专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US07922957B2 Method for forming composite components and tool for use therein 有权
公开(公告)号：US07922957B2
公开(公告)日：2011-04-12
申请号：US12213931
申请日：2008-06-26
申请人： Simon Astwood , Steven Evans
发明人： Simon Astwood , Steven Evans
IPC分类号： B29C70/44
CPC分类号： B29C37/005 , B29C70/446
摘要： A method of making an aircraft component is provided, wherein the method comprises the steps of:providing a mould (1) for the receipt of a material (3) from which the aircraft component is to be made providing the mould with said material providing an intensification tool (14) in spaced relationship to the mould and heating the material, tool and mould so that the tool expands and applies pressure to the material and so as to form the component andwherein the linear coefficient of thermal expansion of the tool in a first direction is matched to the coefficient of thermal expansion of the component in the first direction, and the coefficient of thermal expansion of the tool in a second direction is greater than the coefficient of thermal expansion of the component in the second direction, the tool being provided with at least one contacting surface for contacting the material and through which pressure is applied to the material, the expansion of the tool in the second direction causing the at least one contacting surface to contact, and exert pressure on, the material.

2. 发明申请

US20090001630A1 Method for forming composite components and tool for use therein 有权
标题翻译：用于形成复合部件的方法和用于其中的工具
公开(公告)号：US20090001630A1
公开(公告)日：2009-01-01
申请号：US12213931
申请日：2008-06-26
申请人： Simon Astwood , Steven Evans
发明人： Simon Astwood , Steven Evans
IPC分类号： B28B11/10 , B29C59/02 , B29C70/44
CPC分类号： B29C37/005 , B29C70/446
摘要： A method of making an aircraft component is provided, wherein the method comprises the steps of: providing a mould (1) for the receipt of a material (3) from which the aircraft component is to be made providing the mould with said material providing an intensification tool (14) in spaced relationship to the mould and heating the material, tool and mould so that the tool expands and applies pressure to the material and so as to form the component and wherein the linear coefficient of thermal expansion of the tool in a first direction is matched to the coefficient of thermal expansion of the component in the first direction, and the coefficient of thermal expansion of the tool in a second direction is greater than the coefficient of thermal expansion of the component in the second direction, the tool being provided with at least one contacting surface for contacting the material and through which pressure is applied to the material, the expansion of the tool in the second direction causing the at least one contacting surface to contact, and exert pressure on, the material.
摘要翻译：提供了一种制造飞行器部件的方法，其中该方法包括以下步骤：提供用于接收材料（3）的模具（1），从该材料（3）制造飞行器部件，为模具提供所述材料，所述材料提供增强工具（14）与模具间隔开并加热材料，工具和模具，使得工具膨胀并对材料施加压力并且形成部件，并且其中工具的线性热膨胀系数第一方向与第一方向上的部件的热膨胀系数相匹配，并且工具在第二方向上的热膨胀系数大于部件在第二方向上的热膨胀系数，该工具为设置有至少一个接触表面，用于接触材料并通过该材料施加压力，工具在第二方向的膨胀使所述至少一个接触表面与所述材料接触并施加压力。

3. 发明授权

US08758664B2 Method for forming composite components and tool for use therein 失效
标题翻译：用于形成复合部件的方法和用于其中的工具
公开(公告)号：US08758664B2
公开(公告)日：2014-06-24
申请号：US12929792
申请日：2011-02-16
申请人： Simon Astwood , Steven Evans
发明人： Simon Astwood , Steven Evans
IPC分类号： B29C43/04
CPC分类号： B29C37/005 , B29C70/446
摘要： A method of making an aircraft component is provided, wherein the method comprises the steps of: providing a mold (1) for the receipt of a material (3) from which the aircraft component is to be made providing the mold with said material providing an intensification tool (14) in spaced relationship to the mold and heating the material, tool and mold so that the tool expands and applies pressure to the material and so as to form the component and wherein the linear coefficient of thermal expansion of the tool in a first direction is matched to the coefficient of thermal expansion of the component in the first direction, and the coefficient of thermal expansion of the tool in a second direction is greater than the coefficient of thermal expansion of the component in the second direction, the tool being provided with at least one contacting surface for contacting the material and through which pressure is applied to the material, the expansion of the tool in the second direction causing the at least one contacting surface to contact, and exert pressure on, the material.
摘要翻译：提供了一种制造飞行器部件的方法，其中该方法包括以下步骤：提供用于接收材料（3）的模具（1），从该材料（3）制造飞行器部件，为模具提供所述材料，所述材料提供增强工具（14）与模具间隔开并加热材料，工具和模具，使得工具膨胀并对材料施加压力并且形成部件，并且其中工具的线性热膨胀系数第一方向与第一方向上的部件的热膨胀系数相匹配，并且工具在第二方向上的热膨胀系数大于部件在第二方向上的热膨胀系数，该工具为设置有至少一个接触表面，用于接触材料并通过该材料施加压力，使工具在第二方向上的膨胀导致t 他至少有一个接触表面与材料接触并施加压力。

