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JPH0483911A - Passage changeover device - Google Patents

Passage changeover device

Info

Publication number
JPH0483911A
JPH0483911A JP19772290A JP19772290A JPH0483911A JP H0483911 A JPH0483911 A JP H0483911A JP 19772290 A JP19772290 A JP 19772290A JP 19772290 A JP19772290 A JP 19772290A JP H0483911 A JPH0483911 A JP H0483911A
Authority
JP
Japan
Prior art keywords
flow
flow path
downstream
outside
engine
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
Application number
JP19772290A
Other languages
Japanese (ja)
Inventor
Hikari Takami
光 高見
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP19772290A priority Critical patent/JPH0483911A/en
Publication of JPH0483911A publication Critical patent/JPH0483911A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To achieve smooth and reliable changeover of inside outside flow in a passage to outside inside flow by pivoting upstream and downstream end portions of a first and second bucket type structure which are provided with an inclined bottom surface and both side surfaces directing to inside/outside directions in the passage as the flow advances downstream and are open downstream and upstream, and arranging those in the direction across the passage. CONSTITUTION:A first bucket type structure 1 opened to downstream side is formed of a bottom surface 1a whose upstream end is connected to an external wall 6 of an engine with a hinge line 7, and whose passage 20 is inclined toward the downstream side to make the downstream end contact with an internal wall 5 of the engine, and of side walls 1b which stand upright at each side of the bottom surface 1a and those upper ends are parallel to the flow. A second bucket type structure is formed of an inclined bottom surface 2a whose upstream end is in contact with the internal wall 5 of the engine and is pivoted to the external wall 6 of the engine with a hinge line 8, and side walls 2, and is opened to the upstream side. The first and the second bucket type structures 1, 2 are arranged alternately, allowing smooth and reliable changeover of the inside outside flow in the passage to outside inside flow without generation of pressure losses and turbulences.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、ジェットエンジンの空気流路等のRNの切換
え装置に関する。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a switching device for RN of an air flow path of a jet engine, etc.

〔従来の技術〕[Conventional technology]

従来、流路内の流れを流路外へ導き、同時に流路外の流
れを流路内へ導くような流路の切換え装置iはなかった
Conventionally, there has been no channel switching device i that guides the flow inside the channel to the outside of the channel and simultaneously guides the flow outside the channel into the channel.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

本発明は、 (1)流路内を流れる流れを流路外へ導くと同時に流路
外を流れる流れを流路内へ導く。
The present invention has the following features: (1) At the same time, the flow flowing inside the flow path is guided to the outside of the flow path, and the flow flowing outside the flow path is guided into the flow path.

(2)また、流路内を流れる流れをそのま\下流側へ流
す。
(2) Also, the flow flowing in the channel is allowed to flow directly to the downstream side.

以上の二つの流路の形態をとることができる流路の切換
え装置を提供しようとするものである。
It is an object of the present invention to provide a flow path switching device that can take the form of the above two flow paths.

〔S![を解決するための手段〕[S! [Means to solve]

本発明の流路の切換え装置は、下流側へ行くに従りて流
路内へ向うように傾斜した底面とこの底面の両側に設け
られた側壁を備え下流側へ向って開放された第1のパケ
ット状体の上流側の端部を流路壁に枢着し、下R@へ行
くに従りて流路内から流路外へ向うように傾斜した底面
とこの底面の両側に設けられた**を備え上流側へ向っ
て開放された第2のパケット状態の下流側のIli部を
流路壁に枢着し、前記第1及び第2のパケット状体を流
路を横切る方向だ並んで配置し九つ 〔作用〕 本発明では、流路外を流れる流体は、第1のパケット状
体に入り、下流側へ行くに従って流路内に向うように傾
斜し足底面に案内されて流路内へ流入する。一方、流路
内を流れb流体は、第2のパケット状体に入り、下流側
へ行くに従って流路内から流路外へ向うように傾斜し足
底面に案内されて光路外へ流出する。このようにして、
流路内の流体は流路外へ、ま急逝に流路外の流体は流路
内へと流れ、流路の切j#んが行なわれる。しかも、両
バケット内を流fる流体はその底面と側壁ととよって案
内されて流れ、flすれの障害となるものがなく、流れ
の圧カ損夫や乱れが低減される。
The flow path switching device of the present invention includes a bottom surface that slopes toward the inside of the flow path as it goes downstream, and side walls provided on both sides of this bottom surface, and a first opening that is open toward the downstream side. The upstream end of the packet-like body is pivoted to the channel wall, and a bottom surface is provided on both sides of this bottom surface, which is inclined from inside the channel to outside the channel as it goes toward the lower R@. The downstream side Ili portion of the second packet state, which is equipped with a gasket and opened toward the upstream side, is pivoted to the channel wall, and the first and second packet-like bodies are moved in a direction across the channel. In the present invention, the fluid flowing outside the flow path enters the first packet-like body, and as it goes downstream, it slopes toward the inside of the flow path and is guided to the sole surface of the foot. Flows into the flow path. On the other hand, the fluid b flowing in the channel enters the second packet-like body, and as it goes downstream, it slopes from the inside of the channel to the outside of the channel, and is guided by the sole surface of the foot and flows out of the optical path. In this way,
The fluid in the flow path flows out of the flow path, and the fluid outside the flow path flows into the flow path, and the flow path is cut. Moreover, the fluid flowing in both buckets is guided by the bottom and side walls thereof, and there is no obstacle to the flow, reducing pressure loss and turbulence in the flow.

