公开(公告)号：EP1833721A4

公开(公告)日：2010-05-05

申请号：EP05857018

申请日：2005-11-22

Applicant: HELOU ELIE JR

Inventor： HELOU ELIE JR

IPC: B64C1/22 ,  B64C39/02

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: In one embodiment, an aircraft for transporting at least one cargo container is disclosed. The aircraft comprises a forward fuselage, an empennage, a beam structure, and mounts to detachably and structurally engage the at least one cargo container with the beam structure. The beam structure is disposed between the forward fuselage and the empennage and the beam structure configured to receive the at least one cargo container. The beam structure and structurally engaged cargo container provide sufficient structural rigidity to support the aircraft in flight.

公开(公告)号：CA2589813A1

公开(公告)日：2006-08-10

申请号：CA2589813

申请日：2005-11-22

Applicant: HELOU ELIE JR

Inventor： HELOU ELIE JR

IPC: B64C1/22

Abstract: In one embodiment, an aircraft for transporting at least one cargo container is disclosed. The aircraft comprises a forward fuselage, an empennage, a beam structure, and mounts to detachably and structurally engage the at least one cargo container with the beam structure. The beam structure is disposed between the forward fuselage and the empennage and the beam structure configured to receive the at least one cargo container. The beam structure and structurally engaged cargo container provide sufficient structural rigidity to support the aircraft in flight.

公开(公告)号：EP2205484A4

公开(公告)日：2011-11-16

申请号：EP08848221

申请日：2008-10-07

Applicant: HELOU ELIE JR

Inventor： HELOU ELIE JR

IPC: B64C1/22

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

公开(公告)号：CA2589813C

公开(公告)日：2014-04-22

申请号：CA2589813

申请日：2005-11-22

Applicant: HELOU ELIE JR

Inventor： HELOU ELIE JR

IPC: B64C1/22

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.

公开(公告)号：CA2745554A1

公开(公告)日：2012-01-09

申请号：CA2745554

申请日：2011-07-07

Applicant: HELOU ELIE JR

Inventor： HELOU ELIE JR

IPC: B64D9/00 ,  B64D47/00

Abstract: An aircraft for transporting a plurality of cargo containers comprising a forward fairing, an empennage and a spine disposed between the forward fairing and the empennage. The spine is made of a lightweight structure such that the aircraft has insufficient rigidity to withstand bending and tortional loads in flight. A cargo assembly comprising a plurality of modular cargo units is structurally and detachably mounted onto the spine to provide the additional structure to the aircraft required for it to fully withstand the bending and tortional loads of the aircraft in flight. Mounts may be provided to detachably engage the cargo assembly to the spine of the aircraft.

公开(公告)号：MX2010004964A

公开(公告)日：2010-05-27

申请号：MX2010004964

申请日：2008-10-07

Applicant: HELOU ELIE JR

Inventor： HELOU ELIE JR

IPC: B64D9/00

Abstract: Un método de consumo eficiente del combustible de transportación de carga a una ubicación deseada por medio de una aeronave; el método comprende determinar el peso de la carga con la capacidad de ser transportada en un contenedor único, seleccionar un contenedor que tiene una capacidad de carga suficiente para soportar la carga con base en el peso determinado de la carga, y llenar el contenedor seleccionado con la carga; el contenedor lleno es cargado en una ubicación sobre el eje de la aeronave en relación con el CG de la aeronave con base en el peso del contenedor lleno para permanecer dentro del intervalo CG aceptable para la aeronave; los contenedores llenos que tienen mayor peso son colocados sobre el eje en o adyacente al CG de la aeronave y los contenedores llenos que tienen menor peso son colocados más lejos del CG de la aeronave; los contenedores proporcionan la fuerza y rigidez al eje para sostener las cargas de flexión y torsión durante el vuelo.

公开(公告)号：WO2009105563A2

公开(公告)日：2009-08-27

申请号：PCT/US2009034548

申请日：2009-02-19

Applicant: BIOSPHERE IND LLC ,  HELOU ELIE JR

Inventor： HELOU ELIE JR

IPC: B65D43/00

CPC classification number: B65D65/463 ,  B65D43/0202 ,  B65D65/466 ,  B65D81/3453 ,  B65D2543/00666 ,  B65D2543/00703 ,  B65D2543/00731 ,  B65D2543/00805 ,  Y02A40/961 ,  Y02W90/11 ,  Y02W90/13

Abstract: One embodiment of the present invention provides a novel packaging article, which includes a cover and a base having non-edge localized connecting structures, such as, a protrusion and a receptacle cavity. The cover and the base may have different thermal expansion coefficients such that, when subject to heating (e.g., microwave heating) or cooling (e.g., refrigerate storage), the cover and the base do not expand or shrink to the same degree. Furthermore, the cover and/or the base may comprise a biodegradable or edible material, such as, without limitation, starch.

