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    AUTOROTATING PAYLOAD DELIVERY DEVICE
    1.
    发明申请
    AUTOROTATING PAYLOAD DELIVERY DEVICE 有权

    公开(公告)号：US20250051007A1

    公开(公告)日：2025-02-13

    申请号：US18930078

    申请日：2024-10-29

    Applicant: AeroVironment, Inc.

    Inventor： Joel Ifill ,  Zach Taylor ,  Jason Litzinger ,  Philip Stahlhuth ,  Marc Berte

    IPC: B64D1/14 ,  B64C27/02 ,  B64D19/02 ,  B64U10/13 ,  B64U30/21 ,  B64U30/24 ,  B64U30/291 ,  B64U30/293 ,  B64U70/20 ,  B64U101/60

    Abstract: A payload delivery device configured to deliver an aircraft deployed payload along a flight path to a predetermined landing destination includes a support member configured to be removably attached to the payload, a flight control and navigation system module configured to control orientation of the plurality of control surfaces while the payload is travelling along the flight path to the predetermined landing destination, a control surface assembly module including a plurality of control surfaces, a rotor assembly including a plurality of rotor blades having a central axis of rotation, and a collective control assembly module including at least one collective servomotor configured to control a plurality of control linkages connected to the plurality of rotor blades.

    Inflatable unit load device
    3.
    发明授权
    Inflatable unit load device 有权

    公开(公告)号：US11767113B2

    公开(公告)日：2023-09-26

    申请号：US17322652

    申请日：2021-05-17

    Applicant: S.W.O.R.D. International Inc.

    Inventor： Christopher Collin Klaftenegger ,  Jeremy Allen Elrod

    IPC: B64D1/14

    CPC classification number: B64D1/14

    Abstract: An inflatable unit load device that is used to deploy cargo from an aircraft is described herein. In some instances, the inflatable unit load device may include a bladder having one or more inflatable interior bladder cells and a top surface, the top surface of the bladder forming a rigid support surface when the bladder is inflated on which cargo can be loaded, an outer material that positions the one or more inflatable interior bladder cells of the bladder, and a cargo retaining system that retains the cargo on the top surface.

    AUTOROTATING PAYLOAD DELIVERY DEVICE
    4.
    发明申请
    AUTOROTATING PAYLOAD DELIVERY DEVICE 有权

    公开(公告)号：US20220185477A1

    公开(公告)日：2022-06-16

    申请号：US17644653

    申请日：2021-12-16

    Applicant: Dash Systems, Inc.

    Inventor： Joel Ifill ,  Zach Taylor ,  Jason Litzinger ,  Phil Stahlhuth ,  Marc Berte

    IPC: B64D1/14 ,  B64C27/02 ,  B64C39/02 ,  G05D1/10

    Abstract: A payload delivery device configured to deliver an aircraft deployed payload along a flight path to a predetermined landing destination includes a support member configured to be removably attached to the payload, a flight control and navigation system module configured to control orientation of the plurality of control surfaces while the payload is travelling along the flight path to the predetermined landing destination, a control surface assembly module including a plurality of control surfaces, a rotor assembly including a plurality of rotor blades having a central axis of rotation, and a collective control assembly module including at least one collective servomotor configured to control a plurality of control linkages connected to the plurality of rotor blades.

    LOW CAPITAL AND OPERATIONAL COST E-COMMERCE LOGISTICS SYSTEM FOR FAST AND MASSIVE DELIVERY OF E-COMMERCE MERCHANDISE TO LARGE GEOGRAPHICAL AREAS
    5.
    发明申请
    LOW CAPITAL AND OPERATIONAL COST E-COMMERCE LOGISTICS SYSTEM FOR FAST AND MASSIVE DELIVERY OF E-COMMERCE MERCHANDISE TO LARGE GEOGRAPHICAL AREAS 有权

    公开(公告)号：US20220101253A1

    公开(公告)日：2022-03-31

    申请号：US17547375

    申请日：2021-12-10

    Applicant: Parachute Logistics, LLC

    Inventor： Fernando Benjamin Fischmann

    IPC: G06Q10/08 ,  B64D1/12 ,  B64D1/14 ,  G06Q30/06

    Abstract: The present invention discloses a disruptive low capital and operational cost logistics system and method that provides for fast and massive delivery of e-commerce merchandise, including same day delivery, of thousands of items and packages, in extensive geographical areas, such as whole states, countries and continents, reducing the need for building, operating, or using multiple fulfillment warehouses located near the consumers as in traditional e-commerce logistics, creating a revolution in the e-commerce industry worldwide.
    In a disruptive manner, the systems and methods of the present invention facilitate the logistics for e-commerce delivery processes, and also may allow at the same time reducing the use of massive quantities of cardboard packages that are used for protection and containment for e-commerce orders, being sustainably beneficial for the e-commerce market, the environment, and the consumer. This is achieved by the use of multibox packages that are configured to contain a set of products including orders from different consumers and not necessarily having individual packages for individual consumers, where such multibox packages are sorted at the origin in a Central Fulfillment Center.

    EMERGENCY MECHANICAL AND COMMUNICATION SYSTEMS AND METHODS FOR AIRCRAFT
    10.
    发明申请
    EMERGENCY MECHANICAL AND COMMUNICATION SYSTEMS AND METHODS FOR AIRCRAFT 有权
    紧急机械和通信系统和飞机方法

    公开(公告)号：US20160257415A1

    公开(公告)日：2016-09-08

    申请号：US15060372

    申请日：2016-03-03

    Applicant: COMAC AMERICA CORPORATION

    Inventor： Wei Ye ,  Jianhong Sun

    IPC: B64D25/20 ,  B64D47/08 ,  G07C5/00 ,  B64D1/14 ,  B64D45/00 ,  G07C5/08

    CPC classification number: B64D25/20 ,  B64D1/14 ,  B64D3/00 ,  B64D17/00 ,  B64D45/00 ,  B64D47/08 ,  B64D2045/0065 ,  B65H2701/34 ,  G06F1/18 ,  G07C5/008 ,  G07C5/0858

    Abstract: A system for quickly locating and retrieving flight data of an aircraft after an aircraft mid-air mishap comprises: a flight data recorder; a tracking device comprising at least one camera; a rapid ejection system for ejecting the flight data recorder and tracking device; a soft landing system; and a tow system, wherein the tow system is configured to continue to transmit flight information from the aircraft to the tracking device via the data communication link for a period of time after the ejection of the tracking device; and wherein the tracking device transmits to the flight data recorder the flight information received from the aircraft after ejection and the images captured by the tracking device immediately following the mid-air mishap, and wherein the flight data recorder is configured to in turn transmit said flight information and images to the remote device.

    Abstract translation: 一种用于在飞机空中事故之后快速定位和检索飞行器的飞行数据的系统包括：飞行数据记录器; 跟踪装置，包括至少一个相机; 用于喷射飞行数据记录器和跟踪装置的快速排出系统; 软着陆系统; 以及牵引系统，其中所述牵引系统被配置为在所述跟踪装置的弹出之后的一段时间内，经由所述数据通信链路继续将飞行信息从所述飞机传送到所述跟踪装置; 并且其中所述跟踪装置向所述飞行数据记录器发送在所述飞行数据记录器之后从所述飞行器接收的飞行信息和由所述跟踪装置在所述空中事故之后立即捕获的图像，并且其中所述飞行数据记录器被配置为依次将所述飞行 信息和图像到远程设备。

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