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公开(公告)号：US08387911B2
公开(公告)日：2013-03-05
申请号：US12179690
申请日：2008-07-25
Applicant: Daniel Ross Collette
Inventor： Daniel Ross Collette
IPC: B64C29/00
CPC classification number: B64C39/024 , B64C27/20 , B64C2201/027 , B64C2201/048 , B64C2201/088 , B64C2201/108 , B64C2201/126 , B64C2201/162
Abstract: A ducted fan core for an unmanned aerial vehicle is provided that accommodates a wide variety of payloads. The ducted fan core comprises a frame, attached to which are an engine, gearbox assembly, fan, and a plurality of control vanes. A first surface on the frame comprises a plurality of connects or electrical traces. The plurality of connects are used to removably attach a variety of pods carrying various payloads. Thus, a wide variety of payloads may be delivered using the same unmanned aerial vehicle, simply by removing and attaching different pods to a fixed vehicle core. These pods may be shaped so as to form part of the vehicle exterior, and when the pods are attached to the frame, they enhance the aerodynamics of the vehicle.
Abstract translation: 提供用于无人驾驶飞行器的管道风扇芯，其容纳各种有效载荷。 风扇风扇芯包括框架，附接到发动机，变速箱组件，风扇和多个控制叶片。 框架上的第一表面包括多个连接或电迹线。 多个连接用于可拆卸地附接携带各种有效载荷的各种吊舱。 因此，可以简单地通过将不同的荚移除并附接到固定的车辆核心，使用相同的无人驾驶飞行器来传送各种有效载荷。 这些荚可以成形为形成车辆外部的一部分，并且当荚附接到框架时，它们增强了车辆的空气动力学。
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2.发明授权Structural ring interconnect printed circuit board assembly for a ducted fan unmanned aerial vehicle 失效用于风扇无人驾驶飞行器的结构环互连印刷电路板组件公开(公告)号：US08242623B2
公开(公告)日：2012-08-14
申请号：US12270196
申请日：2008-11-13
Applicant: Michael Lucero , Daniel Ross Collette , David Axtman
Inventor： Michael Lucero , Daniel Ross Collette , David Axtman
IPC: H01R12/00
CPC classification number: H05K1/02 , B64C2201/027 , H05K1/14 , H05K2201/09027 , H05K2201/09063
Abstract: A structural ring interconnect printed circuit board assembly for a ducted fan unmanned aerial vehicle that comprises a printed circuit board attached to a core vehicle body, wherein the printed circuit board conforms to the shape of the core vehicle body's airframe skirt, and wherein the printed circuit board provides structural integrity to the core vehicle body.
Abstract translation: 一种用于管道风扇无人机的结构环互连印刷电路板组件，其包括附接到核心车体的印刷电路板，其中印刷电路板符合核心车身的机身裙部的形状，并且其中印刷电路 主板为核心车身提供了结构完整性。
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公开(公告)号：US20100021288A1
公开(公告)日：2010-01-28
申请号：US12178242
申请日：2008-07-23
Applicant: Daniel Ross Collette
Inventor： Daniel Ross Collette
IPC: F01D25/12
CPC classification number: B64D13/006 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64D2013/0614 , Y02T50/56
Abstract: Electronic equipment frequently requires cooling to maintain the integrity and reliability of the equipment, and to elongate the life expectancy of the equipment. When in operation, the fan of a UAV creates airflow comprising outside air directed across the duct of the UAV. Utilizing this airflow generated by the fan of a UAV to provide heat transfer from a equipment enclosure accomplishes efficient heat transfer. The methods described herein for transferring heat from an equipment enclosure using an airflow generated by a fan of a UAV may be employed for UAVs having a variety of duct shapes, and having equipment enclosures inside the duct or in detachable equipment enclosures located on the duct of the UAV.
Abstract translation: 电子设备经常需要冷却以保持设备的完整性和可靠性，并延长设备的预期寿命。 当操作时，无人机的风扇产生气流，其包括被引导穿过无人机的管道的外部空气。 利用由无人机的风扇产生的这种气流来提供来自设备外壳的热量传递，从而实现有效的热传递。 本文所述的用于使用由UAV的风扇产生的气流从设备外壳传递热量的方法可以用于具有各种管道形状的UAV，并且在管道内部或在位于管道上的可拆卸设备外壳中具有设备外壳 无人机。
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公开(公告)号：US20220409440A1
公开(公告)日：2022-12-29
申请号：US17360936
申请日：2021-06-28
Applicant: Daniel Ross Collette
Inventor： Daniel Ross Collette
Abstract: This patent describes the design of a novel metal snap, either ball or socket, and the process by which it is integrated and connected to conductive elements in incontinence products, manufactured in high speed production lines, which makes possible the monitoring and detection of incontinent events in the product.
