公开(公告)号：US20100116932A1

公开(公告)日：2010-05-13

申请号：US12636381

申请日：2009-12-11

Applicant: ELIE HELOU, JR.

Inventor： ELIE HELOU, JR.

IPC: B64C39/02 ,  B64C1/06 ,  B64C1/20

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 ,  Y02T50/43

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.

Abstract translation: 在一个实施例中，公开了一种用于运输至少一个货物集装箱的飞机。 飞行器包括前机身，尾翼，梁结构，以及可拆卸地和结构地接合具有梁结构的至少一个货物集装箱的安装件。 梁结构设置在前机身和尾翼之间，梁结构被配置成接收至少一个货物集装箱。 梁结构和结构上接合的货物集装箱提供足够的结构刚度以支持飞行中的飞机。

公开(公告)号：US20140092703A1

公开(公告)日：2014-04-03

申请号：US13632291

申请日：2012-10-01

Applicant: ELIE HELOU, JR. ,  Heriberto Alvarado

Inventor： ELIE HELOU, JR. ,  Heriberto Alvarado

IPC: B01F13/00

CPC classification number: B01F15/0224 ,  B01F13/0022 ,  B01F15/0215 ,  B65D51/28 ,  B65D81/3216 ,  B65D81/3222

Abstract: A multi-component mixing device comprising an outer container and an inner vessel. The outer container comprises a closed end, a mouth and a peripheral wall between said closed end and said mouth. The inner vessel is disposed within said outer container and the inner vessel comprises a top portion, a bottom portion and a peripheral side wall between said top portion and bottom portion. The peripheral side wall of the inner vessel is defined by first and second sections, which are slidably engaged to one another between a first position and a second position. In the first position, the inner vessel defines an enclosed cavity and in the second position, the inner vessel comprises a first opening corresponding to the enclosed cavity.

Abstract translation: 一种多组分混合装置，包括外部容器和内部容器。 外部容器包括封闭端，口部和位于所述封闭端和所述口部之间的周壁。 内容器设置在所述外容器内，内容器包括位于所述顶部和底部之间的顶部，底部和周边侧壁。 内容器的周边侧壁由第一和第二部分限定，第一和第二部分在第一位置和第二位置之间可滑动地彼此接合。 在第一位置，内部容器限定封闭空腔，并且在第二位置，内部容器包括对应于封闭空腔的第一开口。

公开(公告)号：US20090026314A1

公开(公告)日：2009-01-29

申请号：US11782850

申请日：2007-07-25

Applicant: ELIE HELOU, JR.

Inventor： ELIE HELOU, JR.

IPC: B64C1/20 ,  B64C1/00

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 ,  Y02T50/43

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定位在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。