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1. 发明专利

BR202019023570U2 veículo aéreo não tripulado alimentado por painéis solares flexíveis e bateria 未知
公开(公告)号：BR202019023570U2
公开(公告)日：2021-05-25
申请号：BR202019023570
申请日：2019-11-08
申请人： ALVARO DANIEL HERRERA ARROYO , ANDRE REZENDE DESSIMONI CARVALHO , ASES ATHENA SOC DE ENGENHARIA E CIENCIA LTDA , GABRIEL ANTONIO MARTINS PEREIRA DE MELO , JOSE ANTONIO FERREIRA BORGES , MARCELO BRAGA DOS SANTOS , ROBERTO MARTINS DE CASTRO NETO , ROGERIO MARQUES RODRIGUES FILHO
发明人： ART 6 § 4 DA LPI 9279/96 , ART 6 § 4 DA LPI 9279/96 , ART 6 § 4 DA LPI 9279/96 , ART 6 § 4 DA LPI 9279/96 , ART 6 § 4 DA LPI 9279/96 , ART 6 § 4 DA LPI 9279/96 , ART 6 § 4 DA LPI 9279/96
IPC分类号： G05D1/10 , B64C31/00
摘要： "veículo aéreo não tripulado alimentado por painéis solares flexíveis e bateria". a seguinte invenção compreende produto industrial caracterizado por fuselagem (1) foi otimizada de forma a gerar o menor arrasto possível ao mesmo tempo que se mantém rígida o suficiente para sustentar os equipamentos utilizados para o voo, para a aquisição de imagem e o motor. desta forma o perfil e as dimensões da asa (2), foram otimizados para que haja uma sustentação adequada ao funcionamento da aeronave e não exijam uma elevada área de painel solar (3). a empenagem vertical (4) e a empenagem horizontal (5) foram desenhadas e posicionadas para que a aeronave seja naturalmente estável, isto é, diante perturbações aerodinâmicas a aeronave se estabiliza com o menor esforço de comando. o motor da aeronave e a hélice utilizada (6) também foram otimizados para proporcionar o empuxo necessário com o menor consumo possível de energia elétrica, com aplicação em plantações de grandes e pequenos hectares, bem como, em áreas de grandes extensões em quilômetros, possuindo características como a versatilidade, modularidade, autonomia de voo de aproximadamente 8 (oito) horas; raio de alcance maior que 40 (quarenta) quilômetros; velocidade de voo superior à 50 km/h; fotogrametria de alta resolução; área coberta superior a 40 mil hectares em um único voo com baixa resolução de imagem ou 4 mil hectares com alta resolução de imagens e; capacidade de ser arremessado manualmente.

2. 发明授权

US07114916B2 Tailored turbulation for turbine blades 有权
标题翻译：涡轮叶片的定制紊流
公开(公告)号：US07114916B2
公开(公告)日：2006-10-03
申请号：US10774822
申请日：2004-02-09
申请人： Bryan P. Dube , William Abdel-Messeh , Daniel Herrera , Richard Page
发明人： Bryan P. Dube , William Abdel-Messeh , Daniel Herrera , Richard Page
IPC分类号： F03D11/00
CPC分类号： F01D5/187 , F05D2250/30 , F05D2260/2212 , F05D2260/22141
摘要： A turbine blade having improved cooling characteristics is provided. The turbine blade has an airfoil portion having a span, and at least one cooling passageway in the airfoil portion extending from a root portion of the airfoil portion to a tip portion of the airfoil portion. A plurality of turbulation promotion devices are placed in the at least one cooling passageway. The turbulation promotion devices have a P/e ratio which varies along the span of the airfoil portion, where P is the pitch between adjacent turbulation promotion devices and e is the height of the turbulation promotion devices.
摘要翻译：提供了具有改进的冷却特性的涡轮叶片。涡轮机叶片具有翼部，翼型部分具有跨度，翼型部分中的至少一个冷却通道从翼型部分的根部延伸到翼型部分的顶端部分。多个紊流促进装置被放置在至少一个冷却通道中。紊流促进装置具有沿翼型部分的跨度变化的P / e比，其中P是相邻的紊流促进装置之间的间距，e是紊流促进装置的高度。