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公开(公告)号：US20100116827A1
公开(公告)日：2010-05-13
申请号：US12269132
申请日：2008-11-12
Applicant: Daniel Ross Collette
Inventor： Daniel Ross Collette
IPC: B65D88/12
CPC classification number: B64C27/20 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/162 , B64D37/04 , B64D37/06 , B64D37/22 , Y10T137/86212 , Y10T137/86348
Abstract: A vertical non-bladdered fuel tank for a ducted fan vehicle comprising: a pod that releasably connects to a core vehicle of a ducted fan vehicle, a vertical fuel tank contained by the pod, wherein the vertical fuel tank is centered between the fore and aft sides of the pod, an outlet in a floor of the vertical fuel tank located adjacent to a sidewall on the fore side of the vertical fuel tank, wherein the outlet is coupled to a draw tube contained by the core vehicle, and a pressure release vent located at the highlight of the pod's duct.
Abstract translation: 一种用于管道式风扇车辆的垂直非风扇燃料箱，包括：可释放地连接到管道式风扇车辆的核心车辆的舱，由舱架容纳的垂直燃料箱，其中垂直燃料箱在前后之间居中 所述荚的侧面是垂直燃料箱的位于垂直燃料箱前侧的侧壁附近的出口，其中所述出口连接到由所述核心车辆容纳的牵引管，以及压力释放口 位于荚管道的高处。
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Patent Agency Ranking
公开(公告)号：US20100024897A1
公开(公告)日：2010-02-04
申请号：US12183277
申请日：2008-07-31
Applicant: Daniel Ross Collette
Inventor： Daniel Ross Collette
CPC classification number: F02M37/20 , Y10T137/3021 , Y10T137/86372
Abstract: A fuel line air trap for an unmanned aerial vehicle has a vessel in-line with a fuel line, fuel line connectors, and fuel inlet and outlet stems. The vessel contains an inlet at a distal end and an outlet at a proximal end. The fuel line connectors are attached to the vessel at the inlet and at the outlet to connect the fuel line to the vessel. The fuel inlet stem attaches to the vessel at the inlet and a fuel outlet stem attaches to the vessel at the outlet. Both the fuel inlet stem and fuel outlet stem protrude into the vessel a predetermined distance such that a gap exists between them. As air bubbles enter the gap in the fuel line air trap, they separate from the flow of fuel and migrate to the exterior walls of the vessel. The air bubbles are purged during remain trapped refueling.
Abstract translation: 用于无人驾驶飞行器的燃料管路空气阱具有与燃料管线，燃料管线连接器以及燃料入口和出口管线一致的容器。 容器在远端包含入口和近端的出口。 燃料管线连接器在入口处和出口处连接到容器以将燃料管线连接到容器。 燃料入口杆在入口处附接到容器，并且燃料出口阀杆在出口处附接到容器。 燃料入口杆和燃料出口阀杆两者都突出到容器中预定的距离，使得它们之间存在间隙。 当气泡进入燃料管路空气阱中的间隙时，它们与燃料流分离并迁移到容器的外壁。 在保留被困的加油期间，气泡被清除。
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公开(公告)号：US20120153087A1
公开(公告)日：2012-06-21
申请号：US12186693
申请日：2008-08-06
Applicant: Daniel Ross Collette , Joseph Scott Helsing, JR.
Inventor： Daniel Ross Collette , Joseph Scott Helsing, JR.
CPC classification number: B64C39/024 , B64C27/20 , B64C2201/027 , B64C2201/048 , B64C2201/088 , B64C2201/108 , B64C2201/126 , B64C2201/162 , B64C2211/00
Abstract: A pod for an unmanned aerial vehicle is provided that may be removed and re-attached to the vehicle. The pod comprises an outer shell, within which a variety of payloads may be carried. A first surface on the vehicle frame comprises a plurality of connects or electrical traces. The plurality of attachments are used to removably attach the pods to the first surface. Thus, a wide variety of payloads may be delivered using the same unmanned aerial vehicle, simply by removing and attaching different pods to a fixed vehicle core. These pods may be shaped so as to form part of the vehicle exterior, and when the pods are attached to the frame, they enhance the aerodynamics of the vehicle.
