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公开(公告)号:US20230184339A1
公开(公告)日:2023-06-15
申请号:US18075075
申请日:2022-12-05
Inventor: Osamu SHINDO , Miyako NIMORI , Shunichi HORII , Ryuhei TAKEMARU
Abstract: There are provided a steam valve and the like capable of preventing breakage of an auxiliary valve element and effectively suppressing the occurrence of a leak of steam in the auxiliary valve element. In the steam valve of an embodiment, the auxiliary valve element is structured to be in an open state in which the valve rod moves in an opening direction to increase a distance between an auxiliary-valve cap and a main valve element, thereby opening an auxiliary-valve steam introduction hole, and to be in a fully-closed state in which the valve rod moves in a closing direction in which the main valve element is closed to bring the auxiliary-valve cap and the main valve element into contact with each other, thereby closing the auxiliary-valve steam introduction holes. A contact position in which the auxiliary-valve cap and the main valve element are brought into contact with each other is located outside in a radial direction of the valve rod from the outer peripheral surface, of the auxiliary-valve tubular part, through which the auxiliary-valve steam introduction holes are formed.
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公开(公告)号:US20180306050A1
公开(公告)日:2018-10-25
申请号:US15771064
申请日:2015-10-28
Inventor: Tomoaki Nogami , Takuro Koda , Kenichi Nishiyama
CPC classification number: F01D17/10 , F05D2220/31 , F16K31/44 , G05D7/0647
Abstract: A valve device includes a main steam valve that is provided on a steam flow channel, a regulating valve that is provided on the steam flow channel to be connected to the main steam valve in series and that includes a first valve seat and a first valve body, an overload valve that is provided on a branch flow channel which connects a portion of the steam flow channel between the main steam valve and the regulating valve and a steam turbine to each other and that includes a second valve seat and a second valve body, and a driving unit that drives the first valve body and the second valve body as a common driving source of the first valve body and the second valve body such that the first valve body and the second valve body are interlocked with each other.
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公开(公告)号:US20180252320A1
公开(公告)日:2018-09-06
申请号:US15770372
申请日:2016-10-21
Applicant: Mitsubishi Hitachi Power Systems, Ltd.
Inventor: Kensuke FUTAHASHI , Hiroyuki KANAZAWA , Kengo IMAOKA , Katsuhisa HAMADA
CPC classification number: F16K1/443 , F01D17/10 , F01D25/00 , F05D2220/31 , F16K1/44 , F16K47/02 , Y10T137/87917
Abstract: A steam valve includes a valve casing, a first valve body having a first cylindrical part and a first end wall part, a second valve body having a second cylindrical part and a second end wall part, a first valve stem capable of vertically biasing the first valve body, a second valve stem capable of vertically biasing the second valve body, a flow guide disposed inside the first cylindrical part and having a projection configured to project downwardly from the first cylindrical part and the second cylindrical part when the first cylindrical part and the second cylindrical part are apart from the valve seat, and a support supporting the flow guide. The support extends from the valve casing or the second valve body to the flow guide through a through hole formed in the first valve body to support the flow guide such that the flow guide is tiltable.
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4.
公开(公告)号:US09926795B2
公开(公告)日:2018-03-27
申请号:US14682786
申请日:2015-04-09
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Leslie Charles Kurz
IPC: F01D5/30 , F01D5/32 , F01D5/02 , F01D5/26 , F01D17/10 , F04D29/36 , F04D29/34 , F04D29/38 , F01D5/16
CPC classification number: F01D5/3007 , F01D5/02 , F01D5/16 , F01D5/26 , F01D17/10 , F04D29/34 , F04D29/362 , F04D29/38 , F05D2220/32 , F05D2230/60 , Y10T29/49323
Abstract: The present disclosure provides a blade positioning and support system for a gas turbine engine including a blade, the blade having a root and a tip, with the root having a surface oriented away from the tip, the surface having a forward end and an aft end, the forward end projecting farther away from the tip than the aft end. Further, the present disclosure provides a blade receiver, the blade receiver having a face and a facet, with the face being oriented away from the facet, the face having a forward end and an aft end, the aft end projecting farther away from the facet than the forward end.
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5.
公开(公告)号:US20180045069A1
公开(公告)日:2018-02-15
申请号:US15673102
申请日:2017-08-09
Applicant: Rolls-Royce Deutschland Ltd & Co KG
Inventor: Predrag TODOROVIC
CPC classification number: F01D17/141 , F01D11/24 , F01D17/10 , F01D17/20 , F05D2220/323 , F05D2260/52 , F05D2260/57 , F05D2270/66 , F16H19/04 , F16H21/44 , F16H33/20 , F16K1/2007 , F16K31/54 , G01D5/2291 , Y02T50/671
Abstract: A device of a turbomachine actuates a setting device to vary a flow cross-section of a flow channel of the turbomachine passable by a fluid flow. The device includes a displacement mechanism having an adjustable actuation appliance and couplable with the setting device, and a drive device for displacing the actuation appliance. The displacement mechanism has a centrifugal force appliance displaceable between a basic position and a maximally displaced working position depending on a number of revolutions of the drive device, wherein the actuation appliance is displaceable depending on the position of the centrifugal force appliance with respect to the drive device. A reset device applies a force to the centrifugal force appliance by which the centrifugal force appliance is pressed in the direction of its basic position.
