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    • 5. 发明授权
    • High-speed airplane deicing installation systems and methods
    • 高速飞机除冰安装系统及方法
    • US09352852B2
    • 2016-05-31
    • US14833564
    • 2015-08-24
    • Valentin Luca
    • Valentin Luca
    • B64F5/00
    • B64F5/23B05B7/08B05B12/02B05B12/04B05B13/005B05B13/0431B05B13/0436B64D15/00B64D15/02B64D15/06B64D15/10B64F5/20Y02P70/585
    • The present disclosure provides an airplane ground deicing installation that minimizes the impact of deicing operations on the airport during icing conditions. The installation does not require alteration of a normal taxi pattern and can be performed as quickly as the average separation time between take-offs. The installation allows modification of its shape to adapt to the contour of almost all types of commercial passengers airplanes operating from major airports, and simultaneously deices large surfaces of the airplane. Deicing and anti-icing fluids are applied to airplane surfaces from nozzles positioned in close proximity to the airplane's surface. Speed and adaptability to different types of airplanes, combined with a design that allows rapid relocation of the installation, are key features that make it possible to place the installation on the taxiway, close to the head of the runway it serves, such that the taxi pattern and the separation in between takeoffs are not altered as compared to the normal operations of the airport.
    • 本公开提供一种飞机地面除冰装置,其在结冰条件期间最小化除冰操作对机场的影响。 安装不需要更改常规的出租车模式,可以像起飞之间的平均间隔时间一样快速地进行。 该装置允许修改其形状以适应几乎所有类型的从主要机场运行的商用乘客飞机的轮廓,并且同时设计飞机的大表面。 来自位于飞机表面附近的喷嘴的除冰和防冰流体应用于飞机表面。 不同类型的飞机的速度和适应性,以及允许快速重新安装设备的设计,是使安装在滑行道上,靠近其所提供的跑道头部成为可能的关键特征,使得出租车 与机场的正常运行相比,起飞之间的距离不会改变。
    • 10. 发明授权
    • Hybrid deicing system and method of operation
    • 混合除冰系统及其操作方法
    • US07431240B1
    • 2008-10-07
    • US09640063
    • 2000-08-17
    • John StankoLowell Pearson
    • John StankoLowell Pearson
    • B64D15/00
    • B64F5/23B64F5/20
    • This invention overcome the disadvantage of the prior systems and produces a high velocity specially formed and constituted pressure aerodynamic stream for efficiently and effectively removing ice from an aircraft. The specially formed stream includes a stream within a stream, wherein a deicing fluid such a glycol is entrained within and encased by a surrounding jacket of entraining fluid such air. This deicing is now known as coaxial stream/stream within a stream deicing. The special nozzle allows the stream to maintain fluid separation over its flight path so that aircraft contact is made by to be known as coaxial stream/stream within a stream deicing. The coaxial stream/stream within a stream deicing is further enhanced by pressurizing the stream to deliver the stream as a high pressure high velocity stream to improved the aerodynamic sweeping action of the airstream.
    • 本发明克服了现有系统的缺点,并且产生高速特别形成和构造的压力空气动力流,用于有效地和有效地从飞机上去除冰。 特殊形成的流包括流内的物流,其中除冰流体如二醇被夹带在夹带流体这样的空气的周围夹套内。 这种除冰现在被称为流除冰中的同轴流/流。 专用喷嘴允许流在其飞行路径上保持流体分离,使得飞行器接触通过在流除冰中被称为同轴流/流来制造。 流除冰中的同轴流/流通过对流进行加压来进一步增强,以将流作为高压高速流输送以改善气流的空气动力学清扫作用。