公开(公告)号：US5088279A

公开(公告)日：1992-02-18

申请号：US501994

申请日：1990-03-30

申请人： Andrew MacGee

发明人： Andrew MacGee

IPC分类号： F02C7/20 ,  F02K3/06

CPC分类号： F02C7/20 ,  F05D2230/644 ,  Y02T50/671

摘要： A duct support assembly includes first and second spaced rings joined by a plurality of circumferentially spaced links. First and second means pivotally join the links to the first and second rings, and the links may be assembled through an outer surface of the first ring and are adjustable from the first ring outer surface.

摘要翻译： 管道支撑组件包括由多个周向间隔开的连接件连接的第一和第二隔开的环。 第一和第二装置将链节枢转地连接到第一和第二环，并且连杆可以通过第一环的外表面组装并且可以从第一环外表面调节。

公开(公告)号：US4971497A

公开(公告)日：1990-11-20

申请号：US487488

申请日：1990-03-02

申请人： Lewis J. Stoffer ,  Andrew MacGee

发明人： Lewis J. Stoffer ,  Andrew MacGee

IPC分类号： F16B37/04 ,  F16B37/06 ,  F16B39/02

CPC分类号： F16B37/04 ,  F16B37/044 ,  F16B39/025 ,  F16B37/064

摘要： A flush mounting fastener system for threadably attaching a threaded member to a plate or shell structure is described which comprises in one representative embodiment an internally threaded bushing flanged on a first end for attachment to the housing within a hole of preselected size in the housing, a plurality of circumferentially spaced crenelations of preselected size and spacing on the second end of the bushing, an insert threaded on the outer surface for threadably engaging the bushing and on the inner surface for threadably attaching a threaded member to the housing structure, and a plurality of tangs on one end of the insert corresponding in size and spacing with the spaced crenelations in the bushing and being radially outwardly bendable into spaces between the crenelations to lock the insert within the bushing. In a second representative embodiment, an annular flange is defined on the end of the bushing opposite the crenelations and a ball nut is disposed within the bushing and supported on the annular flange, the ball nut having a threaded diametric hole for receiving the threaded member and a pair of diametrically oppositely disposed protrusions, and wherein the threaded insert has two diametrically opposed axial slots near the first end for engaging the protrusions of the ball nut and restraining the ball nut from rotation about its threading axis but permitting rotation within predetermined limits about an axis containing the protrusions and an axis orthogonal thereto, whereby a threaded member having a threading axis non-coaxial with the axis of the insert may be threadably received by the ball nut.

摘要翻译： 描述了一种用于将螺纹构件螺纹连接到板或壳结构的齐平安装紧固件系统，其在一个代表性实施例中包括在第一端上凸缘的内螺纹衬套，用于在壳体内预定尺寸的孔内附接到壳体， 在衬套的第二端上具有预选尺寸和间隔的多个圆周间隔的螺纹，在外表面上螺纹连接的衬套，用于螺纹地接合衬套和内表面，用于将螺纹构件螺纹连接到壳体结构;以及多个 刀片的一端上的刀柄的尺寸和间距对应于衬套中的间隔的锯齿形，并且径向向外可弯曲成楔形件之间的空间，以将插入件锁定在衬套内。 在第二代表性实施例中，环形凸缘限定在衬套相对于螺纹的端部上，并且滚珠螺母设置在衬套内并支撑在环形凸缘上，滚珠螺母具有用于接纳螺纹构件的螺纹直径孔， 一对直径相对设置的突起，并且其中所述螺纹插入件在所述第一端附近具有两个直径相对的轴向槽，用于接合所述滚珠螺母的突出部，并且限制所述滚珠螺母不受围绕其螺纹轴线的旋转，但允许在围绕 轴的轴线和与其正交的轴线，由此具有与插入件的轴线不同轴的螺纹轴线的螺纹构件可以被滚珠螺母螺纹接纳。

公开(公告)号：US5085559A

公开(公告)日：1992-02-04

申请号：US509926

申请日：1990-04-16

申请人： Lewis J. Stoffer ,  Andrew MacGee

发明人： Lewis J. Stoffer ,  Andrew MacGee

IPC分类号： F01D5/18 ,  F01D5/28 ,  F02C7/047

CPC分类号： F02C7/047 ,  F01D5/18 ,  F01D5/282 ,  Y02T50/672 ,  Y02T50/673 ,  Y02T50/676

摘要： Metal darts are captured either in bonded assembly or in riveted assembly with composite airfoil skins. The darts have a thin fin extending rearward with a dam at its rear end forming a hot air duct on either side of the fin. As hot compressor bleed air is diverted down through the fin duct, heat is transferred forward to the dart leading edge. The fin may contain ripples or other perturbances to improve heat transfer if necessary. Sufficient heat should be transferred to inhibit ice buildup on the final coating that covers the entire airfoil and further provides FOD protection by having a metal leading edge.

摘要翻译： 金属飞镖被捕获在粘合组件或铆接组件中，复合翼型外皮。 飞镖具有向后延伸的薄翅片，在其后端具有坝，在翅片的任一侧形成热空气管道。 当热压缩机排放空气通过翅片管道向下流动时，热量向前传递到飞镖前缘。 如果需要，翅片可能包含波纹或其他扰动，以改善热传递。 应转移足够的热量以阻止覆盖整个翼型件的最终涂层上的积冰，并通过具有金属前缘进一步提供FOD保护。

公开(公告)号：US4712370A

公开(公告)日：1987-12-15

申请号：US855243

申请日：1986-04-24

申请人： Andrew MacGee

发明人： Andrew MacGee

IPC分类号： F01D21/00 ,  F02C6/04 ,  F02C7/28 ,  F23R3/28 ,  F02C6/18 ,  F02G3/00

CPC分类号： F02C7/28 ,  F01D21/003 ,  F02C6/04 ,  F23R3/283

摘要： A seal assembly 34 for forming an air seal around conduits or accessories 32 crossing aircraft engine bypass ducts 30. The seal assembly comprises a seal retainer plate 40, a seal plate 36 and a seal ring 44. The seal ring 44 has two opposingly sprung legs which seat and form air seals at the duct wall 30 and the seal plate 36.

摘要翻译： 密封组件34，用于在穿过飞机发动机旁通管道30的导管或附件32周围形成空气密封。密封组件包括密封保持板40，密封板36和密封环44.密封环44具有两个相对的弹簧支腿 该座位在管道壁30和密封板36上形成空气密封。