公开(公告)号：MX2011007339A

公开(公告)日：2012-01-23

申请号：MX2011007339

申请日：2011-07-08

Applicant: HELOU ELIE JR

Inventor： HELOU ELIE JR

IPC: B64C1/20

Abstract: Una aeronave para transportar una pluralidad de contenedores de carga que comprende una envoltura aerodinámica delantera, una cola de avión y una columna dispuesta entre la envoltura aerodinámica delantera y la cola de avión; la columna está elaborada de una estructura de peso ligero, de manera que la aeronave tiene una rigidez insuficiente para soportar las cargas de doblado y torsión durante el vuelo; un ensamble de carga que comprende una pluralidad de unidades de carga modulares está montado en forma estructural y desmontable sobre la columna para proporcionar la estructura adicional a la aeronave, requerida para que esta soporte por completo las cargas de doblado y torsión de la aeronave durante el vuelo; los soportes pueden ser provistos para acoplar de manera que se puede desmontar el ensamble de carga a la columna de la aeronave.

公开(公告)号：CA2704678A1

公开(公告)日：2009-05-14

申请号：CA2704678

申请日：2008-10-07

Applicant: HELOU ELIE JR

Inventor： HELOU ELIE JR

IPC: B64C1/22

Abstract: A fuel-efficient method for transporting cargo to a desired location via an aircraft. The method comprises determining the weight of the cargo capable of being transported in a single container, selecting a container having a sufficient weight capacity to support the cargo based on the determined weight of the cargo, and filing the selected container with the cargo. The filled container is loaded onto a location on the aircraft beam relative to the aircraft's CG based on the weight of the filled container to stay within the acceptable CG range for the aircraft. The filled containers having the greater weight are positioned on the beam at or adjacent to the aircraft's CG and the filled containers having lower weight are positioned farther from the aircraft's CG. The containers provide strength and rigidity to the beam to sustain the bending and torsional loads in flight.

公开(公告)号：MX2007007077A

公开(公告)日：2007-11-14

申请号：MX2007007077

申请日：2005-11-22

Applicant: HELOU ELIE JR

Inventor： HELOU ELIE JR

IPC: B64D9/00

Abstract: Una aeronave para llevar al menos un contendor de carga rigido incluye una estructura de larguero con un fuselaje delantero unido al extremo delantero de la estructura de larguero y un empenaje unido al extremo posterior de la estructura de larguero; alas y motores se montan en relacion con la estructura de larguero y una guarda aerodinamica crea una bahia de carga capas de recibir contenedores de carga intermodales de tamano estandar; contenedores de carga intermodal de carga ligera y estructura rigida se posicionan dentro de la mayoria de carga y se montan de forma segura sobre esta; la estructura de larguero esta disenada para soportar vuelos, despegues y aterrizajes cuando la aeronave esta vacia pero requiere la mayor resistencia de los contenedores montados de forma segura a la estructura de larguero cuando la aeronave despega; la aeronave se contempla como avion a control remoto.

公开(公告)号：WO2012129524A3

公开(公告)日：2014-05-01

申请号：PCT/US2012030423

申请日：2012-03-23

Applicant: BIOSPHERE SPIRITS LLC ,  HELOU ELIE JR

Inventor： HELOU ELIE JR

IPC: B65D25/08

CPC classification number: B65D81/3222 ,  B65B31/00 ,  B65B2230/02

Abstract: A mixing container comprising an outer vessel, one or more inner vessels, and a lid. The outer vessel comprises a bottom, an open mouth and a peripheral sidewall between the open mouth and the bottom. The one or more inner vessels each have an end, an open mouth and a peripheral sidewall between the end and the open mouth. The lid is configured to be removably coupled to the open mouth of the outer vessel and the lid comprises an outer surface and an inner surface coupled to the ends of the one or more inner vessels. A seal is formed between the open mouth of each one of the one or more inner vessels and the bottom of the outer vessel when the lid is coupled to the open mouth of the outer vessel.

Abstract translation: 混合容器，其包括外容器，一个或多个内容器和盖。 外容器包括底部，开口和在开口和底部之间的周边侧壁。 一个或多个内部容器各自具有端部，开口和在端部和开口之间的周边侧壁。 盖被构造成可移除地联接到外部容器的开口，并且盖包括外表面和连接到一个或多个内容器的端部的内表面。 当盖子连接到外部容器的开口时，在一个或多个内部容器中的每一个的敞开的口部和外部容器的底部之间形成密封件。

公开(公告)号：WO2009061576A2

公开(公告)日：2009-05-14

申请号：PCT/US2008079066

申请日：2008-10-07

Applicant: HELOU ELIE JR

Inventor： HELOU ELIE JR

IPC: B64D9/00

CPC classification number: B64C1/10 ,  B64C1/061 ,  B64C1/065 ,  B64C1/22 ,  B64C17/08 ,  B64C39/02 ,  B64C39/024 ,  B64C2201/128 ,  B64C2211/00 ,  B64D9/00 ,  B64D13/02 ,  B64D13/06 ,  B64D2013/0629 ,  Y02T50/44 ,  Y02T50/46 ,  Y02T50/56

