-
公开(公告)号：US261226A
公开(公告)日：1882-07-18
申请号：US261226D
CPC classification number: A24F19/06 , F17C2201/0152
-
公开(公告)号：US20240263739A1
公开(公告)日：2024-08-08
申请号：US18439374
申请日：2024-02-12
Applicant: MAGNA INTERNATIONAL INC.
Inventor： James McBRIDE , William PERRY
CPC classification number: F17C1/14 , F17C1/08 , F17C13/06 , F17C2201/0128 , F17C2201/0152 , F17C2203/012 , F17C2203/0646 , F17C2209/2181 , F17C2209/221 , F17C2209/224 , F17C2209/232 , F17C2209/234 , F17C2223/0123
Abstract: A reservoir assembly includes one or more pressure vessels each having a non-circular cross-sectional shape including a rounded rectangle having four generally flat sides with rounded corners. The pressure vessels may be formed of extruded metal, such as aluminum, and have a generally constant cross-section. The pressure vessels include stiffening ribs and varying wall thicknesses to improve strength and to minimize stresses when pressurized, such as during operation when filled with compressed gas. The stiffening ribs meet in the center of each of the pressure vessels and divide the interior volumes into four equal sections. A cap of stamped aluminum is fitted and fully welded to enclose each end of the pressure vessels. One or both of the caps on each of the pressure vessels has a pressure fitting. Two or more pressure vessels extend parallel to one another and are attached together to form the reservoir assembly.
-
公开(公告)号：US20240151353A1
公开(公告)日：2024-05-09
申请号：US17983847
申请日：2022-11-09
Applicant: Karbon CCS ltd.
Inventor： Henrik Fleischer , Knut Erik Børseth , Nils Christian Høy-Petersen
IPC: F17C1/08
CPC classification number: F17C1/08 , F17C2201/0152 , F17C2201/0171 , F17C2203/012 , F17C2205/0352 , F17C2221/013 , F17C2221/033 , F17C2270/0105
Abstract: A four-lobe cargo tank for transporting and/or storage of liquefied gases includes four main lobes, each with a cylinder sector outer shell and main lobe axis. The four main lobes are arranged with the four main lobe axis axial-parallel with and about a common main central axis, such that the four main lobes are joined by four web frames with four corresponding diagonally arranged perforated bulkheads directed outwardly from the main central axis. The tank includes a first and a second end cover. Each end cover includes four quarter spherical shell portions, each forming an end portion of the cylinder sector outer shell. The quarter spherical shell portions of the first and second end covers, respectively, are joined and closing toward the main central axis by a first and a second four diagonally arranged cylindrical 45-degree cut pipe portions, which are each arranged with its axis transverse to the main axis.
-
公开(公告)号：US11873947B2
公开(公告)日：2024-01-16
申请号：US17664283
申请日：2022-05-20
Applicant: Trelleborg Sealing Solutions Germany GmbH
Inventor： David Edgar Hauber
IPC: B29C70/14 , F17C1/06 , B29C70/32 , B29K307/04 , B29K105/14 , B29L31/00
CPC classification number: F17C1/06 , B29C70/14 , B29C70/32 , B29K2105/14 , B29K2307/04 , B29L2031/7156 , F17C2201/0109 , F17C2201/0128 , F17C2201/0138 , F17C2201/0152 , F17C2203/0621 , F17C2203/0673 , F17C2209/2109 , F17C2209/2163 , F17C2209/232 , F17C2221/012 , F17C2221/033 , F17C2223/036 , F17C2270/0171
Abstract: A method of manufacturing a high-pressure composite pressure vessel for high-pressure being at or above 70 bar (1000 PSI or 7 MPa) includes providing an expandable core vessel defining a hoop section between end domes. An aligned discontinuous fiber composite material is wrapped over the expandable core vessel aligning with a plurality of load paths present in the expandable core vessel being over the hoop section and end domes. The aligned discontinuous fiber composite material has fibers in a prepreg tape that are at least 5 mm in length to 100 mm in length or less. Next, a continuous fiber-reinforced composite is wrapped over the aligned discontinuous fiber-reinforced composite along the hoop section and not wrapped along the end domes. The expandable core vessel may be pressurized and heated to consolidate the composite overwrap. Finally, the vessel is cooled under pressure resulting in the high-pressure composite pressure vessel.
-
公开(公告)号：US20180356038A1
公开(公告)日：2018-12-13
申请号：US15779139
申请日：2015-11-25
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Wenping Zhao , Ellen Y. Sun
IPC: F17C1/06
CPC classification number: F17C1/06 , F17C2201/0152 , F17C2201/0171 , F17C2203/0604 , F17C2203/0629 , F17C2203/0631 , F17C2203/0636 , F17C2203/066 , F17C2203/0663 , F17C2205/013 , F17C2209/2118 , F17C2209/2127 , F17C2221/012 , F17C2221/031 , F17C2221/033 , F17C2221/035 , F17C2260/012 , F17C2270/0168 , Y02E60/321
Abstract: A composite pressure vessel assembly includes at least one liner defining a chamber. The liner is perforated such that an applied composite layer envelops the liner and at least partially extrudes into the perforations during manufacture and when the chamber is placed under a vacuum.
