公开(公告)号：US4747900A

公开(公告)日：1988-05-31

申请号：US741587

申请日：1985-06-05

申请人： James P. Angus

发明人： James P. Angus

IPC分类号： B29C45/00 ,  B29C45/14 ,  F01D5/28 ,  F01D5/34 ,  B65H81/00 ,  B64C27/46

CPC分类号： B29C45/0005 ,  B29C45/14786 ,  F01D5/282 ,  F01D5/34 ,  F04D29/023 ,  F04D29/321 ,  B29K2105/14 ,  B29L2031/087 ,  F05D2300/603 ,  F05D2300/6032 ,  F05D2300/614 ,  Y10S164/90

摘要： A compressor rotor assembly comprises a shaft and at least one disc having integral radially extending aerofoil blades which disc is integral with the shaft. The assembly comprises a matrix material in which a plurality of short reinforcing fibres are so disposed that the majority thereof within the shaft are generally axially aligned while the majority thereof within the aerofoil blades are generally radially aligned. At least one filament wound support ring provides radial support for the aerofoil blades.

摘要翻译： 压缩机转子组件包括轴和至少一个盘，其具有一体的径向延伸的翼型叶片，该盘与轴成一体。 组件包括基体材料，其中多个短增强纤维被布置成使得其中大部分在轴内大致轴向对准，而其中大部分在翼型叶片内大致径向对准。 至少一个长丝缠绕的支撑环为翼型叶片提供径向支撑。

公开(公告)号：US4685864A

公开(公告)日：1987-08-11

申请号：US790200

申请日：1985-10-22

申请人： James P. Angus ,  Derick A. Perry

发明人： James P. Angus ,  Derick A. Perry

IPC分类号： B64C11/20 ,  F01D5/28 ,  F03D1/06 ,  F01D5/12

CPC分类号： F01D5/282 ,  B64C11/20 ,  F03D1/0675 ,  F05B2240/30 ,  F05D2240/30 ,  Y02E10/721 ,  Y02T50/66 ,  Y02T50/672

摘要： A hollow aerofoil cross-section aircraft propeller blade is provided with a tow of KEVLAR fibres internally thereof. The fibres which are anchored to the blade root and tip portions are arranged to be passive under all normal operating conditions of the blade. However in the event of a structural failure of the blade between its root and tip portions the fibres serve to contain the blade tip together with any portion of the blade attached thereto. The invention is additionally applicable to prop-fan and fan blades for gas turbine engines.

摘要翻译： 空心机翼横截面飞机螺旋桨叶片内部设有一束KEVLAR纤维。 锚固到叶片根部和尖端部分的纤维被布置成在叶片的所有正常操作条件下被动。 然而，在叶片在其根部和尖端部分之间的结构故障的情况下，纤维用于将叶片尖端与其附接的叶片的任何部分一起容纳。 本发明另外适用于燃气轮机发动机的风扇和风扇叶片。

公开(公告)号：US4829539A

公开(公告)日：1989-05-09

申请号：US144177

申请日：1988-01-15

申请人： James P. Angus ,  Derek Salt

发明人： James P. Angus ,  Derek Salt

IPC分类号： G01K11/06

CPC分类号： G01K11/06

摘要： A temperature indicating device which comprises a plurality of panels in a fixed array. Some of the panels are adapted to undergo a reversible change in appearance at a given temperature whereas the remainder are adapted to undergo irreversible change in appearance at a given temperature. The device is useful in indicating the temperature which an object has achieved as well as its actual temperature.

摘要翻译： 一种温度指示装置，包括固定阵列中的多个面板。 一些面板适于在给定温度下经历外观的可逆变化，而其余面板适于在给定温度下经历不可逆的外观变化。 该装置可用于指示物体达到的温度及其实际温度。

公开(公告)号：US4786347A

公开(公告)日：1988-11-22

申请号：US741584

申请日：1985-06-05

申请人： James P. Angus

发明人： James P. Angus

IPC分类号： B29C45/00 ,  B29C45/14 ,  F01D5/28 ,  F01D5/34 ,  B65H81/00

CPC分类号： B29C45/0005 ,  B29C45/14786 ,  F01D5/282 ,  F01D5/34 ,  F04D29/023 ,  F04D29/321 ,  B29L2031/087 ,  F05D2300/43 ,  F05D2300/603 ,  F05D2300/6032 ,  F05D2300/614 ,  Y10S164/90

摘要： A gas turbine engine disc having integral, radially extending aerofoil blades and an integral shroud interconnecting the radially outer extents of the blades is described. In the manufacture thereof continuous fibres are wound around an annular array of inserts provided in a dividable disc. The inserts define the spaces between adjacent blades on the disc. A mixture of chopped carbon fibre and an epoxy resin matrix material is then injected into the central portion of the die interior. Any part of the wound fibres which has not been impregnated by the chopped fibre/resin matrix material is subsequently impregnated by a matrix material whereupon the die is opened to release the thus produced bladed disc.

