JPS6432995A - Interior structure for aircraft - Google Patents
Interior structure for aircraftInfo
- Publication number
- JPS6432995A JPS6432995A JP18892887A JP18892887A JPS6432995A JP S6432995 A JPS6432995 A JP S6432995A JP 18892887 A JP18892887 A JP 18892887A JP 18892887 A JP18892887 A JP 18892887A JP S6432995 A JPS6432995 A JP S6432995A
- Authority
- JP
- Japan
- Prior art keywords
- shape
- reinforcements
- aircraft
- fiber
- hours
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Abstract
PURPOSE: To reduce the man-hours by fitting plate-shaped polyetherimide on both sides of a frame in which fiber-reinforced bar-shaped reinforcements are vertically and horizontally assembled in a plane shape, and by integrally filling a foam material therebetween. CONSTITUTION: Reinforcements 12 of a fiber-reinforced bar shape (pipe shape) are vertically and horizontally assembled in a lane shape (truss shape), and is fixed by means of fittings 16 for constituting a frame 13. Next, polyetherimides 14a, 14b formed in a plate shape having a high strength and capable of satisfying the combustion test specification, are fitted to both the side surfaces of the reinforcements 12, and a foam material 15 for heat-insulating and sound-proofing is filled therebetween, and between the reinforcements 12 so that the interior material 11 for an aircraft can be integrally manufactured. Thus, the working man-hours can be remarkably reduced, and also the combustion test specification (FAA) can be satisfied.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP18892887A JPS6432995A (en) | 1987-07-30 | 1987-07-30 | Interior structure for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP18892887A JPS6432995A (en) | 1987-07-30 | 1987-07-30 | Interior structure for aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6432995A true JPS6432995A (en) | 1989-02-02 |
Family
ID=16232342
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP18892887A Pending JPS6432995A (en) | 1987-07-30 | 1987-07-30 | Interior structure for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6432995A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH04218493A (en) * | 1989-12-26 | 1992-08-10 | Florida Internatl Univ | Airframe of aircraft, method of reinforcing sheathing wall of airframe and barrier structure |
| WO2014150336A3 (en) * | 2013-03-15 | 2014-11-06 | National Nonwovens Inc. | Composites comprising nonwoven structures and foam |
| US9314993B2 (en) | 2013-03-15 | 2016-04-19 | National Nonwovens Inc. | Composites and articles made from nonwoven structures |
-
1987
- 1987-07-30 JP JP18892887A patent/JPS6432995A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH04218493A (en) * | 1989-12-26 | 1992-08-10 | Florida Internatl Univ | Airframe of aircraft, method of reinforcing sheathing wall of airframe and barrier structure |
| WO2014150336A3 (en) * | 2013-03-15 | 2014-11-06 | National Nonwovens Inc. | Composites comprising nonwoven structures and foam |
| US9314995B2 (en) | 2013-03-15 | 2016-04-19 | National Nonwovens Inc. | Composites comprising nonwoven structures and foam |
| US9314993B2 (en) | 2013-03-15 | 2016-04-19 | National Nonwovens Inc. | Composites and articles made from nonwoven structures |
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