公开(公告)号：US08616498B2

公开(公告)日：2013-12-31

申请号：US12415040

申请日：2009-03-31

Applicant: Zahid Hossain ,  Khashayar Borumand ,  Neha Sharma ,  Keith Couilliard ,  Gaurav Kumar ,  Sean M. Finerty ,  Sara Lynn Walter

Inventor： Zahid Hossain ,  Khashayar Borumand ,  Neha Sharma ,  Keith Couilliard ,  Gaurav Kumar ,  Sean M. Finerty ,  Sara Lynn Walter

IPC: B64C1/10 ,  B64D7/00

CPC classification number: B64C1/40 ,  B32B27/12 ,  B32B37/1207 ,  B32B37/1284 ,  B32B2037/1223 ,  B32B2305/18 ,  B32B2307/3065 ,  B32B2315/02 ,  B32B2371/00 ,  B32B2605/18 ,  Y02T50/46

Abstract: In one of the embodiments of the disclosure, there is provided an aircraft insulation system and method for providing fire penetration resistance and/or thermal and acoustic protection. The aircraft insulation system comprises one or more insulation blankets, each having an inboard side and an outboard side. The aircraft insulation system further comprises a fire penetration resistant cover material having a heat seal adhesive, wherein the fire penetration resistant cover material covers the outboard side of the one or more insulation blankets. The aircraft insulation system further comprises an insulation cover film having a heat seal adhesive, wherein the insulation cover film covers the inboard side of the one or more insulation blankets. The aircraft insulation system further comprises a thermal heat seal that joins the fire penetration resistant cover material and the insulation cover film together to form a continuous insulation blanket assembly.

Abstract translation: 在本公开的一个实施例中，提供了一种用于提供防火穿透性和/或热和声保护的飞机绝缘系统和方法。 飞机绝缘系统包括一个或多个绝缘毯，每个绝缘毯具有内侧和外侧。 飞机绝缘系统还包括具有热密封粘合剂的防火穿透覆盖材料，其中防火穿透覆盖材料覆盖所述一个或多个绝缘毯的外侧。 飞机绝缘系统还包括具有热封粘合剂的绝缘覆盖膜，其中所述绝缘覆盖膜覆盖所述一个或多个隔离层的内侧。 飞机绝缘系统还包括将防火穿透覆盖材料和绝缘覆盖膜连接在一起以形成连续绝缘毯组件的热热密封。

公开(公告)号：US20100243807A1

公开(公告)日：2010-09-30

申请号：US12415040

申请日：2009-03-31

Applicant: Zahid Hossain ,  Khashayar Borumand ,  Neha Sharma ,  Keith Couilliard ,  Gaurav Kumar ,  Sean M. Finerty ,  Sara Lynn Walter

Inventor： Zahid Hossain ,  Khashayar Borumand ,  Neha Sharma ,  Keith Couilliard ,  Gaurav Kumar ,  Sean M. Finerty ,  Sara Lynn Walter

IPC: B64C1/40 ,  B32B37/14 ,  B29C65/08

CPC classification number: B64C1/40 ,  B32B27/12 ,  B32B37/1207 ,  B32B37/1284 ,  B32B2037/1223 ,  B32B2305/18 ,  B32B2307/3065 ,  B32B2315/02 ,  B32B2371/00 ,  B32B2605/18 ,  Y02T50/46

Abstract: In one of the embodiments of the disclosure, there is provided an aircraft insulation system and method for providing fire penetration resistance and/or thermal and acoustic protection. The aircraft insulation system comprises one or more insulation blankets, each having an inboard side and an outboard side. The aircraft insulation system further comprises a fire penetration resistant cover material having a heat seal adhesive, wherein the fire penetration resistant cover material covers the outboard side of the one or more insulation blankets. The aircraft insulation system further comprises an insulation cover film having a heat seal adhesive, wherein the insulation cover film covers the inboard side of the one or more insulation blankets. The aircraft insulation system further comprises a thermal heat seal that joins the fire penetration resistant cover material and the insulation cover film together to form a continuous insulation blanket assembly.

Abstract translation: 在本公开的一个实施例中，提供了一种用于提供防火穿透性和/或热和声学保护的飞行器绝缘系统和方法。 飞机绝缘系统包括一个或多个绝缘毯，每个绝缘毯具有内侧和外侧。 飞机绝缘系统还包括具有热密封粘合剂的防火穿透覆盖材料，其中耐火穿透覆盖材料覆盖一个或多个绝缘毯的外侧。 飞机绝缘系统还包括具有热封粘合剂的绝缘覆盖膜，其中所述绝缘覆盖膜覆盖所述一个或多个绝缘毯的内侧。 飞机绝缘系统还包括将防火穿透覆盖材料和绝缘覆盖膜连接在一起以形成连续绝缘毯组件的热热密封。