JP6142063B1 - Rear support device for removable pressure bulkhead of jet machine - Google Patents
Rear support device for removable pressure bulkhead of jet machine Download PDFInfo
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- JP6142063B1 JP6142063B1 JP2016219210A JP2016219210A JP6142063B1 JP 6142063 B1 JP6142063 B1 JP 6142063B1 JP 2016219210 A JP2016219210 A JP 2016219210A JP 2016219210 A JP2016219210 A JP 2016219210A JP 6142063 B1 JP6142063 B1 JP 6142063B1
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- pressure bulkhead
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Abstract
【課題】 ジエット機の着脱自在圧力隔壁は、ゴム質であるため、高空から着陸にするにつれ、機体内外の気圧差がなくなり、圧力隔壁は僅かであるが垂れる。そのため、変形T型フレームに押し圧力がかかる。【解決手段】 圧力隔壁の球面頂部の後部を吊り、着陸時でも垂れ下らないようにした。これにより、変形T型フレームに押し圧力がかからないので安全である。【選択図】図2PROBLEM TO BE SOLVED: To remove a removable pressure bulkhead of a jet machine, since it is rubbery, there is no pressure difference between the inside and outside of the body as it is landed from a high altitude, and the pressure bulkhead slightly drops. Therefore, a pressing force is applied to the modified T-shaped frame. SOLUTION: The rear part of the spherical top of the pressure bulkhead is hung so that it does not sag even when landing. This is safe because no pressure is applied to the deformed T-shaped frame. [Selection] Figure 2
Description
本発明は、ジエット機の着脱自在圧力隔壁の後部支持装置に関する。 The present invention relates to a rear support device for a removable pressure bulkhead of a jet machine.
0003の先行技術文献のジエット機の着脱自在・圧力隔壁(以下圧力隔壁に畧)は、ゴム質であるため、高空から着陸するにつれ、機体内外の気圧差がなくなり、圧力隔壁は僅かであるが垂れる。
そのため、変形T型フレームに押し圧力がかかる。The detachable and pressure bulkhead (hereinafter referred to as the pressure bulkhead) of the jet machine of 0003 prior art document is rubbery, so there is no pressure difference between the inside and outside of the body as it lands from high altitude, and the pressure bulkhead is slight. Droop.
Therefore, a pressing force is applied to the modified T-shaped frame.
前記0003の圧力隔壁の変形T型フレームにかかる押し圧力は、圧力隔壁が軽量であるため、変形T型フレームの許容応力に比して微少で何ら問題にならないが、セフテイ、セフテイの理念から、圧力隔壁の押し圧力を減じ、安心感をもたせることを目的とする。 The pressure applied to the deformed T-shaped frame of the pressure partition of 0003 is small and no problem compared to the allowable stress of the deformed T-shaped frame because the pressure bulkhead is lightweight, but from the philosophy of safety, safety, The purpose is to reduce the pressure applied to the pressure bulkhead and give a sense of security.
そして、本発明は、変形T型フレームに取り付けた、圧力隔壁の球面項部の内外面の中央部を肉厚に形成し、内面の内厚に当板を当て、外面の内厚には当板より大径で、外径はテーパを形成し、該テーパに6つのボルト通し孔を開けた吊板を、2つのボルト通し孔を上側に向け対象にして当板と一体に取り付け、またテーパ方向の外板に、2列の不等辺傾斜フレームを、大径の長輪が入る間隔で取り付け、且、テーパと同様に、全周に6つのボル通し孔を開け、而して、吊板の上方2つと両側のボルト通し孔に大径のUボルトを、対する不等辺傾斜フレームには大径の長輪を取り付け、Uボルトと長輪間に細線を撚ったしなやかなワイヤロープでゆるめに吊り、ワイヤクリップで締め付けたものである。 In the present invention, the central part of the inner and outer surfaces of the spherical section of the pressure bulkhead attached to the deformed T-shaped frame is formed thick, the contact plate is applied to the inner thickness of the inner surface, and the inner thickness of the outer surface is applied. Larger than the plate, the outer diameter forms a taper, and a suspension plate with six bolt holes formed in the taper is attached to the plate with the two bolt holes facing upwards. Two rows of unequal-sided inclined frames are attached to the outer plate in the direction at intervals where large-diameter long wheels enter, and, like the taper, six bolt holes are drilled in the entire circumference, and the suspension plate Attach large diameter U-bolts to the top two bolt holes and the bolt through holes on both sides, and attach large-diameter long rings to the unequal-sided inclined frame, and loosen them with a supple wire rope twisting a thin wire between the U-bolts and the long rings. It is hung on and clamped with a wire clip.
