公开(公告)号：US3974359A

公开(公告)日：1976-08-10

申请号：US585417

申请日：1975-06-09

Applicant: Dee R. Orcutt ,  Kenneth C. Collier

Inventor： Dee R. Orcutt ,  Kenneth C. Collier

IPC: B32B17/10 ,  B64C1/14 ,  H05B3/86 ,  H05B3/06

CPC classification number: B32B17/10761 ,  B32B17/10036 ,  B32B17/10174 ,  B32B17/10366 ,  B32B17/1077 ,  B64C1/1484 ,  H05B3/86 ,  H05B2203/014

Abstract: A laminated glass-plastic glazing unit suitable for aircraft is disclosed. The unit comprises a pair of sheets of rigid transparent material such as glass and an interlayer of thermoplastic material that is susceptible to crack at low temperatures and that has a higher coefficient of thermal expansion than the sheets of rigid transparent material. Electrical resistance material preferably in the form of thin metal wire, is embedded within the interlayer and disposed locally in areas along a pair of opposite marginal edges of the interlayer and electrically energized to heat the interlayer portion adjacent thereto sufficiently to overcome the tendency of the interlayer to pull chips from the marginal portion of one or both of the rigid sheets when the unit is subjected to extremely low temperature conditions in a high-flying aircraft. The electroconductive material is embedded within the interlayer in spaced relation to a transparent electroconductive coating on one of the glass sheets for heating the glazing unit to dissipate mist or frost and is located relative to the thickness of the interlayer in a plane that is closer to the rigid sheet more likely to become damaged when the unit is exposed to the aforesaid low temperature conditions. The interlayer may also include a metal reinforcement frame in heat exchanging relation to the electroconductive material that extends to the edge of the interlayer to conduct heat received from the electroconductive material to the edge of the interlayer, thereby retarding the cooling of the edge of the interlayer to a temperature at which it cracks.

Abstract translation: 公开了一种适用于飞机的夹层玻璃塑料玻璃装置。 该单元包括一对刚性透明材料如玻璃和热塑性材料的中间层，其在低温下易于裂纹，并且具有比刚性透明材料片材更高的热膨胀系数。 优选以细金属丝的形式的电阻材料嵌入在中间层内并且局部地设置在沿着中间层的一对相对的边缘边缘的区域中，并被电通电以加热与其相邻的中间层部分，足以克服中间层的趋势 当高速飞行器中的单元受到极低温度条件时，从一个或两个刚性片材的边缘部分拉出芯片。 导电材料以与玻璃板之一上的透明导电涂层间隔开的方式嵌入在中间层内，用于加热玻璃窗单元以消散雾或霜，并且相对于中间层的厚度位于更靠近 当单元暴露于上述低温条件下时，刚性片更容易损坏。 中间层还可以包括与导电材料热交换的金属增强框架，该金属增强框架延伸到中间层的边缘以将从导电材料接收的热量传导到中间层的边缘，从而延缓中间层边缘的冷却 达到其破裂的温度。

公开(公告)号：US4396826A

公开(公告)日：1983-08-02

申请号：US292458

申请日：1981-08-13

Applicant: Dee R. Orcutt ,  David C. Allen

Inventor： Dee R. Orcutt ,  David C. Allen

IPC: B64C1/14 ,  H05B3/84 ,  H05B3/86 ,  H05B3/06

CPC classification number: B32B17/10018 ,  B32B17/10385 ,  B32B17/10761 ,  B32B17/1077 ,  B32B17/10798 ,  B32B17/10853 ,  B64C1/1492 ,  H05B3/84 ,  H05B3/86 ,  B32B2333/12 ,  B32B2369/00 ,  H05B2203/013 ,  H05B2203/016 ,  Y10S428/922

Abstract: A novel solderless connection between a bus bar and an array of electroconductive wires avoids cracks in plastic window elements, particularly the outer component of curved lightweight heated windows, particularly those used in aircraft.

Abstract translation: 汇流条和导电线阵列之间的新颖的无焊接连接避免了塑料窗口元件中的裂纹，特别是弯曲的轻质加热窗户的外部部件，特别是在飞机上使用的那些。

公开(公告)号：US4277294A

公开(公告)日：1981-07-07

申请号：US46150

申请日：1979-06-06

Applicant: Dee R. Orcutt

Inventor： Dee R. Orcutt

IPC: B32B17/10 ,  B32B31/20 ,  C03C27/04

CPC classification number: B32B17/10366 ,  B32B17/10045 ,  B32B17/10174 ,  B32B17/10293 ,  Y10T428/24777 ,  Y10T428/31601 ,  Y10T428/31605 ,  Y10T428/3163

Abstract: Fabricating a panel comprising a rigid mounting frame surrounding a laminated transparency having a metal reinforcing insert embedded therein in such a manner that the insert is parallel to the outer major surface of the transparency after its fabrication.

Abstract translation: 制造面板，其包括围绕具有嵌入其中的金属加强插入件的层压透明体的刚性安装框架，使得插入件在其制造之后平行于透明体的外主表面。