3. 发明授权

US06997675B2 Turbulated hole configurations for turbine blades 有权
标题翻译：涡轮叶片的涡轮孔配置
公开(公告)号：US06997675B2
公开(公告)日：2006-02-14
申请号：US10774989
申请日：2004-02-09
申请人： Bryan P. Dube , William Abdel-Messeh , Daniel Herrera , Richard Page
发明人： Bryan P. Dube , William Abdel-Messeh , Daniel Herrera , Richard Page
IPC分类号： F01D5/08
CPC分类号： F01D5/187 , F05D2250/141 , F05D2250/25 , F05D2250/30 , F05D2250/314 , F05D2260/2212 , F05D2260/22141
摘要： A turbine blade having improved cooling has an airfoil with a root end and a tip end and at least one cooling passageway in the airfoil. Each cooling passageway extends from the root end to the tip end and has a circular cross-section. A plurality of turbulation promotion devices are arranged in each cooling passageway. Each of the turbulation promotion devices is arcuate in shape and circumscribes an arc less than 180 degrees.
摘要翻译：具有改进的冷却的涡轮机叶片具有具有根端和顶端的翼型和在翼型中的至少一个冷却通道。每个冷却通道从根端延伸到尖端并具有圆形横截面。在每个冷却通道中布置有多个紊流促进装置。每个紊流促进装置的形状都是弧形的，并且外接一个小于180度的弧。

4. 发明授权

US06964091B1 Wiper blade claw with crimping design 失效
标题翻译：雨刮片带压接设计
公开(公告)号：US06964091B1
公开(公告)日：2005-11-15
申请号：US10210749
申请日：2002-07-31
申请人： Daniel Herrera
发明人： Daniel Herrera
IPC分类号： A47L1/00 , B21D39/00 , B23P11/00 , B60S1/02 , B60S1/38
CPC分类号： B60S1/3801 , B23P11/005 , B60S2001/3812 , B60S2001/3813 , B60S2001/3836 , Y10T29/49908 , Y10T29/49922 , Y10T29/49924
摘要： A method of manufacturing a wiper blade for a windshield wiper system of motor vehicles with a yoke system for guiding an elongate wiper strip including a lip mounted on a carrier via a web is disclosed. The wiper blade and method of manufacturing the wiper blade includes the wiper strip installed with respect to the yoke system with the carrier extending through at least one claw of the yoke system. Each claw has opposing bendable sidewalls defining a generally U-shaped channel therebetween and located initially in an opened position with respect to one another during installation of the wiper strip. The opposing sidewalls of at least one claw are bent inwardly in two directions toward the longitudinal axis of the elongate wiper strip to a closed position, where one of the two directions of bending movement is at an angle other than perpendicular with respect to the longitudinal axis of the elongate wiper strip and the other of the two directions is toward a base wall extending between the opposing sidewalls of the U-shaped channel in the yoke system.
摘要翻译：公开了一种制造用于机动车辆的挡风玻璃刮水器系统的刮水片的方法，其具有用于引导细长刮水条的轭系统，所述轭状系统包括经由腹板安装在载体上的唇缘。刮水片和刮水片的制造方法包括相对于磁轭系统安装的刮片，载体延伸穿过轭系统的至少一个爪。每个爪具有相对的可弯曲的侧壁，其在它们之间限定大致U形的通道，并且在安装刮水条期间最初位于相对于彼此的打开位置。至少一个爪的相对的侧壁在两个方向上朝向细长刮水条的纵向轴线向内弯曲到闭合位置，其中两个弯曲方向之一处于与纵向轴线垂直的角度并且两个方向中的另一个朝向在轭系统中的U形通道的相对侧壁之间延伸的底壁。

