公开(公告)号：WO1996004997A1

公开(公告)日：1996-02-22

申请号：PCT/US1995010122

申请日：1995-08-08

Applicant: USBI, CO.

Inventor： USBI, CO. ,  MATHIAS, David, D. ,  SCARPA, Jack, G. ,  HALL, Terry, L.

IPC: B05B07/14

CPC classification number: B05B7/1431 ,  B05B7/0815 ,  B05B7/0861 ,  B05B7/1495

Abstract: A convergent end-effector which combines a liquid and dry flow external to a spray nozzle eliminates clogging problems common in the prior art spray coating systems. The end-effector utilizes a nozzle (1) with an orifice (7) and at least one atomizing hole (6), a conduit (12) for directing a liquid resin through the nozzle and an outer housing (14) disposed around said conduit to form a cavity (13). Reinforcing material enters the cavity (13) on a gas stream supplied and controlled by an eductor (28) located prior to the outer housing (14), in the direction of the nozzle, and at an angle of less than about 90 DEG with respect to the conduit. The end of the conduit near the nozzle (1) is preferably angled toward the nozzle (1) to further direct the reinforcing material into the liquid resin.

Abstract translation: 在喷嘴外部组合液体和干流的会聚式末端执行器消除了现有技术喷涂系统中常见的堵塞问题。 末端执行器利用具有孔口（7）和至少一个雾化孔（6）的喷嘴（1），用于引导液体树脂通过喷嘴的导管（12）和设置在所述导管周围的外壳体 以形成空腔（13）。 加强材料以位于外壳体（14）之前的喷射器（28）供给和控制的气流在喷嘴的方向上进入空腔（13），并以小于约90°的角度相对于 到管道。 喷嘴（1）附近的导管的端部优选地朝向喷嘴（1）成角度，以进一步将增强材料引导到液体树脂中。

公开(公告)号：WO1996018879A1

公开(公告)日：1996-06-20

申请号：PCT/US1995016303

申请日：1995-12-14

Applicant: USBI CO.

Inventor： USBI CO. ,  NOVAK, Howard, L.

IPC: G01N19/04

CPC classification number: G01N19/04

Abstract: In both the aircraft and aerospace industries, coatings are essential protection for structures, such as the fuselage, from destructive environmental conditions. Typically, the structure has a coating bonded to a substrate. It is essential in these industries that various tests be perfomed on the structures, such as corrosion and adhesion tests. The present invention relates to a method for testing the properties of a workpiece having a coating bonded to a substrate and an apparatus for preparing the workpiece for testing. The method comprises the steps of directing an abrasive media stream against the coating such that a portion of the coating is removed and then performing a test on the properties of the workpiece.

Abstract translation: 在飞机和航空航天工业中，涂层是对破坏性环境条件下的结构（如机身）的基本保护。 通常，该结构具有结合到基底的涂层。 在这些行业中，必须对结构进行各种测试，如腐蚀和粘附试验。 本发明涉及一种用于测试具有粘合到基底上的涂层的工件的性质的方法和用于制备用于测试的工件的装置。 该方法包括以下步骤：将研磨介质流引导到涂层上，使得去除涂层的一部分，然后对工件的性质进行测试。

公开(公告)号：WO1995014609A1

公开(公告)日：1995-06-01

申请号：PCT/US1994013032

申请日：1994-11-14

Applicant: USBI, CO.

Inventor： USBI, CO. ,  FISHER, Jeffrey, A. ,  MILLER, Edward, V. ,  VAN DAM, Dennis

IPC: B64C31/028

CPC classification number: B64C31/028 ,  Y10S244/901 ,  Y10S244/904

Abstract: The deployable wing (1) of the present invention comprises an internal structure having diverging leading edge spars (7) attached to a keel spar (11) and cross spars (9) to form a delta wing configuration. This internal structure is enclosed within a volume defined by a fabric sail having an upper section (3a), a lower section (3b), and fabric ribs (5) disposed therebetween. This fabric sail volume is internally pressurized through a ram air intake (15) at the nose stagnation point. This deployable wing can be folded and deployed in the air.

Abstract translation: 本发明的可展开翼片（1）包括内部结构，其具有附接到龙骨翼梁（11）和交叉翼梁（9）的分叉的前缘翼梁（7）以形成三角翼构型。 该内部结构封闭在由具有上部（3a），下部（3b）和布置在其间的织物肋（5）的织物帆布限定的体积内。 这种织物帆布体积在鼻部停滞点处通过压头进气口（15）内部加压。 这种可部署的机翼可以折叠和部署在空中。

公开(公告)号：WO1994011113A1

公开(公告)日：1994-05-26

申请号：PCT/US1993011181

申请日：1993-11-17

Applicant: USBI, CO.

Inventor： USBI, CO. ,  HALL, Terry, L. ,  SCARPA, Jack, G. ,  MATHIAS, David, D.

IPC: B05B07/14

CPC classification number: B05B7/0815 ,  B05B7/1495 ,  Y10S239/08

Abstract: Coating a substrate with a reinforced resin matrix comprised of liquid resin and reinforcing material can be accomplished with an apparatus where the liquid resin and the reinforcing material are mixed external to the apparatus prior to impacting the substrate. The liquid resin is directed through a cylinder (12) and then through an orifice (7) in nozzle (1), while the reinforcing material is carried in a gas stream through cavity (13), around cylinder (12), and past the nozzle (1). As the reinforcing material passes the nozzle (1), it is drawn into the liquid resin. Due to the distribution of the reinforcing material around the liquid resin flow, the reinforcing material is substantially homogeneously wetted by the liquid resin prior to impacting the substrate.

Abstract translation: 用由液体树脂和增强材料构成的增强树脂基体涂覆基材可以用液体树脂和增强材料在冲击基材之前混合在设备外部的装置来实现。 液体树脂被引导通过圆柱体（12）然后通过喷嘴（1）中的孔口（7），而增强材料以气流运送通过腔体（13），围绕圆柱体（12）并经过 喷嘴（1）。 当加强材料通过喷嘴（1）时，它被吸入液体树脂中。 由于增强材料在液体树脂流动周围的分布，在冲击衬底之前，增强材料基本均匀地被液体树脂润湿。