JPH01180400U - - Google Patents
Info
- Publication number
- JPH01180400U JPH01180400U JP7772688U JP7772688U JPH01180400U JP H01180400 U JPH01180400 U JP H01180400U JP 7772688 U JP7772688 U JP 7772688U JP 7772688 U JP7772688 U JP 7772688U JP H01180400 U JPH01180400 U JP H01180400U
- Authority
- JP
- Japan
- Prior art keywords
- fuselage
- spar
- frame
- windows
- window
- 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
- 230000003014 reinforcing effect Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 5
- 230000002787 reinforcement Effects 0.000 description 1
Description
第１図は本考案の一実施例の航空機の概念図、
第２図は同実施例の窓とその周辺部分の説明図、
第３図は胴体に働くせん断力の説明図、第４図は
上記実施例の窓補強部の変形を示す説明図、第５
図は従来の四角窓の説明図である。
２…フレーム、３…ストリンガー、４…三角窓
、４ａ，４ｂ，４ｃ…三角窓の辺、５…斜材、１
０…胴体、１１…主翼、１１ａ…主翼前桁、１１
ｂ…主翼後桁。
FIG. 1 is a conceptual diagram of an aircraft according to an embodiment of the present invention.
Fig. 2 is an explanatory diagram of the window and its surrounding parts in the same embodiment;
FIG. 3 is an explanatory diagram of the shear force acting on the fuselage, FIG. 4 is an explanatory diagram showing the deformation of the window reinforcement part of the above embodiment, and FIG.
The figure is an explanatory diagram of a conventional square window. 2... Frame, 3... Stringer, 4... Triangular window, 4a, 4b, 4c... Triangular window side, 5... Diagonal material, 1
0... Fuselage, 11... Main wing, 11a... Main wing front spar, 11
b... Main wing rear spar.
Claims (1)
し、同三角形のほゞ直角の内角を形成する一辺が
上下方向に、同ほゞ直角の内角を形成する他の一
方の辺が先方に向つてそれぞれ配置された複数の
窓を設け、主翼後桁より後方の胴体にほゞ直角三
角形をなし、同三角形のほゞ直角の内角を形成す
る一辺が上下方向に、同ほゞ直角の内角形を形成
する他の一辺が後方に向つてそれぞれ配置された
複数の窓を設け、上記主翼前桁より先方の窓及び
主翼後桁より後方の窓の各々の周辺に上下方向の
フレーム、水平方向のストリンガ及び上記フレー
ムとストリンガに連結された斜材で窓を取囲んだ
補強部を設けたことを特徴とする三角窓をもつ航
空機。 The fuselage beyond the front wing spar has a nearly right-angled triangle, with one side of the triangle that forms a nearly right-angled interior angle pointing vertically, and the other side that forms a nearly right-angled interior angle facing forward. The fuselage behind the rear spar of the main wing is provided with a plurality of windows, each of which has a rectangular shape, forming an almost right-angled triangle in the fuselage. A plurality of windows are provided with the other side facing rearward, and a frame in the vertical direction and a frame in the horizontal direction are installed around each of the windows ahead of the front spar of the main wing and the window behind the rear spar of the main wing. An aircraft having a triangular window, characterized in that it is provided with a reinforcing part that surrounds the window with a stringer and a diagonal member connected to the frame and the stringer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7772688U JPH01180400U (en) | 1988-06-14 | 1988-06-14 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7772688U JPH01180400U (en) | 1988-06-14 | 1988-06-14 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH01180400U true JPH01180400U (en) | 1989-12-26 |
Family
ID=31302691
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP7772688U Pending JPH01180400U (en) | 1988-06-14 | 1988-06-14 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH01180400U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009531226A (en) * | 2006-03-29 | 2009-09-03 | エアバス・ユ―ケ―・リミテッド | Aircraft fuselage internal structure |
| JP2010514628A (en) * | 2007-01-05 | 2010-05-06 | エアバス フランス | Aircraft with an aircraft fuselage section and one such section |
-
1988
- 1988-06-14 JP JP7772688U patent/JPH01180400U/ja active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009531226A (en) * | 2006-03-29 | 2009-09-03 | エアバス・ユ―ケ―・リミテッド | Aircraft fuselage internal structure |
| JP2010514628A (en) * | 2007-01-05 | 2010-05-06 | エアバス フランス | Aircraft with an aircraft fuselage section and one such section |
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