なお、ワイヤロープは、下部側は必要ないが、状況により取り付けることを考えて、テーパと不等辺傾斜フレームに孔明けした。
また、ロープの取り付け孔は両者共6つにしたが、必要に応じて増し、ワイヤロープの数を増してもよく、ワイヤロープの代りに、ピアの線やチエンを使用してもよい。
また、不等辺傾斜フレームを1列のみ取り付け、長輪の代りにUボルトを取り付け、ワイヤロープで吊ってもよい。The wire rope does not need to be on the lower side, but in consideration of attachment depending on the situation, a taper and an unequal side inclined frame were perforated.
Further, the number of the attachment holes of the ropes is six, but the number of the wire ropes may be increased as necessary, and a peer wire or chain may be used instead of the wire rope.
Alternatively, only one row of unequal side inclined frames may be attached, U bolts may be attached instead of the long wheels, and hung with wire ropes.
本発明は、上記のように形成したので、着陸するにつれ、圧力隔壁の球面部が僅かであるが垂れ下らうとしても、ワイヤロープが支えるので、少ししか垂れない。
したがって、変形T型フレームにかかる圧力隔壁の押し圧力は軽減される。
また、この時、ワイヤーを取り付けた不等辺傾斜フレームには引っ張り荷重がかかるが、圧力隔壁は軽量であり、変形T型フレーム共々両者にかかる荷重は、許容応力より極小であるの
強度を増す効果がある。Since the present invention is formed as described above, even if the spherical surface portion of the pressure bulkhead slightly hangs down as it lands, the wire rope supports it so that it hangs only slightly.
Therefore, the pressing force of the pressure partition applied to the modified T-frame is reduced.
In addition, at this time, a tensile load is applied to the unequal-side inclined frame to which the wire is attached, but the pressure bulkhead is lightweight, and the load applied to both of the deformed T-type frames is smaller than the allowable stress.
There is an effect of increasing the strength.
また、長輪とUボルトは大径に形成し、ワイヤロープを無理なく曲がるようにしたので、ワイヤロープは傷まない。
なお、ワイヤロープは、圧力隔壁にゆるめに取り付けたので、飛行中、変形T型フレームと不等辺傾斜フレームは影響を受けないので安全である。Moreover, since the long wheel and the U-bolt are formed to have a large diameter and the wire rope is bent without difficulty, the wire rope is not damaged.
Since the wire rope is loosely attached to the pressure bulkhead, the deformed T-shaped frame and the unequal-side inclined frame are not affected during the flight, which is safe.