4. 发明申请

US20110147994A1 Method for forming composite components and tool for use therein 失效
标题翻译：用于形成复合部件的方法和用于其中的工具
公开(公告)号：US20110147994A1
公开(公告)日：2011-06-23
申请号：US12929792
申请日：2011-02-16
申请人： Simon Astwood , Steven Evans
发明人： Simon Astwood , Steven Evans
IPC分类号： B29C43/04
CPC分类号： B29C37/005 , B29C70/446
摘要： A method of making an aircraft component is provided, wherein the method comprises the steps of:providing a mould (1) for the receipt of a material (3) from which the aircraft component is to be made providing the mould with said material providing an intensification tool (14) in spaced relationship to the mould and heating the material, tool and mould so that the tool expands and applies pressure to the material and so as to form the component and wherein the linear coefficient of thermal expansion of the tool in a first direction is matched to the coefficient of thermal expansion of the component in the first direction, and the coefficient of thermal expansion of the tool in a second direction is greater than the coefficient of thermal expansion of the component in the second direction, the tool being provided with at least one contacting surface for contacting the material and through which pressure is applied to the material, the expansion of the tool in the second direction causing the at least one contacting surface to contact, and exert pressure on, the material.
摘要翻译：提供了一种制造飞行器部件的方法，其中该方法包括以下步骤：提供用于接收材料（3）的模具（1），从该材料（3）制造飞行器部件，为模具提供所述材料，所述材料提供增强工具（14）与模具间隔开并加热材料，工具和模具，使得工具膨胀并对材料施加压力并且形成部件，并且其中工具的线性热膨胀系数第一方向与第一方向上的部件的热膨胀系数相匹配，并且工具在第二方向上的热膨胀系数大于部件在第二方向上的热膨胀系数，该工具为设置有至少一个接触表面，用于接触材料并通过该材料施加压力，工具在第二方向的膨胀使所述至少一个接触表面与所述材料接触并施加压力。

5. 发明授权

US08963359B2 Apparatus and method for co-generation of electricity 有权
标题翻译：用于共同发电的装置和方法
公开(公告)号：US08963359B2
公开(公告)日：2015-02-24
申请号：US13235359
申请日：2011-09-17
申请人： Steven Evans , Steven Evans, II , Frank D. Clark
发明人： Steven Evans , Steven Evans, II , Frank D. Clark
IPC分类号： F03B13/00 , F01D15/10 , F03D9/00
CPC分类号： F01D15/10 , F01D1/20 , F01D13/02 , F01D17/085 , F03D9/11 , F03D9/25 , F05B2220/602 , F05D2220/62 , Y02B10/30 , Y02E10/725
摘要： A co-generation apparatus for the generation of electricity from an external source of forced air is described in which the co-generation apparatus comprises a turbine, a generator, a co-generation control unit, and an adjustable standoff. The turbine is connected to the generator for the production of electricity. The generator interface electrically connects the generator to an electrical system. The co-generation control unit is connected to the turbine and generator interface. The forced air drives the turbine. The turbine can be positioned in a turbine housing that receives the forced air. An adjustable standoff is connected to the turbine. The standoff adjusts the position of the turbine relative to the forced air.
摘要翻译：描述了用于从外部强制空气源产生电力的联合发电装置，其中共发电装置包括涡轮机，发电机，共发电控制单元和可调节支架。涡轮机连接到发电机用于生产电力。发电机接口将发电机电连接到电气系统。联合发电控制单元连接到涡轮和发电机接口。强制空气驱动涡轮。涡轮机可以定位在接收强制空气的涡轮机壳体中。可调节的支座连接到涡轮机。间隔调整涡轮机相对于强制空气的位置。