Abstract: A fuel-efficient method for transporting cargo to a desired location via an aircraft. The method comprises determining the weight of the cargo capable of being transported in a single container, selecting a container having a sufficient weight capacity to support the cargo based on the determined weight of the cargo, and filing the selected container with the cargo. The filled container is loaded onto a location on the aircraft beam relative to the aircraft's CG based on the weight of the filled container to stay within the acceptable CG range for the aircraft. The filled containers having the greater weight are positioned on the beam at or adjacent to the aircraft's CG and the filled containers having lower weight are positioned farther from the aircraft's CG. The containers provide strength and rigidity to the beam to sustain the bending and torsional loads in flight.

Abstract translation: 一种用于将货物经由飞机运输到所需位置的节省燃料的方法。 该方法包括确定能够在单个容器中运输的货物的重量，选择具有足够重量容量的容器以基于所确定的货物重量来支撑货物，并且将所选择的容器与货物一起备存。 填充的容器基于填充的容器的重量而相对于飞机的CG装载在飞机梁上的位置上，以保持在飞行器的可接受的CG范围内。 具有较大重量的填充容器位于或靠近飞行器CG的梁上，并且具有较低重量的填充容器位于离飞机CG更远的位置。 容器为梁提供强度和刚度，以维持飞行中的弯曲和扭转载荷。

公开(公告)号：WO2006083368A3

公开(公告)日：2007-06-14

申请号：PCT/US2005042674

申请日：2005-11-22

Applicant: HELOU ELIE JR

Inventor： HELOU ELIE JR

IPC: B64C1/22

CPC classification number: B64C1/10 ,  B64C1/00 ,  B64C1/061 ,  B64C1/065 ,  B64C39/02 ,  B64C39/024 ,  B64C2001/0072 ,  B64C2201/021 ,  B64C2201/048 ,  B64C2201/086 ,  B64C2201/104 ,  B64C2201/128 ,  B64C2201/162 ,  B64C2201/167 ,  B64C2211/00 ,  Y02T50/433

Abstract: An aircraft for carrying at least one rigid cargo container includes a beam structure with a forward fuselage attached to the forward end of the beam structure and an empennage attached to the rearward end of the beam structure. Wings and engines are mounted relative to the beam structure and a fairing creates a cargo bay able to receive standard sized intermodal cargo containers. Intermodal cargo containers of light construction and rigid structure are positioned within the cargo bay and securely mounted therein. The beam structure is designed to support flight, takeoffs and landings when the aircraft is empty but requires the added strength of the containers securely mounted to the beam structure when the aircraft is loaded. The aircraft is contemplated to be a drone.

Abstract translation: 用于承载至少一个刚性货物集装箱的飞机包括具有附接到梁结构的前端的前机身的梁结构和附接到梁结构的后端的后轮。 翼和发动机相对于梁结构安装，整流罩产生能够接收标准尺寸的联运货物集装箱的货舱。 轻型结构和刚性结构的多式联运集装箱位于货舱内并牢固地安装在货舱内。 梁结构设计用于在飞机空置时支持飞行，起飞和着陆，但是当飞机加载时，需要将集装箱的强度牢固地安装到梁结构上。 飞机被认为是无人机。

公开(公告)号：WO2005002341A3

公开(公告)日：2007-03-08

申请号：PCT/US2004019619

申请日：2004-06-18

Applicant: BIOSPHERE IND CORP ,  HELOU ELIE JR ,  DELLINGER DAVID A ,  KANE RYAN M ,  SPRADLIN MATT A

Inventor： HELOU ELIE JR ,  DELLINGER DAVID A ,  KANE RYAN M ,  SPRADLIN MATT A

IPC: A23P1/10 ,  A21B3/13 ,  A21B5/02 ,  A47J37/00 ,  B29C43/00

CPC classification number: A21B3/139 ,  A21B3/13 ,  A21B5/026 ,  Y10S425/812

Abstract: The present invention relates to a method for producing baked goods and a mold apparatus having a cavity in a desired shape for use in said method, the mold apparatus comprising a gap that allows for venting of vapor produced during heating or baking of a mixture in the mold apparatus but does not allow any significant amount of the mixture to escape from the cavity of the mold apparatus via the gaps.

Abstract translation: 本发明涉及一种生产烘焙食品的方法和一种具有所需形状的空腔的模具装置，用于所述方法，该模具装置包括一个间隙，该间隙允许在该混合物的加热或烘烤过程中产生的蒸气排出 模具装置，但不允许任何大量的混合物经由间隙从模具装置的空腔逸出。