図中1は圧力隔壁で、変形T型フレーム2に取り付けている。
本発明においては、圧力隔壁1の球面頂部の内外を肉厚3に形成し、内面の肉厚3に当板4を当て、外面の肉厚3には、当板4より大径で、外周にテーパ6を形成し、該テーパ6に6つのボルト通し孔7を開けた吊板5を、2つのボルト通し孔7を上側に向け対象にして当板4と一体に取り付けている。
8は外板で、該外板8の内側に、2列の不等辺傾斜フレーム9をテーパ6方向に大径の長輪10が入る間隔で取り付けている。不等辺傾斜フレーム9にはテーパ6方向に6つのボルト通し孔7を開けている。
而して、吊板5の上方2つと両側のボルト通し孔7にUボルト11を取り付け、対する不等辺傾斜フレーム9のボルト通し孔7に長輪10を取り付け、Uボルト11と長輪10間にワイヤロープ12をゆるめに張り、ワイヤークリップ13で締め付けている。In the figure, reference numeral 1 denotes a pressure partition, which is attached to the modified T-
In the present invention, the inner surface and outer surface of the spherical surface of the pressure bulkhead 1 are formed to have a thickness of 3, the
Reference numeral 8 denotes an outer plate, and two rows of unequal-side inclined frames 9 are attached to the inner side of the outer plate 8 at intervals at which large-diameter
Thus, U bolts 11 are attached to the upper two of the suspension plate 5 and the bolt through
なおUボルト11と長輪10は軽量化するため、中空材で形成したがよい。 The U bolt 11 and the
1 着脱自在圧力隔壁
2 変形T型フレーム
3 肉厚
4 当板
5 吊板
6 テーパ
7 ボルト通し孔
8 外板
9 不等辺傾斜フレーム
10 長輪
11 Uボルト
12 ワイヤロープ
13 ワイヤクリップDESCRIPTION OF SYMBOLS 1
Claims (3)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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JP2016219210A JP6142063B1 (en) | 2016-09-29 | 2016-09-29 | Rear support device for removable pressure bulkhead of jet machine |
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JP2016219210A JP6142063B1 (en) | 2016-09-29 | 2016-09-29 | Rear support device for removable pressure bulkhead of jet machine |
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JP6142063B1 true JP6142063B1 (en) | 2017-06-07 |
JP2018052476A JP2018052476A (en) | 2018-04-05 |
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JP2016219210A Expired - Fee Related JP6142063B1 (en) | 2016-09-29 | 2016-09-29 | Rear support device for removable pressure bulkhead of jet machine |
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Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2009541131A (en) * | 2006-06-26 | 2009-11-26 | エアバス・オペレーションズ・ゲーエムベーハー | Pressure bulkhead for aerospace aircraft |
JP2015006872A (en) * | 2013-06-12 | 2015-01-15 | ザ・ボーイング・カンパニーTheBoeing Company | Self-balancing pressure bulkhead |
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 |
EP2886444A1 (en) * | 2013-12-20 | 2015-06-24 | Airbus SAS | Folding pressure bulkhead for aircraft, and aircraft provided with such a pressure bulkhead |
US20160257393A1 (en) * | 2015-03-06 | 2016-09-08 | Airbus Operations Gmbh | Pressure bulkhead adapted to non-cirular fuselage section |
US20160288896A1 (en) * | 2015-04-03 | 2016-10-06 | The Boeing Company | Tool and method of installing a bulkhead within a structure |
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2016
- 2016-09-29 JP JP2016219210A patent/JP6142063B1/en not_active Expired - Fee Related
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2009541131A (en) * | 2006-06-26 | 2009-11-26 | エアバス・オペレーションズ・ゲーエムベーハー | Pressure bulkhead for aerospace aircraft |
JP2015006872A (en) * | 2013-06-12 | 2015-01-15 | ザ・ボーイング・カンパニーTheBoeing Company | Self-balancing pressure bulkhead |
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 |
EP2886444A1 (en) * | 2013-12-20 | 2015-06-24 | Airbus SAS | Folding pressure bulkhead for aircraft, and aircraft provided with such a pressure bulkhead |
US20160257393A1 (en) * | 2015-03-06 | 2016-09-08 | Airbus Operations Gmbh | Pressure bulkhead adapted to non-cirular fuselage section |
US20160288896A1 (en) * | 2015-04-03 | 2016-10-06 | The Boeing Company | Tool and method of installing a bulkhead within a structure |
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Publication number | Publication date |
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JP2018052476A (en) | 2018-04-05 |
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