公开(公告)号：WO2008156932A3

公开(公告)日：2010-02-25

申请号：PCT/US2008063618

申请日：2008-05-15

Applicant: GEN ELECTRIC ,  ARIK MEHMET ,  SEELEY CHARLES ERKLIN ,  UTTURKAR YOGEN VISHWAS ,  BURDICK WILLIAM EDWARD JR ,  GORAY KUNAL RAVINDRA ,  WEAVER STANTON EARL JR

Inventor： ARIK MEHMET ,  SEELEY CHARLES ERKLIN ,  UTTURKAR YOGEN VISHWAS ,  BURDICK WILLIAM EDWARD JR ,  GORAY KUNAL RAVINDRA ,  WEAVER STANTON EARL JR

IPC: H01L23/40 ,  H01L23/467

CPC classification number: H01L23/40 ,  G06F1/20 ,  H01L23/467 ,  H01L2924/0002 ,  Y10T29/49002 ,  Y10T29/4935 ,  Y10T29/5313 ,  H01L2924/00

Abstract: A mounting apparatus for a cooling device is disclosed. The mounting apparatus includes a plurality of connectors extending outwardly from the cooling device. The mounting apparatus also includes at least one mounting post coupled to the plurality of connectors and configured to mount the cooling device on a substrate.

Abstract translation: 公开了一种用于冷却装置的安装装置。 安装装置包括从冷却装置向外延伸的多个连接器。 安装设备还包括至少一个安装柱，其连接到多个连接器并被配置成将冷却装置安装在基板上。

公开(公告)号：EP2969235A4

公开(公告)日：2016-11-16

申请号：EP14774640

申请日：2014-03-13

Applicant: GEN ELECTRIC

Inventor： DE BOCK HENDRIK PIETER JACOBUS ,  WHALEN BRYAN PATRICK ,  WEAVER STANTON EARL ,  SEELEY CHARLES ERKLIN

IPC: B23P17/00 ,  B05B17/06 ,  F04B43/04 ,  G06F1/20 ,  H01L23/467 ,  H05K7/20

CPC classification number: B05B17/0615 ,  F04D29/666 ,  F04D33/00 ,  G06F1/20 ,  H01L23/4336 ,  H01L23/467 ,  H01L23/4735 ,  H05K7/20172

Abstract: A system and method for reducing or increasing the mechanical structure resonance of a synthetic jet device is disclosed. A synthetic jet device includes a first plate, a second plate spaced apart from the first plate, a spacing component coupled to and positioned between the first and second plates to form a chamber and including an orifice therein, and an actuator element coupled to at least one of the first and second plates to selectively cause deflection thereof, thereby changing a volume within the chamber so that a series of fluid vortices is generated and projected out from the orifice of the spacing component. At least one of the first and second plates includes a modified section that alters a mechanical resonance of the synthetic jet device, so as to control a level of acoustic noise generated by the synthetic jet device.

公开(公告)号：DE602007009347D1

公开(公告)日：2010-11-04

申请号：DE602007009347

申请日：2007-10-29

Applicant: GEN ELECTRIC

Inventor： SHELDON KARL EDWARD ,  SEELEY CHARLES ERKLIN ,  HABER LUDWIG CHRISTIAN

IPC: B64D33/02 ,  B64D41/00 ,  F02C7/045 ,  F02C7/32

公开(公告)号：DE602005009625D1

公开(公告)日：2008-10-23

申请号：DE602005009625

申请日：2005-09-08

Applicant: GEN ELECTRIC

Inventor： SAIA RICHARD JOSEPH ,  NAJEWICZ DAVID JOSEPH ,  SEELEY CHARLES ERKLIN ,  WU GUANGHUA ,  KNOBLOCH AARON JAY

IPC: B81B7/02 ,  F15C5/00 ,  F23N1/00 ,  F24C3/12

Abstract: A control valve assembly (22) includes an inlet (16) for receiving a gas flow and an outlet (20) for providing the gas flow to a gas burner (18). The assembly (22) also includes a positive-shutoff valve (24) for interrupting the gas flow from the inlet (16). A micro electromechanical system (MEMS) valve (26) is coupled in series to the positive-shutoff valve (24) between the inlet (16) and the outlet (20) for regulating the gas flow from the inlet (16) to the outlet (20).

公开(公告)号：BR102013030756A2

公开(公告)日：2015-10-27

申请号：BR102013030756

申请日：2013-11-29

Applicant: GEN ELECTRIC

Inventor： AKHTAR AFROZ ,  NANUKUTTAN BIJU ,  SEELEY CHARLES ERKLIN ,  HYNUM DANIEL ALAN ,  SRIKANTA SANTHOSHA YELWAL ,  SAMUDRALA SRIKANTH ,  BONALA SRINATH ,  KANCHUMARTHY VAMSI KRISHNA

IPC: F03D1/06 ,  B23P11/00

Abstract: junta e método para conectar um primeiro segmento de pá a um segundo segmento de pá de uma pá de rotor de turbina eólica. trata-se de juntas para conectar um primeiro segmento de pá a um segundo segmento de pá de uma pá de rotor de turbina eólica que incluem um primeiro parafuso que compreende uma primeira extremidade proximal conectada ao primeiro segmento de pá e uma primeira extremidade distal conectada ao segundo segmento de pá, sendo que um segundo parafuso compreende uma segunda extremidade proximal conectada ao primeiro segmento de pá e uma segunda extremidade distal conectada ao segundo segmento de pá e um terceiro parafuso compreende uma terceira extremidade proximal conectada ao primeiro segmento de pá e uma terceira extremidade distal conectada ao terceiro segmento de pá. pelo menos dois dentre o primeiro parafuso, o segundo parafuso e o terceiro parafuso se diferem em tamanho e uma primeira distância entre o primeiro parafuso e o segundo parafuso é diferente de uma segunda distância entre o segundo parafuso e o terceiro parafuso.

