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1.发明申请METHODS AND APPARATUSES FOR STORING, LAUNCHING, AND CAPTURING UNMANNED AIRCRAFT 审中-公开用于存储，启动和捕获未经规定的飞机的方法和装置
公开(公告)号：WO2005014390A3
公开(公告)日：2006-03-23
申请号：PCT/US2004001033
申请日：2004-01-17
Applicant: INSITU GROUP , DENNIS BRYAN D , JACKSON CLIFFORD , MCGEER BRIAN T , ROESELER CORY , VONFLOTOW ANDREAS H
Inventor： DENNIS BRYAN D , JACKSON CLIFFORD , MCGEER BRIAN T , ROESELER CORY , VONFLOTOW ANDREAS H
IPC: B64F1/00 , B63B27/10 , B63B27/16 , B63B27/26 , B64C25/68 , B64C39/02 , B64F1/02 , B64F1/04 , B64F1/06
CPC classification number: B64F1/02 , B63B27/26 , B64C25/68 , B64C39/024 , B64C2201/042 , B64C2201/044 , B64C2201/048 , B64C2201/084 , B64C2201/102 , B64C2201/146 , B64C2201/165 , B64C2201/182 , B64C2201/201 , B64F1/04 , B64F1/06
Abstract: Methods and apparatuses for assembling, launching, recovering, disassembling, capturing, and storing unmanned aircraft (140) and other flight devices or projectiles are described. In one embodiment, the aircraft (140) can be assembled from a container (111) with little or no manual engagement by an operator. The container (111) can include a guide structure to control motion of the aircraft components. The aircraft (140) can be launched from an apparatus that includes an extendable boom (103). The boom (103) can be extended to deploy a recovery line (853) to capture the aircraft (140) in flight. The aircraft (140) can then be returned to its launch platform, disassembled, and stored in the container (111), again with little or no direct manual contact between the operator and the aircraft (140).
Abstract translation: 描述了组装，发射，恢复，拆卸，捕获和存储无人机（140）和其他飞行装置或射弹的方法和装置。 在一个实施例中，飞行器（140）可以由操作者很少或没有手动接合的容器（111）组装。 容器（111）可以包括用于控制飞行器部件的运动的引导结构。 飞机（140）可以从包括可伸缩吊杆（103）的装置发射。 悬臂（103）可以延伸以部署回收线（853）以在飞行中捕获飞行器（140）。 然后，飞机（140）可以在操作员和飞行器（140）之间很少或没有直接的手动接触的情况下再次返回到其发射平台，拆卸并存储在容器（111）中。
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公开(公告)号：CA2513507C
公开(公告)日：2011-05-03
申请号：CA2513507
申请日：2004-01-17
Applicant: INSITU GROUP INC
Inventor： DENNIS BRIAN D , JACKSON CLIFFORD , MCGEER BRIAN T , ROESELER CORY , VON FLOTOW ANDREAS H
IPC: B64F1/04 , B63B27/10 , B63B27/16 , B63B27/26 , B64C25/68 , B64C39/02 , B64F1/02 , B64F1/06 , B64F1/10
Abstract: Methods and apparatuses for assembling, launching, recovering, disassembling, capturing, and storing unmanned aircraft and other flight devices or projectiles are described. In one embodiment, the aircraft can be assembled from a container with little or no manual engagement by an operator. The container can include a guide structure to control motion of the aircraft components. The aircraft can be launched from an apparatus that includes an extendable boom. The boom can be extended to deploy a recovery line to capture the aircraft in flight. The aircraft can then be returned to its launch platform, disassembled, and stored in the container, again with little or no direct manual contact between the operator and the aircraft.
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公开(公告)号：DE60010881T2
公开(公告)日：2005-06-02
申请号：DE60010881
申请日：2000-06-06
Applicant: INSITU GROUP BINGEN
Inventor： MCGEER BRIAN T , VON FLOTOW ANDREAS H , ROESLER CORY , JACKSON CLIFFORD
Abstract: A method and apparatus for retrieving an aircraft in a confined space involves hanging a cable, for example from a kite or mast, across the aircraft's flight path. The aircraft approaches the cable in steady forward flight, and may strike the cable at any point on the wing, fuselage, or other leading surface. The cable then slides along the airframe as the aircraft moves forward, until it is intercepted by a hook attached to the wing tip or other convenient location. The hook captures the cable, and prevents further sliding; the cable then pulls the aircraft to a stop. Compliance of the cable, optionally combined with compliance of the cable suspension, provides acceptably gradual deceleration. The aircraft is left suspended in mid-air, and is then winched or slid to the base of the cable or other convenient retrieval point. The cable suspension and other fixed objects can be kept well clear of the flight path, so that the aircraft can continue safely in the event that it misses the cable, and make another approach.
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公开(公告)号：CA2513507A1
公开(公告)日：2005-02-17
申请号：CA2513507
申请日：2004-01-17
Applicant: INSITU GROUP
Inventor： VONFLOTOW ANDREAS H , DENNIS BRYAN D , JACKSON CLIFFORD , ROESELER CORY , MCGEER BRIAN T
Abstract: Methods and apparatuses for assembling, launching, recovering, disassembling , capturing, and storing unmanned aircraft and other flight devices or projectiles are described. In one embodiment, the aircraft can be assembled from a container with little or no manual engagement by an operator. The container can include a guide structure to control motion of the aircraft components. The aircraft can be launched from an apparatus that includes an extendable boom. The boom can be extended to deploy a recovery line to captu re the aircraft in flight. The aircraft can then be returned to its launch platform, disassembled, and stored in the container, again with little or no direct manual contact between the operator and the aircraft.