6. 发明申请

US20150218960A1 APPARATUS AND METHOD FOR CO-GENERATION 审中-公开
标题翻译：装置和方法联合生成
公开(公告)号：US20150218960A1
公开(公告)日：2015-08-06
申请号：US14608628
申请日：2015-01-29
申请人： Steven Evans , Steven Evans, II , Frank Clark
发明人： Steven Evans , Steven Evans, II , Frank Clark
IPC分类号： F01D15/10 , F01D13/02 , F01D17/08 , F01D1/20
CPC分类号： F01D15/10 , F01D1/20 , F01D13/02 , F01D17/085 , F03D9/11 , F03D9/25 , F05B2220/602 , F05D2220/62 , Y02B10/30 , Y02E10/725
摘要： A co-generation apparatus for the generation of electricity from an external source of forced air is described in which the co-generation apparatus comprises a turbine, a generator, a co-generation control unit, and an adjustable standoff. The turbine is connected to the generator for the production of electricity. The generator interface electrically connects the generator to an electrical system. The co-generation control unit is connected to the turbine and generator interface. The forced air drives the turbine. The turbine can be positioned in a turbine housing that receives the forced air. An adjustable standoff is connected to the turbine. The standoff adjusts the position of the turbine relative to the forced air.
摘要翻译：描述了用于从外部强制空气源产生电力的联合发电装置，其中共发电装置包括涡轮机，发电机，共发电控制单元和可调节支架。涡轮机连接到发电机用于生产电力。发电机接口将发电机电连接到电气系统。联合发电控制单元连接到涡轮和发电机接口。强制空气驱动涡轮。涡轮机可以定位在接收强制空气的涡轮机壳体中。可调节的支座连接到涡轮机。间隔调整涡轮机相对于强制空气的位置。

7. 发明申请

US20120091710A1 APPARATUS AND METHOD FOR CO-GENERATION 审中-公开
标题翻译：装置和方法联合生成
公开(公告)号：US20120091710A1
公开(公告)日：2012-04-19
申请号：US13235359
申请日：2011-09-17
申请人： Steven Evans , Steven Evans, II , Frank D. Clark
发明人： Steven Evans , Steven Evans, II , Frank D. Clark
IPC分类号： H02P9/04 , H02K7/18
CPC分类号： F01D15/10 , F01D1/20 , F01D13/02 , F01D17/085 , F03D9/11 , F03D9/25 , F05B2220/602 , F05D2220/62 , Y02B10/30 , Y02E10/725
摘要： A co-generation apparatus for the generation of electricity from an external source of forced air is described in which the co-generation apparatus comprises a turbine, a generator, a co-generation control unit, and an adjustable standoff. The turbine is connected to the generator for the production of electricity. The generator interface electrically connects the generator to an electrical system. The co-generation control unit is connected to the turbine and generator interface. The forced air drives the turbine. The turbine can be positioned in a turbine housing that receives the forced air. An adjustable standoff is connected to the turbine. The standoff adjusts the position of the turbine relative to the forced air.
摘要翻译：描述了用于从外部强制空气源产生电力的联合发电装置，其中共发电装置包括涡轮机，发电机，共发电控制单元和可调节支架。涡轮机连接到发电机用于生产电力。发电机接口将发电机电连接到电气系统。联合发电控制单元连接到涡轮和发电机接口。强制空气驱动涡轮。涡轮机可以定位在接收强制空气的涡轮机壳体中。可调节的支座连接到涡轮机。间隔调整涡轮机相对于强制空气的位置。