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公开(公告)号:US09840933B2
公开(公告)日:2017-12-12
申请号:US14577757
申请日:2014-12-19
Applicant: Schlumberger Technology Corporation
Inventor: Gocha Chochua , Kent D. Harms
Abstract: An apparatus for extending the operational flow rate range of a turbine is described herein. Two or more removable sleeves may be used to change the cross-sectional area of a turbine. Each removable sleeve may define or eliminate the stator gap between a stator blade tip and an inner wall of the removable sleeve and a rotor gap between a rotor blade tip and an inner wall of the removable sleeve. A movable sleeve may be disposed in the turbine and may move between a first position and a second position in response to changes in the pressure differential across the turbine. The movable sleeve may define or eliminate a stator gap between a stator blade tip and the inner conical surface of the sleeve or a hub of the turbine and a rotor gap between a rotor blade tip and the inner conical surface of the sleeve.
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7.
公开(公告)号:US20170268374A1
公开(公告)日:2017-09-21
申请号:US15071264
申请日:2016-03-16
Applicant: General Electric Company
Inventor: Aaron Todd Sellinger , Nicholas Joseph Kray , Wendy Wenling Lin
CPC classification number: F01D17/141 , F01D5/148 , F01D17/10 , F02C7/042 , F02C9/18 , F04D27/0215 , F04D27/023 , F04D29/563 , F05D2220/32 , F05D2250/90 , F05D2270/20 , F05D2270/60 , F05D2270/64 , F05D2270/65 , F05D2300/501 , Y02T50/672 , Y02T50/673
Abstract: A system for actuating components of a gas turbine engine may generally include a turbine component incorporating a jamming device. The jamming device may include a bladder and a jammable media contained within the bladder. The jammable media may be jammable within the bladder from an unjammed state, wherein a fluid is contained within the bladder, to a jammed state, wherein the fluid is at least partially evacuated from the bladder. The system may also include a fluid coupling in fluid communication with the bladder. A portion of the turbine component may be located at a first position when the jammable media is in the unjammed state. Additionally, such portion of the turbine component may be located at a second position when the jammable media is in the jammed state.
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公开(公告)号:US20170191508A1
公开(公告)日:2017-07-06
申请号:US14985770
申请日:2015-12-31
Applicant: WESTINGHOUSE ELECTRIC COMPANY LLC
Inventor: Dylan T. Boby , DAVID J. BUBECK
IPC: F15B20/00
CPC classification number: F15B20/004 , F01D17/10 , F15B20/008 , F15B2211/30505 , F15B2211/30565 , F15B2211/31582 , F15B2211/411 , F15B2211/41527 , F15B2211/8755 , F15B2211/8757
Abstract: A hydraulic apparatus includes a first valve manifold that provides a shutdown capability and a second valve manifold that provides an overspeed control capability. The hydraulic apparatus advantageously further employs a hydraulic appliance that includes a check valve and a bypass apparatus. The hydraulic appliance enables the second valve manifold to additionally provide as an alternative function a redundant shutdown capability, thereby obviating the need to have three separate valve manifolds.
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公开(公告)号:US09677460B2
公开(公告)日:2017-06-13
申请号:US14727563
申请日:2015-06-01
Applicant: Ford Global Technologies, LLC
Inventor: Daniel Joseph Styles , Jack Adams , Keith Michael Plagens , Neal James Corey , David Born , Xiaogang Zhang
IPC: F02D23/00 , F02B33/44 , F16K11/07 , F02B37/02 , F02B37/12 , F01D9/02 , F01D17/10 , F02B33/38 , F02B37/18
CPC classification number: F02B37/025 , F01D9/026 , F01D17/10 , F02B33/38 , F02B37/12 , F02B37/18 , F05D2220/40 , F05D2240/40 , F05D2260/60 , Y02T10/144
Abstract: Methods and systems are provided for a branch communication valve in a twin turbocharger system. A branch communication valve may be positioned adjacent to a dividing wall separating a first scroll and a second scroll of the twin turbocharger. In an open position, the branch communication valve increases fluid communication between the first scroll and the second scroll and in a closed position, the branch communication valve decreases fluid communication between the first scroll and the second scroll.
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公开(公告)号:US09567867B2
公开(公告)日:2017-02-14
申请号:US13618733
申请日:2012-09-14
Applicant: Parthiv N. Shah
Inventor: Parthiv N. Shah
Abstract: An aircraft control structure for drag management includes a nozzle structure configured to exhaust a swirling fluid stream. A plurality of swirl vanes are positioned within the nozzle structure, and an actuation subsystem is configured to cause the plurality of swirl vanes to move from a deployed state to a non-deployed state. In the non-deployed state, the plurality of swirl vanes are substantially flush with the inner surface of the nozzle structure. In the deployed state, the plurality of swirl vanes produce the swirling fluid stream.
Abstract translation: 用于拖曳管理的飞行器控制结构包括被配置为排出旋流流体流的喷嘴结构。 多个旋流叶片位于喷嘴结构内,并且致动子系统构造成使得多个旋流叶片从展开状态移动到非展开状态。 在非展开状态下,多个旋流叶片基本上与喷嘴结构的内表面齐平。 在展开状态下,多个旋流叶片产生旋流流体流。
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