5. 发明申请

US20050175454A1 Turbulated hole configurations for turbine blades 有权
标题翻译：涡轮叶片的涡轮孔配置
公开(公告)号：US20050175454A1
公开(公告)日：2005-08-11
申请号：US10774989
申请日：2004-02-09
申请人： Bryan Dube , William Abdel-Messeh , Daniel Herrera , Richard Page
发明人： Bryan Dube , William Abdel-Messeh , Daniel Herrera , Richard Page
IPC分类号： F01D5/18 , B63H1/14
CPC分类号： F01D5/187 , F05D2250/141 , F05D2250/25 , F05D2250/30 , F05D2250/314 , F05D2260/2212 , F05D2260/22141
摘要： A turbine blade having improved cooling has an airfoil with a root end and a tip end and at least one cooling passageway in the airfoil. Each cooling passageway extends from the root end to the tip end and has a circular cross-section. A plurality of turbulation promotion devices are arranged in each cooling passageway. Each of the turbulation promotion devices is arcuate in shape and circumscribes an arc less than 180 degrees.
摘要翻译：具有改进的冷却的涡轮机叶片具有具有根端和顶端的翼型和在翼型中的至少一个冷却通道。每个冷却通道从根端延伸到尖端并具有圆形横截面。在每个冷却通道中布置有多个紊流促进装置。每个紊流促进装置的形状都是弧形的，并且外接一个小于180度的弧。

6. 发明授权

US07361019B2 Dental instrument 失效
标题翻译：牙科仪器
公开(公告)号：US07361019B2
公开(公告)日：2008-04-22
申请号：US11294052
申请日：2005-12-05
申请人： Domingo V. Autran , Dominic F. Verderese , Hector Daniel Herrera
发明人： Domingo V. Autran , Dominic F. Verderese , Hector Daniel Herrera
IPC分类号： A61C19/04
CPC分类号： A61C19/04 , A61B5/107 , A61B5/4547
摘要： An instrument for determining the occlusal space between a person's upper and lower teeth thereby facilitating the formation of apparatus such as dentures and splints for removable positioning in the person's mouth.
摘要翻译：一种用于确定人的上牙和下牙之间的咬合空间的仪器，从而便于形成诸如假牙和夹板的装置，以便可拆卸地定位在人的口中。

7. 发明申请

US20050175452A1 Tailored turbulation for turbine blades 有权
标题翻译：涡轮叶片的定制紊流
公开(公告)号：US20050175452A1
公开(公告)日：2005-08-11
申请号：US10774822
申请日：2004-02-09
申请人： Bryan Dube , William Abdel-Messeh , Daniel Herrera , Richard Page
发明人： Bryan Dube , William Abdel-Messeh , Daniel Herrera , Richard Page
IPC分类号： F01D5/18 , B63H1/14
CPC分类号： F01D5/187 , F05D2250/30 , F05D2260/2212 , F05D2260/22141
摘要： A turbine blade having improved cooling characteristics is provided. The turbine blade has an airfoil portion having a span, and at least one cooling passageway in the airfoil portion extending from a root portion of the airfoil portion to a tip portion of the airfoil portion. A plurality of turbulation promotion devices are placed in the at least one cooling passageway. The turbulation promotion devices have a P/e ratio which varies along the span of the airfoil portion, where P is the pitch between adjacent turbulation promotion devices and e is the height of the turbulation promotion devices.
摘要翻译：提供了具有改进的冷却特性的涡轮叶片。涡轮机叶片具有翼部，翼型部分具有跨度，翼型部分中的至少一个冷却通道从翼型部分的根部延伸到翼型部分的顶端部分。多个紊流促进装置被放置在至少一个冷却通道中。紊流促进装置具有沿翼型部分的跨度变化的P / e比，其中P是相邻的紊流促进装置之间的间距，e是紊流促进装置的高度。

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