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    SURVIVABILITY AND MISSION FLEXIBILITY ENHANCEMENTS FOR RECONNAISSANCE AIRCRAFT
    1.
    发明申请
    SURVIVABILITY AND MISSION FLEXIBILITY ENHANCEMENTS FOR RECONNAISSANCE AIRCRAFT 审中-公开
    恢复性和使命灵活性增强用于重新评估飞机

    公开(公告)号：WO0150135A3

    公开(公告)日：2001-12-20

    申请号：PCT/US0100033

    申请日：2001-01-02

    Applicant: ADVANCED AEROSPACE TECHNOLOGIE ,  MCDONNELL WILLIAM R

    Inventor： MCDONNELL WILLIAM R

    IPC: B64D3/00 ,  B64D7/00 ,  B64D47/08 ,  F41G3/02 ,  B64C

    CPC classification number: B64D3/02 ,  B64D7/00 ,  B64D47/08 ,  F41G3/02

    Abstract: A pod (34) containing sensors and/or targeting systems such as laser designators or range finders are hung on a cable (30) below an aircraft (12). The line (30) can be reeled in or out similar to towed decoys. This allows the aircraft (12) to operate above or in the cloud cover while the sensors/targeting equipment (34) are operating below the cloud cover to find the enemy forces.

    Abstract translation: 包含传感器和/或目标系统（例如激光指示器或测距仪）的舱（34）悬挂在飞机（12）下方的电缆（30）上。 线（30）可以与拖曳的诱饵类似地卷起或出去。 这样就可以使飞机（12）在云盖上方或云盖中操作，同时传感器/瞄准设备（34）在云盖下方操作以找到敌方的力量。

    LAUNCH AND RECOVERY SYSTEM FOR UNMANNED AERIAL VEHICLES
    7.
    发明专利
    LAUNCH AND RECOVERY SYSTEM FOR UNMANNED AERIAL VEHICLES 未知

    公开(公告)号：CA2384557A1

    公开(公告)日：2001-02-01

    申请号：CA2384557

    申请日：2000-07-24

    Applicant: ADVANCED AEROSPACE TECHNOLOGIE

    Inventor： MCDONNELL WILLIAM R

    IPC: B64C25/68 ,  B64C39/02 ,  B64D3/00 ,  B64F1/02 ,  B64F1/04 ,  B64F1/10

    Abstract: An improved method of launching and retrieving a UAV (Unmanned Aerial Vehicl e) (10) is disclosed. The preferred method of launch involves carrying the UAV (10) up to altitude using a parasail (8) similar to that used to carry tourists aloft. The UAV is dropped and picks up enough airspeed in the dive to perform a pull-up into level controlled flight. The preferred method of recovery is for the UAV to fly into and latch onto the parasail tow line (4) or cables hanging off the tow line and then be winched back down to the boat (2).

    LANDING AND TAKE-OFF ASSEMBLY FOR VERTICAL TAKE-OFF AND LANDING AND HORIZONTAL FLIGHT AIRCRAFT
    8.
    发明专利
    LANDING AND TAKE-OFF ASSEMBLY FOR VERTICAL TAKE-OFF AND LANDING AND HORIZONTAL FLIGHT AIRCRAFT 未知

    公开(公告)号：IL128054A

    公开(公告)日：2003-06-24

    申请号：IL12805497

    申请日：1997-07-14

    Applicant: ADVANCED AEROSPACE TECHNOLOGIE

    IPC: B64C29/02 ,  B64F1/12

    Abstract: An aircraft adapted for flight in helicopter mode with its longitudinal axis oriented generally vertically and in airplane mode with its longitudinal axis oriented generally horizontally is provided with the capability of launching and landing with the tail end directed skyward. The invention also includes improvements to the controllability and efficiency of aircraft in helicopter mode provided by the stabilizer wings and relative rotation of the fuselage section about the aircraft's longitudinal axis. The aircraft has an elongate boom positioned between the rear fuselage and the stabilizer wings for engagement with a base structure. The base structure may be attached to a building, a trailer transporter, a ship or some other structure. The base may be a beam having latching arms that swing inward when pressure from the boom is applied, then trap the boom in a recess between the latching arm and beam, thereby suspending the aircraft. An actuator for releasing the latching arms is provided to allow the aircraft to launch.

    LAUNCH AND RECOVERY SYSTEM FOR UNMANNED AERIAL VEHICLES
    9.
    发明专利
    LAUNCH AND RECOVERY SYSTEM FOR UNMANNED AERIAL VEHICLES 未知

    公开(公告)号：CA2384557C

    公开(公告)日：2010-02-16

    申请号：CA2384557

    申请日：2000-07-24

    Applicant: ADVANCED AEROSPACE TECHNOLOGIE

    Inventor： MCDONNELL WILLIAM R

    IPC: B64C25/68 ,  B64C39/02 ,  B64D3/00 ,  B64F1/02 ,  B64F1/04 ,  B64F1/10

    Abstract: An improved method of launching and retrieving a UAV (Unmanned Aerial Vehicle) (10) is disclosed. The preferred method of launch involves carrying the UAV (10) up to altitude using a parasail (8) similar to that used to carry tourists aloft. The UAV is dropped and picks up enough airspeed in the dive to perform a pull-up into level controlled flight. The preferred method of recovery is for the UAV to fly into and latch onto the parasail tow line (4) or cables hanging off the tow line and then be winched back down to the boat (2).

    SISTEMA DE LANZAMIENTO Y RECUPERACION DE VEHICULOS AEREOS NO TRIPULADOS.
    10.
    发明专利
    SISTEMA DE LANZAMIENTO Y RECUPERACION DE VEHICULOS AEREOS NO TRIPULADOS. 未知

    公开(公告)号：ES2307524T3

    公开(公告)日：2008-12-01

    申请号：ES00952173

    申请日：2000-07-24

    Applicant: ADVANCED AEROSPACE TECHNOLOGIE

    Inventor： MCDONNELL WILLIAM R ,  BAKER CHARLES H

    IPC: B64C25/68 ,  B64C39/02 ,  B64D3/00 ,  B64F1/02 ,  B64F1/04 ,  B64F1/10

    Abstract: En combinación, un sistema de recuperación aérea de aviones y avión (10; 51; 52; 616;); comprendiendo dicho sistema de recuperación aérea, como mínimo, un cabo de captación (20; 21; 76; 121; 212; 608; 610) mantenido en elevación como mínimo por un extremo superior por una estructura de soporte (8; 78; 600), quedando frenado el extremo inferior del cabo de captación; teniendo dicho avión un dispositivo de recogida (26) para recoger dicho cabo y una estructura de desviación para desviar dicho cabo lateralmente para establecer contacto con el dispositivo de recogida; caracterizado porque la estructura de soporte (8; 78; 600) se extiende desde un punto superior de suspensión para el cabo de captación a una base, y que la estructura de desviación comprende un ala de dicho avión, poseyendo dicha estructura de desviación, como mínimo, un ángulo de 15º dirigido hacia atrás o de 20º dirigido hacia adelante para desviar de manera más fiable dicho cabo de captación lateralmente con respecto a dicho dispositivo de recogida.

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