公开(公告)号：DE102012107415A1

公开(公告)日：2013-02-28

申请号：DE102012107415

申请日：2012-08-13

Applicant: GEN ELECTRIC

Inventor： HYNUM DANIEL ,  SEELEY CHARLES ERKLIN ,  BUSBEY BRUCE C ,  GERBER BRANDON S ,  BAEHMANN PEGGY LYNN ,  JOHNSON ROGER NEAL

IPC: F03D1/06

Abstract: Es wird ein Verbindungsstück (50) zum Verbinden eines ersten Blattsegmentes (52) und eines zweiten Blattsegmentes (54) eines Rotorblattes (16) einer Windkraftanlage (10) offengelegt. Das Verbindungsstück 50 enthält einen Körper (60), wobei der Körper (60) eine Außenoberfläche (62) und eine Innenoberfläche (64) enthält. Die Außenoberfläche (62) hat eine aerodynamische Kontur, die im Wesentlichen einer aerodynamischen Kontur des ersten Blattsegmentes (52) und des zweiten Blattsegmentes (54) entspricht. Der Körper (60) enthält eine sich zwischen einer Vorderkante (76) und einer Hinterkante (78) erstreckende Druckseite (72) und eine Saugseite (74). In einigen Ausführungsformen enthält das Verbindungsstück (50) ferner einen in der Außenoberfläche (62) des Körpers (60) definierten Kanal (80). Der Kanal (80) enthält eine im Wesentlichen zusammenhängende Basiswand (82), die sich zwischen gegenüberliegenden Seitenwänden (84, 86) erstreckt. Die Innenoberfläche (64) enthält die Basiswand (82). In weiteren Ausführungsformen enthält das Verbindungsstück (50) ferner einen in dem Körper (60) definierten Kanal (80) und eine sich von dem Körper (60) aus im Wesentlichen in Spannenrichtung erstreckende Schale (90).

公开(公告)号：DE602007013933D1

公开(公告)日：2011-05-26

申请号：DE602007013933

申请日：2007-10-26

Applicant: GEN ELECTRIC

Inventor： ARIK MEHMET ,  WOLFE CHARLES FRANKLIN ,  UTTURKAR YOGEN VISHWAS ,  SEELEY CHARLES ERKLIN ,  SLATON DAVID SHANNON ,  LUECKENBACH WILLIAM HENRY

IPC: G06F1/20

公开(公告)号：AT505759T

公开(公告)日：2011-04-15

申请号：AT07844627

申请日：2007-10-26

Applicant: GEN ELECTRIC

Inventor： ARIK MEHMET ,  WOLFE CHARLES FRANKLIN ,  UTTURKAR YOGEN VISHWAS ,  SEELEY CHARLES ERKLIN ,  SLATON DAVID ,  LUECKENBACH WILLIAM HENRY

IPC: G06F1/20

Abstract: A thermal management system for an embedded environment is described. The thermal management system includes a pleumo-jet that has at least one wall defining a chamber, at least one piezoelectric device on the at least one wall, and a compliant material within the at least one wall and encompassing the chamber. The compliant material has at least one opening providing fluid communication between said chamber and the embedded environment. A cooling system is also described. A method for making a pleumo-jet is also described.

公开(公告)号：CA2607051A1

公开(公告)日：2008-04-30

申请号：CA2607051

申请日：2007-10-18

Applicant: GEN ELECTRIC

Inventor： SHELDON KARL EDWARD ,  HABER LUDWIG CHRISTIAN ,  SHIEH CHINGWEI MICHAEL ,  SEELEY CHARLES ERKLIN ,  WOOD TREVOR HOWARD ,  LUEDKE JONATHAN GLENN

IPC: B64D41/00 ,  B64D33/02

Abstract: An embodiment of the technology described herein is an auxiliary power uni t assembly (10). The auxiliary power unit assembly (10) includes an auxiliary power unit being installable in an aircraft (18) having a cabin (22), a duct (28) connecting the cabin (22) and the auxiliary power unit, and a noise reduction feature (26) in the duct (28).

公开(公告)号：CA2606739A1

公开(公告)日：2008-04-30

申请号：CA2606739

申请日：2007-10-18

Applicant: GEN ELECTRIC

Inventor： SEELEY CHARLES ERKLIN ,  HABER LUDWIG CHRISTIAN ,  SHELDON KARL EDWARD

IPC: B64D41/00 ,  B64D33/02

Abstract: An embodiment of the technology described herein is an auxiliary power uni t assembly (10). The auxiliary power unit assembly (10) includes an auxiliary power unit being installable in an aircraft (18) having a cabin (22), a duct (28) connecting the cabin (22) and the auxiliary power unit, and an airflow management feature i n the duct.