摘要翻译： 描述了一种具有整体的径向延伸的翼型叶片的燃气涡轮发动机圆盘和互连叶片的径向外部范围的整体式护罩。 在其制造中，连续纤维缠绕在设置在可分割盘中的插入件的环形阵列上。 刀片定义盘上相邻刀片之间的间隔。 然后将切碎的碳纤维和环氧树脂基质材料的混合物注入模具内部的中心部分。 未被短切纤维/树脂基质材料浸渍的卷绕纤维的任何部分随后被基质材料浸渍，由此打开模具以释放由此产生的叶片盘。

公开(公告)号：US4453721A

公开(公告)日：1984-06-12

申请号：US552369

申请日：1983-11-16

申请人： James P. Angus ,  Jack Palfreyman

发明人： James P. Angus ,  Jack Palfreyman

IPC分类号： F16J15/44 ,  F16J15/42 ,  F16J15/48

CPC分类号： F16J15/441 ,  Y10S277/938

摘要： Two seal elements are respectively mounted on generally coaxial relatively rotatable members so that each seal element is capable of relative radial movment with respect to its associated member. One of the seal elements is mounted on its associated member in such a manner that they remain coaxial. The seal elements have confronting radially spaced apart surfaces which are so configured that together they define a hydrodynamic gas bearing. The arrangement is such that upon the relative rotation of the members said seal element which is mounted so as to remain coaxial with its associated member hydrodynamically supports the other seal element so that they remain coaxial.

摘要翻译： 两个密封元件分别安装在大致同轴的相对旋转的构件上，使得每个密封元件能够相对于其相关联的构件相对径向移动。 其中一个密封元件以它们保持同轴的方式安装在其相关联的构件上。 密封元件具有面对的径向间隔开的表面，其被构造成一起它们限定了流体动力气体轴承。 这种布置使得在所述构件的相对旋转时，所述密封元件被安装成与其相关联的构件保持同轴，其水动力地支撑另一个密封元件，使得它们保持同轴。

公开(公告)号：US4826645A

公开(公告)日：1989-05-02

申请号：US741583

申请日：1985-06-05

申请人： James P. Angus

发明人： James P. Angus

IPC分类号： B29C45/00 ,  B29C45/14 ,  F01D5/28 ,  F01D5/34

CPC分类号： F01D5/282 ,  B29C45/0005 ,  B29C45/0013 ,  B29C45/14786 ,  F01D5/34 ,  F04D29/023 ,  F04D29/321 ,  B29L2031/08 ,  F05D2300/43 ,  F05D2300/603 ,  F05D2300/6032 ,  F05D2300/614

摘要： A method of manufacturing a bladed disc from a fiber reinforced composite material which comprises injecting a mixture of short fibers and a matrix material into a dividable die so configured as to define the form of a disc having integral radially extending aerofoil blades. The mixture is injected into the die at such a location that the short fibers within the aerofoil-defining portions of the die are radially aligned. The die contains two support rings which are coaxially disposed within the bladed disc after injection molding so as to provide radial support for the aerofoil blades of the thus formed bladed disc. The method may be modified to provide the bladed disc with an integral shroud.

摘要翻译： 一种从纤维增强复合材料制造叶片的方法，其包括将短纤维和基质材料的混合物注入到可分割模具中，所述模具被构造成限定具有整体径向延伸的翼型叶片的盘的形式。 将混合物注入到模具中，使得模具的机翼限定部分内的短纤维径向对齐。 模具包含两个支撑环，其在注射成型之后同轴地设置在叶片盘内，以便为由此形成的叶片盘的翼型叶片提供径向支撑。 该方法可以被修改以提供具有整体护罩的叶片盘。

公开(公告)号：US4330133A

公开(公告)日：1982-05-18

申请号：US274884

申请日：1981-06-18

申请人： Jack Palfreyman ,  James P. Angus ,  John M. Robertson

发明人： Jack Palfreyman ,  James P. Angus ,  John M. Robertson

IPC分类号： F16J15/44 ,  F16J15/16

CPC分类号： F16J15/441 ,  Y10S277/931

摘要： A seal arrangement suitable for sealing between two coaxially mounted, axially restrained, radially spaced apart and relatively rotatable members comprises two concentric, ring-shaped seal elements having adjacent sealing faces. The seal elements are mounted on the respective members by a spline and groove arrangement which permits radial growth or shrinkage of the relatively rotatable members due to their thermal expansion or contraction without such growth or shrinkage being transferred to the seal elements. The arrangement insures that the gap between the sealing faces of the seal elements remains substantially constant during thermal variations.

摘要翻译： 适合于在两个同轴安装的，轴向限制的，径向间隔开并且相对可旋转的构件之间密封的密封装置包括具有相邻密封面的两个同心的环形密封元件。 密封元件通过花键和槽布置安装在相应的构件上，其允许相对可旋转的构件由于其热膨胀或收缩而径向生长或收缩，而没有这种增长或收缩被转移到密封元件。 该布置确保了在热变化期间，密封元件的密封面之间的间隙保持基本上恒定。