JPS6297100U - - Google Patents
Info
- Publication number
- JPS6297100U JPS6297100U JP19232885U JP19232885U JPS6297100U JP S6297100 U JPS6297100 U JP S6297100U JP 19232885 U JP19232885 U JP 19232885U JP 19232885 U JP19232885 U JP 19232885U JP S6297100 U JPS6297100 U JP S6297100U
- Authority
- JP
- Japan
- Prior art keywords
- lighter
- reinforced
- bonding
- adhesive
- utility
- 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
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 3
- 239000004917 carbon fiber Substances 0.000 claims description 3
- 239000000853 adhesive Substances 0.000 claims 1
- 230000001070 adhesive effect Effects 0.000 claims 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 239000004744 fabric Substances 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
Landscapes
- Woven Fabrics (AREA)
Description
第1図は球面状をなす航空機客室後部の圧力隔
壁の外側正面図にて、
1……同隔壁を構成する18枚のパネル板、2
……同パネル板の補強用骨材(1周の一部)、3
……同パネル板の抱え式補強の「たが」、4……
本案による圧力隔壁に接着の炭素繊維布(1周の
一部)、5……本案に於て炭素繊維の糸を用いた
ところ(1周の一部)。
第2図は圧力隔壁を横より見た断面。
Figure 1 is an external front view of the spherical pressure bulkhead at the rear of the aircraft cabin, showing 1...the 18 panels that make up the bulkhead, 2
... Reinforcing aggregate for the same panel board (part of one circumference), 3
...Hoplet type reinforcement of the same panel board, 4...
Carbon fiber cloth bonded to the pressure bulkhead according to the present invention (part of one circumference), 5... Where carbon fiber thread was used in the present invention (part of one circumference). Figure 2 is a cross section of the pressure bulkhead viewed from the side.
Claims (1)
剤をもつて接着し補強した航空機の圧力隔壁。 Aircraft pressure bulkheads reinforced by bonding lighter and stronger carbon fibers with adhesive on the outside or inside.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP19232885U JPS6297100U (en) | 1985-12-09 | 1985-12-09 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP19232885U JPS6297100U (en) | 1985-12-09 | 1985-12-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS6297100U true JPS6297100U (en) | 1987-06-20 |
Family
ID=31147302
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP19232885U Pending JPS6297100U (en) | 1985-12-09 | 1985-12-09 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6297100U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20150014843A (en) * | 2013-07-30 | 2015-02-09 | 더 보잉 컴파니 | Natural-path tearstraps and stiffeners for spherical or near-spherical composite pressure bulkheads |
-
1985
- 1985-12-09 JP JP19232885U patent/JPS6297100U/ja active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20150014843A (en) * | 2013-07-30 | 2015-02-09 | 더 보잉 컴파니 | Natural-path tearstraps and stiffeners for spherical or near-spherical composite pressure bulkheads |
JP2015027873A (en) * | 2013-07-30 | 2015-02-12 | ザ・ボーイング・カンパニーTheBoeing Company | Natural-path tearstraps and stiffeners for spherical composite pressure bulkheads |
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