8. 发明授权

US09366152B2 Apparatus and method for co-generation of electrical energy from an external source of forced air 有权
标题翻译：用于从外部强制空气源共同生成电能的装置和方法
公开(公告)号：US09366152B2
公开(公告)日：2016-06-14
申请号：US14608628
申请日：2015-01-29
申请人： Steven Evans , Steven Evans, II , Frank Clark
发明人： Steven Evans , Steven Evans, II , Frank Clark
IPC分类号： F01D15/10 , F03D9/00 , F01D1/20 , F01D13/02 , F01D17/08
CPC分类号： F01D15/10 , F01D1/20 , F01D13/02 , F01D17/085 , F03D9/11 , F03D9/25 , F05B2220/602 , F05D2220/62 , Y02B10/30 , Y02E10/725
摘要： A co-generation apparatus for the generation of electricity from an external source of forced air is described in which the co-generation apparatus comprises a turbine, a generator, a co-generation control unit, and an adjustable standoff. The turbine is connected to the generator for the production of electricity. The generator interface electrically connects the generator to an electrical system. The co-generation control unit is connected to the turbine and generator interface. The forced air drives the turbine. The turbine can be positioned in a turbine housing that receives the forced air. An adjustable standoff is connected to the turbine. The standoff adjusts the position of the turbine relative to the forced air.
摘要翻译：描述了用于从外部强制空气源产生电力的联合发电装置，其中共发电装置包括涡轮机，发电机，共发电控制单元和可调节支架。涡轮机连接到发电机用于生产电力。发电机接口将发电机电连接到电气系统。联合发电控制单元连接到涡轮和发电机接口。强制空气驱动涡轮。涡轮机可以定位在接收强制空气的涡轮机壳体中。可调节的支座连接到涡轮机。间隔调整涡轮机相对于强制空气的位置。

9. 发明申请

US20200230474A1 Golf Tee Tethering Assembly 审中-公开
公开(公告)号：US20200230474A1
公开(公告)日：2020-07-23
申请号：US16253298
申请日：2019-01-22
申请人： Steven Evans
发明人： Steven Evans
IPC分类号： A63B57/12 , A63B69/36
摘要： A golf tee tethering assembly for inhibiting a rubber mat tee from flying away during golf practice includes a rubber mat tee that is positionable on a rubber golfing mat to have a golf ball positioned thereon for striking. A washer is positioned around the rubber mat tee and a tether is coupled to the washer. A fastener is coupled to the tether on an opposite end of the tether from the ring. The fastener releasably engages a shaft of a golf club such that the rubber mat tee is retained on the golf club. The golf club is laid on the rubber golf mat and the rubber mat tee is positioned at a chosen spot on the rubber golf mat. Thus, the tether inhibits the rubber mat tee from flying away when the golf ball is struck from the rubber mat tee.

10. 发明申请

US20130288006A1 LASER-ENGRAVEABLE ELEMENTS AND METHOD OF USE 审中-公开
标题翻译：激光可雕刻元件和使用方法
公开(公告)号：US20130288006A1
公开(公告)日：2013-10-31
申请号：US13456301
申请日：2012-04-26
申请人： Anna C. Greene , Christine J. Landry-Coltrain , Steven Evans
发明人： Anna C. Greene , Christine J. Landry-Coltrain , Steven Evans
IPC分类号： B32B7/02 , B32B27/18 , C08L27/18 , B05D3/02 , B29C35/08 , B32B3/30 , B29C35/02
CPC分类号： B41C1/1025 , B41C1/05 , B41C1/1033 , B41M1/10 , B41N1/12 , B41N1/22 , C08K9/04 , H05K3/1275 , Y10T428/24479 , Y10T428/24612 , Y10T428/25 , Y10T428/269 , Y10T428/3154
摘要： A composition comprises a fluoropolymer such as an elastomeric fluoropolymer and at least 1 weight % of a fluoro-functionalized near-infrared radiation absorber. This composition can be formed into laser-engraveable layers for various elements that can be laser-engraved to provide relief images. The resulting laser-engraved elements can take various forms including flexographic printing members, and can be used to apply various inks to receiver materials in an imagewise fashion.
摘要翻译：组合物包含含氟聚合物如弹性体氟聚合物和至少1重量％的氟官能化的近红外辐射吸收剂。该组合物可以形成激光雕刻层，用于可被激光雕刻以提供浮雕图像的各种元件。所得到的激光雕刻元件可以采取各种形式，包括柔性版印刷构件，并且可以用于以成像方式将各种油墨应用于接收器材料。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式