Abstract translation: 提供用于无人驾驶飞行器的舱架，其可以被移除并重新附接到车辆。 荚包括外壳，在其中可以携带各种有效载荷。 车架上的第一表面包括多个连接或电迹线。 多个附件用于将荚可移除地附接到第一表面。 因此，可以简单地通过将不同的荚移除并附接到固定的车辆核心，使用相同的无人驾驶飞行器来传送各种有效载荷。 这些荚可以成形为形成车辆外部的一部分，并且当荚附接到框架时，它们增强了车辆的空气动力学。
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公开(公告)号：US08123169B2
公开(公告)日：2012-02-28
申请号：US12269132
申请日：2008-11-12
Applicant: Daniel Ross Collette
Inventor： Daniel Ross Collette
IPC: B64D37/02
CPC classification number: B64C27/20 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/162 , B64D37/04 , B64D37/06 , B64D37/22 , Y10T137/86212 , Y10T137/86348
Abstract: A vertical non-bladdered fuel tank for a ducted fan vehicle comprising: a pod that releasably connects to a core vehicle of a ducted fan vehicle, a vertical fuel tank contained by the pod, wherein the vertical fuel tank is centered between the fore and aft sides of the pod, an outlet in a floor of the vertical fuel tank located adjacent to a sidewall on the fore side of the vertical fuel tank, wherein the outlet is coupled to a draw tube contained by the core vehicle, and a pressure release vent located at the highlight of the pod's duct.
Abstract translation: 一种用于管道式风扇车辆的垂直非风扇燃料箱，包括：可释放地连接到管道式风扇车辆的核心车辆的舱，由舱架容纳的垂直燃料箱，其中垂直燃料箱在前后之间居中 所述荚的侧面是垂直燃料箱的位于垂直燃料箱前侧的侧壁附近的出口，其中所述出口连接到由所述核心车辆容纳的牵引管，以及压力释放口 位于荚管道的高处。
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公开(公告)号：US20100328169A1
公开(公告)日：2010-12-30
申请号：US12267246
申请日：2008-11-07
Applicant: Daniel Ross Collette , Joseph Scott Helsing, JR.
Inventor： Daniel Ross Collette , Joseph Scott Helsing, JR.
CPC classification number: H01Q1/286 , B64C1/36 , B64C11/001 , B64C27/20 , B64C2201/027 , B64C2201/108 , B64C2201/162
Abstract: A conformal antenna for an unmanned aerial vehicle is provided that may be applied to a surface of the vehicle. The conformal antenna may be integrated with a surface on the vehicle, and is used to effectively transmit and receive video, command and/or control signals. The conformal antenna allows for the transmission and reception of signals from any direction, and may work with signals greater than a quarter wavelength. A protective layer may be placed over the conformal antenna.
Abstract translation: 提供了可以应用于车辆表面的用于无人驾驶飞行器的保形天线。 适形天线可以与车辆上的表面集成，并且用于有效地发送和接收视频，命令和/或控制信号。 保形天线允许从任何方向发射和接收信号，并且可以使用大于四分之一波长的信号。 保护层可以放置在适形天线上。
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公开(公告)号：US08358677B2
公开(公告)日：2013-01-22
申请号：US12145349
申请日：2008-06-24
Applicant: Daniel Ross Collette , Vaughn Fulton
Inventor： Daniel Ross Collette , Vaughn Fulton
IPC: H04B1/00
CPC classification number: G05D1/0044 , G05D1/0022 , G08G5/0069
Abstract: A system and method for transmitting UAV position data to a central flight control center transmits UAV position data using a virtual transponder. A ground control station for controlling the UAV receives data from the UAV, including UAV position data. The UAV may provide GPS data, or corrected position data based on readings from an inertial navigation system. The ground control station transmits the UAV position data to a flight control center.
Abstract translation: 用于将UAV位置数据发送到中央飞行控制中心的系统和方法使用虚拟转发器发送UAV位置数据。 用于控制UAV的地面控制站从UAV接收数据，包括UAV位置数据。 UAV可以基于惯性导航系统的读数提供GPS数据或校正的位置数据。 地面控制站将无人机位置数据发送到飞行控制中心。
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