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Patent Agency Ranking
公开(公告)号：ES2220498T3
公开(公告)日：2004-12-16
申请号：ES00950213
申请日：2000-06-06
Applicant: INSITU GROUP
Inventor： MCGEER BRIAN T , VON FLOTOW ANDREAS H , ROESLER CORY , JACKSON CLIFFORD
Abstract: Aparato para capturar, y aparato comprendiendo un objeto volante provisto de una superficie de elevación en el sentido de la longitud del ala (16)(16) con un dispositivo de captura (19) y que vuela a lo largo de una trayectoria de vuelo (5, 14, 25), el aparato adicionalmente comprendiendo: una fijación globalmente lineal, curvilínea, o lineal y curvilínea (2, 10, 17) que se puede colocar en la trayectoria de vuelo del objeto volante, por lo menos una parte de la fijación estando inclinada en un ángulo con relación a la superficie de elevación en el sentido de la longitud del ala para formar intersección con la superficie de elevación en el sentido de la longitud del ala, la fijación estando provista de una superficie de acoplamiento colocada para acoplar el dispositivo de captura del objeto volante para fijar de forma que se pueda soltar el objeto volante a la fijación; y una estructura de soporte (1, 9) acoplada a la fijación y colocada para sostener la fijación en la trayectoria de vuelo.
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公开(公告)号：AU2004262619A1
公开(公告)日：2005-02-17
申请号：AU2004262619
申请日：2004-01-17
Applicant: INSITU GROUP
Inventor： DENNIS BRYAN D , JACKSON CLIFFORD , MCGEER BRIAN T , ROESELER CORY , VONFLOTOW ANDREAS H
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公开(公告)号：PT1185457E
公开(公告)日：2004-10-29
申请号：PT00950213
申请日：2000-06-06
Applicant: INSITU GROUP
Inventor： FLOTOW ANDREAS H VON , MCGEER BRIAN T , JACKSON CLIFFORD , ROESLER CORY
Abstract: A method and apparatus for retrieving an aircraft in a confined space involves hanging a cable, for example from a kite or mast, across the aircraft's flight path. The aircraft approaches the cable in steady forward flight, and may strike the cable at any point on the wing, fuselage, or other leading surface. The cable then slides along the airframe as the aircraft moves forward, until it is intercepted by a hook attached to the wing tip or other convenient location. The hook captures the cable, and prevents further sliding; the cable then pulls the aircraft to a stop. Compliance of the cable, optionally combined with compliance of the cable suspension, provides acceptably gradual deceleration. The aircraft is left suspended in mid-air, and is then winched or slid to the base of the cable or other convenient retrieval point. The cable suspension and other fixed objects can be kept well clear of the flight path, so that the aircraft can continue safely in the event that it misses the cable, and make another approach.
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公开(公告)号：DE60010881D1
公开(公告)日：2004-06-24
申请号：DE60010881
申请日：2000-06-06
Applicant: INSITU GROUP BINGEN
Inventor： MCGEER BRIAN T , VON FLOTOW ANDREAS H , ROESLER CORY , JACKSON CLIFFORD
Abstract: A method and apparatus for retrieving an aircraft in a confined space involves hanging a cable, for example from a kite or mast, across the aircraft's flight path. The aircraft approaches the cable in steady forward flight, and may strike the cable at any point on the wing, fuselage, or other leading surface. The cable then slides along the airframe as the aircraft moves forward, until it is intercepted by a hook attached to the wing tip or other convenient location. The hook captures the cable, and prevents further sliding; the cable then pulls the aircraft to a stop. Compliance of the cable, optionally combined with compliance of the cable suspension, provides acceptably gradual deceleration. The aircraft is left suspended in mid-air, and is then winched or slid to the base of the cable or other convenient retrieval point. The cable suspension and other fixed objects can be kept well clear of the flight path, so that the aircraft can continue safely in the event that it misses the cable, and make another approach.
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公开(公告)号：AT267119T
公开(公告)日：2004-06-15
申请号：AT00950213
申请日：2000-06-06
Applicant: INSITU GROUP
Inventor： MCGEER BRIAN T , VON FLOTOW ANDREAS H , ROESLER CORY , JACKSON CLIFFORD
Abstract: A method and apparatus for retrieving an aircraft in a confined space involves hanging a cable, for example from a kite or mast, across the aircraft's flight path. The aircraft approaches the cable in steady forward flight, and may strike the cable at any point on the wing, fuselage, or other leading surface. The cable then slides along the airframe as the aircraft moves forward, until it is intercepted by a hook attached to the wing tip or other convenient location. The hook captures the cable, and prevents further sliding; the cable then pulls the aircraft to a stop. Compliance of the cable, optionally combined with compliance of the cable suspension, provides acceptably gradual deceleration. The aircraft is left suspended in mid-air, and is then winched or slid to the base of the cable or other convenient retrieval point. The cable suspension and other fixed objects can be kept well clear of the flight path, so that the aircraft can continue safely in the event that it misses the cable, and make another approach.
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