed. The heating blanket may include a thermoplastic matrix configured to become conformable at a predetermined temperature, a conductor embedded in the thermoplastic matrix and configured to receive electrical current and generate a magnetic field in response to the electrical current, and a plurality of susceptors embedded in the thermoplastic matrix and composed of a magnetic material having a Curie point.
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