-
Patent Agency Ranking
公开(公告)号：US20170299122A1
公开(公告)日：2017-10-19
申请号：US15517017
申请日：2014-10-07
Applicant: UNITED TECHNOLOGIES RESEARCH CENTER
Inventor： Paul F. Croteau , Andrzej Ernest Kuczek , Daniel V. Viens , Justin R. Hawkes , Wenping Zhao , Thomas J. Garosshen
CPC classification number: F17C13/002 , F17C1/00 , F17C1/14 , F17C1/16 , F17C2201/0152 , F17C2201/0166 , F17C2201/0171 , F17C2201/056 , F17C2203/0617 , F17C2203/0636 , F17C2203/0643 , F17C2203/0646 , F17C2203/0663 , F17C2205/0146 , F17C2205/0305 , F17C2209/2181 , F17C2209/221 , F17C2221/012 , F17C2221/031 , F17C2221/033 , F17C2221/035 , F17C2223/0123 , F17C2223/035 , F17C2260/018 , F17C2270/0168 , Y02E60/321
Abstract: A pressure vessel fluid manifold assembly includes a pressure vessel having a plurality of lobes joined to each other, each of the plurality of lobes having a wall disposed in contact with an adjacent wall of an adjacent lobe, and wherein the manifold can be external or internal to the lobes.
-
公开(公告)号：US09476546B2
公开(公告)日：2016-10-25
申请号：US14671787
申请日：2015-03-27
Applicant: GOODRICH CORPORATION
Inventor： Paul F. Croteau , Andrzej E. Kuczek , Wenping Zhao
CPC classification number: F17C1/14 , F17C1/00 , F17C1/16 , F17C2201/0109 , F17C2201/0152 , F17C2201/0166 , F17C2201/054 , F17C2201/056 , F17C2203/0617 , F17C2203/0639 , F17C2203/0646 , F17C2203/0648 , F17C2203/0663 , F17C2209/221 , F17C2209/222 , F17C2221/013 , F17C2221/014 , F17C2221/033 , F17C2221/035 , F17C2223/0123 , F17C2223/0153 , F17C2223/033 , F17C2223/035 , F17C2260/018 , F17C2270/0105 , F17C2270/0168 , F17C2270/0189
Abstract: A high-pressure vessel is provided. The high-pressure vessel may comprise a first chamber defined at least partially by a first wall, and a second chamber defined at least partially by the first wall. The first chamber and the second chamber may form a curved contour of the high-pressure vessel. A modular tank assembly is also provided, and may comprise a first mid tube having a convex geometry. The first mid tube may be defined by a first inner wall, a curved wall extending from the first inner wall, and a second inner wall extending from the curved wall. The first inner wall may be disposed at an angle relative to the second inner wall. The first mid tube may further be defined by a short curved wall opposite the curved wall and extending from the second inner wall to the first inner wall.
Abstract translation: 提供高压容器。 高压容器可以包括至少部分地由第一壁限定的第一室和至少部分地由第一壁限定的第二室。 第一室和第二室可以形成高压容器的弯曲轮廓。 还提供了一种模块化油箱组件，并且可以包括具有凸几何形状的第一中间管。 第一中管可以由第一内壁，从第一内壁延伸的弯曲壁和从弯曲壁延伸的第二内壁限定。 第一内壁可以相对于第二内壁成一定角度设置。 第一中管还可以由与弯曲壁相对的短弯曲壁限定，并从第二内壁延伸到第一内壁。
-
公开(公告)号：US20160281926A1
公开(公告)日：2016-09-29
申请号：US14671787
申请日：2015-03-27
Applicant: GOODRICH CORPORATION
Inventor： Paul F. Croteau , Andrzej E. Kuczek , Wenping Zhao
CPC classification number: F17C1/14 , F17C1/00 , F17C1/16 , F17C2201/0109 , F17C2201/0152 , F17C2201/0166 , F17C2201/054 , F17C2201/056 , F17C2203/0617 , F17C2203/0639 , F17C2203/0646 , F17C2203/0648 , F17C2203/0663 , F17C2209/221 , F17C2209/222 , F17C2221/013 , F17C2221/014 , F17C2221/033 , F17C2221/035 , F17C2223/0123 , F17C2223/0153 , F17C2223/033 , F17C2223/035 , F17C2260/018 , F17C2270/0105 , F17C2270/0168 , F17C2270/0189
Abstract: A high-pressure vessel is provided. The high-pressure vessel may comprise a first chamber defined at least partially by a first wall, and a second chamber defined at least partially by the first wall. The first chamber and the second chamber may form a curved contour of the high-pressure vessel. A modular tank assembly is also provided, and may comprise a first mid tube having a convex geometry. The first mid tube may be defined by a first inner wall, a curved wall extending from the first inner wall, and a second inner wall extending from the curved wall. The first inner wall may be disposed at an angle relative to the second inner wall. The first mid tube may further be defined by a short curved wall opposite the curved wall and extending from the second inner wall to the first inner wall.
