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    • 3. 发明公开
    • COMPLEX ADAPTIVE FIR FILTER
    • 复杂的自适应FIR滤波器
    • EP0700543A4
    • 1997-11-26
    • EP94919221
    • 1994-05-24
    • GRUMMAN AEROSPACE CORP
    • WEDGWOOD JANET EPETRSORIC JOHN F
    • H03H21/00G06F17/00
    • H03H21/0012
    • A complex adaptive Finite-Impulse-Response filter (10) for processing complex digital data having real and imaginary data portions that includes a first data path (17) for receiving and processing the real data portion of the complex input and a second data path (16) for receiving and processing the imaginary data portion. Each first and second data path includes a corresponding plurality of adaptive weight circuits (4) and accumulator circuits (5) to perform respectively, multiplications of input data with a set of updatable coefficient data and accumulations of the multiplication results obtained. Two sets of multiplication results are obtained for each data path and a subset from each are accumulated to form a real output portion and imaginary output portion for the filter. A time delay circuit (6) is provided to allow for proper time multiplexing of the imaginary output portion. The plurality of adaptive weight circuits have associated therewith first and second memory storage banks (24, 27) for storing the current coefficient data values.
    • 7. 发明公开
    • OCCUPANT ARM AND HEAD RESTRAINING ASSEMBLY.
    • FESTHALTEVORRICHTUNGFÜRDIE ARME UND DEN KOPF EINES SITZBESETZERS。
    • EP0643660A4
    • 1995-08-02
    • EP94912344
    • 1994-04-05
    • GRUMMAN AEROSPACE CORP
    • ARONNE ARMAND J
    • B64D25/02B64D25/115
    • B64D25/02
    • An assembly (5) for restraining the upper limbs of an occupant of a seat, particularly an aircraft ejector seat (1), includes a storage unit (65) which is adapted to be fixedly secured to an upper back portion (16) of the seat (1). The storage unit (65) houses a pair of movable cover members (69, 70) and first and second bladder units (75, 76). The cover members (69, 70) and bladder units (75, 76) are connected by means of straps (90, 91) to quick release fittings (94, 95) which mate with corresponding connecting members (111, 112) carried by the occupant and then to a fixed structure adjacent the seat (1). When it is desired to deploy the restraint assembly (5), a tension is applied to the straps (90, 91) which causes the cover members (69, 70) to extend around opposite sides and laterally inward of the occupant's body, about respective arms of the occupant, and the bladder units (75, 76) to extend about the occupant's neck. The bladder units (75, 76) are then inflated so as to permit undesirable movement of the occupant's head.
    • 一种用于约束座椅乘员的上肢尤其是飞机弹射座椅(1)的组件(5)包括存储单元(65),所述存储单元(65)适于固定地固定到所述座椅的上背部分(16) 座位(1)。 存储单元(65)容纳一对活动盖构件(69,70)以及第一和第二气囊单元(75,76)。 盖构件(69,70)和囊单元(75,76)通过带(90,91)连接到快速释放配件(94,95),所述快速释放配件与相应的连接构件(111,112) 然后到邻近座位(1)的固定结构。 当期望展开约束组件(5)时,对带(90,91)施加张力,该张力导致罩构件(69,70)绕乘坐者的身体的相对侧和横向向内延伸 乘员的手臂和膀胱单元(75,76)围绕乘员的颈部延伸。 然后膨胀囊单元(75,76)以便允许乘客头部的不希望的移动。