Abstract translation: 本发明的一个实施例提供了一种新颖的包装物品，其包括具有非边缘局部连接结构（例如突起和容纳腔）的盖和底座。 盖子和基座可以具有不同的热膨胀系数，使得当受到加热（例如微波加热）或冷却（例如冷藏）时，盖子和基座不会膨胀或收缩到相同的程度。 此外，盖子和/或底座可以包括生物可降解或可食用材料，例如但不限于淀粉。

公开(公告)号：WO2008083247A2

公开(公告)日：2008-07-10

申请号：PCT/US2007088989

申请日：2007-12-27

Applicant: BIOSPHERE HOLDINGS CORP ,  HELOU ELIE JR ,  DELLINGER DAVID

Inventor： HELOU ELIE JR ,  DELLINGER DAVID

IPC: A23L1/00

CPC classification number: B29C47/12 ,  A21C11/16 ,  B29C47/0016 ,  B29C47/003 ,  B29C47/20 ,  B29C47/76 ,  B29K2003/00 ,  Y10S425/812

Abstract: In one embodiment of the invention a mold system and method of use are provided such that aqueous starch-based compositions and baked goods articles that use the conversion of water to steam may be produced using an extruder that allows the venting of such gases and/or steam. The extruder is vented in such a way as to allow steam to escape, but retain the composition until the exit end.

Abstract translation: 在本发明的一个实施方案中，提供了一种模具系统和使用方法，使得使用将水转化成蒸汽的水性淀粉基组合物和烘焙食品可以使用挤出机来生产，所述挤出机允许排放这种气体和/或 蒸汽。 挤出机以允许蒸汽逸出的方式排放，但保留组合物直到出口端。

公开(公告)号：WO2005021633A2

公开(公告)日：2005-03-10

申请号：PCT/US2004027824

申请日：2004-08-26

Applicant: BIOSPHERE IND CORP ,  HELOU ELIE JR ,  DELLINGER DAVID

Inventor： HELOU ELIE JR ,  DELLINGER DAVID

IPC: C08L20060101 ,  C12C1/027 ,  C08L

CPC classification number: C08L3/02 ,  C08L1/02 ,  C08L89/00 ,  C08L89/005 ,  C08L2666/26

Abstract: The present invention relates to a composition for use in making a starch-based food or beverage container, the formulation allowing the container to be water resistant for a usable amount of time without the need for coatings or similar. An embodiment of the formulation comprising water, native and pregelatinized starch, an insolubilizing compound, proteins or natural polymeric compounds, fibers, a wax emulsion, and a fiber-sizing agent.

Abstract translation: 本发明涉及一种用于制备淀粉类食品或饮料容器的组合物，该制剂允许容器在不需要涂层或类似物的情况下耐水可用的时间量。 包含水，天然和预胶化淀粉，不溶化合物，蛋白质或天然聚合物，纤维，蜡乳液和纤维施胶剂的制剂的一个实施方案。

公开(公告)号：CA2747596A1

公开(公告)日：2012-01-29

申请号：CA2747596

申请日：2011-07-29

Applicant: HELOU ELIE JR

Inventor： HELOU ELIE JR

IPC: B64D1/08

Abstract: A system for loading and unloading a cargo assembly onto and from an aircraft. The system comprises an aircraft and a moveable platform. The aircraft comprises a forward fairing, an aft fairing, a spine disposed between the forward fairing and the aft fairing and a plurality of mounts coupled to the spine and configured to structurally engage the cargo container onto the spine. The aft fairing is movable between a fixed position for flight and an open position for at least loading and unloading of the cargo assembly. The aircraft is configured such that an unobstructed passageway is provided in an area underneath the spine during loading or unloading of the cargo assembly. An aft access is provided when the aft fairing is moved to the open position. The moveable platform is used to maneuver the cargo assembly for loading and unloading onto and from the spine, respectively.