Abstract translation: 提供高压容器。 高压容器可以包括至少部分地由第一壁限定的第一室和至少部分地由第一壁限定的第二室。 第一室和第二室可以形成高压容器的弯曲轮廓。 还提供了一种模块化油箱组件，并且可以包括具有凸几何形状的第一中间管。 第一中管可以由第一内壁，从第一内壁延伸的弯曲壁和从弯曲壁延伸的第二内壁限定。 第一内壁可以相对于第二内壁成一定角度设置。 第一中管还可以由与弯曲壁相对的短弯曲壁限定，并从第二内壁延伸到第一内壁。
-
99.发明申请Tank System For The Cryogenic Storage Of Hydrogen, And Aircraft With A Tank System For The Cryogenic Storage Of Hydrogen 审中-公开用于低温储存氢气的坦克系统和具有用于氢的低温储存的罐系统的飞机公开(公告)号：US20150336680A1
公开(公告)日：2015-11-26
申请号：US14718229
申请日：2015-05-21
Applicant: Airbus Operations GmbH
Inventor： Markus Schumacher , Claus Hoffjann , Frank Lehmberg
CPC classification number: B64D37/06 , B64D37/04 , B64D37/30 , B64D37/32 , F17C3/00 , F17C2201/0104 , F17C2201/0128 , F17C2201/0147 , F17C2201/0152 , F17C2201/0157 , F17C2201/0166 , F17C2201/0171 , F17C2201/054 , F17C2203/013 , F17C2203/0304 , F17C2203/0391 , F17C2221/012 , F17C2223/0161 , F17C2223/033 , F17C2260/018 , F17C2270/0189 , Y02E60/321 , Y02T50/44 , Y02T90/44
Abstract: A tank system for the cryogenic storage of hydrogen includes a tank structure with at least one hollow body for accommodating liquid hydrogen and at least one insulating means, which encloses the tank structure, for insulating the at least one hollow body. The tank structure has an exterior shape that is integrateable in a load-bearing primary structure of an aircraft. The tank structure is load bearing and is designed to at least partially absorb a load introduced into the primary structure. This makes it possible to achieve a particularly efficient design of an aircraft in which the fuselage of the aircraft is not divided into two parts by the hydrogen tank integrated therein, can be arranged near the center of gravity, and essentially does not increase the additional weight of the aircraft.
Abstract translation: 用于氢的低温储存的罐系统包括具有用于容纳液态氢的至少一个中空体的罐结构和封闭罐结构的至少一个绝缘装置，用于绝缘至少一个中空体。 油箱结构具有可与飞行器的承载主结构相结合的外部形状。 罐结构是负载轴承，并且被设计成至少部分地吸收引入到主结构中的负载。 这使得可以实现飞机的特别有效的设计，其中飞行器的机身不被集成在其中的氢罐分成两部分，可以布置在重心附近，并且基本上不增加额外的重量 的飞机。
-
公开(公告)号：US20150114975A1
公开(公告)日：2015-04-30
申请号：US14517028
申请日：2014-10-17
Applicant: Kevin L. Simmons , Kenneth I. Johnson , Curt A. Lavender , Norman L. Newhouse , Brian C. Yeggy
Inventor： Kevin L. Simmons , Kenneth I. Johnson , Curt A. Lavender , Norman L. Newhouse , Brian C. Yeggy
IPC: F17C1/08 , B21D26/031 , B21D26/029
CPC classification number: F17C1/08 , B21D26/021 , B21D51/18 , F17C2201/0152 , F17C2201/0161 , F17C2203/013 , F17C2209/2127 , F17C2221/033
Abstract: A non-cylindrical pressure vessel storage tank is disclosed. The storage tank includes an internal structure. The internal structure is coupled to at least one wall of the storage tank. The internal structure shapes and internally supports the storage tank. The pressure vessel storage tank has a conformability of about 0.8 to about 1.0. The internal structure can be, but is not limited to, a Schwarz-P structure, an egg-crate shaped structure, or carbon fiber ligament structure.
Abstract translation: 公开了一种非圆柱形压力容器储罐。 储罐包括内部结构。 内部结构耦合到储罐的至少一个壁。 内部结构形状和内部支撑储罐。 压力容器储罐具有约0.8至约1.0的一致性。 内部结构可以是但不限于施瓦茨-P结构，蛋壳状结构或碳纤维韧带结构。
-
-
-
-
-
-
-
-
-
Search Results
127
records
(took 0.015 seconds)