ま几、第1及び第2のパケット状体を1それぞれの上流
Il端部と下fi側端部の枢着点1ゎりに回動すること
によって、流路の外に移動さぜると、こ几によって流路
内には、その上流側からそのま\下流側へ連続して流れ
る流体の流れが得られる、 〔実施例〕 本発明の一実施例ケ、第1図ないし第3図によって説明
する。
When the first and second packet-like bodies are moved out of the flow path by rotating them around the pivot points of the upstream Il end and the lower fi side end of each one, [Embodiment] An embodiment of the present invention, as shown in Figs. 1 to 3, allows a continuous flow of fluid from the upstream side to the downstream side in the flow path. explain.

本実施例は、第3図に示すように、上i側の第1フアン
10と下流側の第27アン11の間に、筒状のエンジン
内壁5とこれを取囲む筒状のエンジン外壁6によって形
成され之タンデムファン式のジェクトエンジンの流Nt
 20の切換え装置に係る。
In this embodiment, as shown in FIG. 3, a cylindrical engine inner wall 5 and a cylindrical engine outer wall 6 surrounding the first fan 10 on the upper i side and the 27th fan 11 on the downstream side are provided. The flow of the tandem fan type jet engine formed by Nt
20 switching devices.

第1図に示すように、第1のパケット状体1は、その上
流側の端部がエンジン外壁6上に位置し、同上流側の端
部から後光側へ行くに促って流路20内へ向うように傾
斜しその下流側の端部がエンジン内壁5に接する底面1
aと、この底面1aの両側に、同底面1aK直又して立
上Qその士酸が流れとはソ平行(第1図においてはソ水
干)を々し、かつ流れに対して平行に延びる三角形の側
壁1b、lbを備えており、同第1のパケット状体1は
下流側へ向って開放されている。ま几、この第1のパケ
ット状体1の上流側の端部は、流れに直交しエンジン外
壁6の面内にあるヒンジライン7によってエンジン外壁
6に枢着されている。
As shown in FIG. 1, the first packet-like body 1 has an upstream end located on the engine outer wall 6, and a flow path extending from the upstream end toward the halo side. A bottom surface 1 that is inclined toward the inside of the engine 20 and whose downstream end touches the engine inner wall 5.
a, and on both sides of this bottom surface 1a, the same bottom surface 1aK stands upright Q and is parallel to the flow (so-sui-dry in Figure 1), and extends parallel to the flow. It has triangular side walls 1b, lb, and the first packet-shaped body 1 is open toward the downstream side. The upstream end of this first packet-shaped body 1 is pivoted to the engine outer wall 6 by a hinge line 7 that is perpendicular to the flow and in the plane of the engine outer wall 6.

ま九、第2のパケット状体2は、その底面2aの上流側
の端部がエンジン内壁5に接し、同底面2aが下流側に
行ぐに従って流路2o内から流路外へ向うように傾斜し
て底面2aの下流側の端部がエンジン外!6上に位置す
ると共K、この底面22の両11に、同底面2aK直交
して立上シその上縁が流れとはソ平行(第1図において
はy水平)をなし、かつ流れに対して平行く延びる三角
形の2b、2bを備えており、同第2のパケット状体2
は上流側へ向って開放されているつまた、この第2のパ
ケット状体2の下流側の端部は、流れI/Ci[交しエ
ンジン外壁6の面内にあるヒンジライン8によってエン
ジン外壁6に枢着されている。
(9) The second packet-shaped body 2 is arranged such that the upstream end of its bottom surface 2a contacts the engine inner wall 5, and the bottom surface 2a extends from inside the flow path 2o to outside the flow path as it goes downstream. The downstream end of the inclined bottom surface 2a is outside the engine! 6, the upper edge of the bottom surface 2aK is perpendicular to both 11 of the bottom surface 22, and its upper edge is parallel to the flow (y-horizontal in FIG. 1), and The second packet-shaped body 2 has triangular shapes 2b and 2b extending parallel to each other.
is open toward the upstream side, and the downstream end of the second packet-shaped body 2 is connected to the engine outer wall by the hinge line 8 in the plane of the engine outer wall 6. It is pivoted to 6.

以上のような第1及び第2のパケット状体l。The first and second packet-like bodies l as described above.

2は、流路20を横切る方向に交互に並んで配置きれ、
それぞれ複数個設けられている。ま念、エンジン外!1
6は、同第1及び第2のパケット状体1.2を設けた部
分くお電ハて切欠かれている。
2 can be arranged alternately in a direction crossing the flow path 20,
Multiple pieces of each are provided. Seriously, outside the engine! 1
6 is cut out in a portion where the first and second packet-like bodies 1.2 are provided.

本実施例では、第1図(al、(blに矢印で示すよう
に、エンジン内壁5とエンジン外壁6で形成される流路
20の外を流れる気流4は、第1のパケット状体Iの、
底面1aと両側の111I壁1b。
In this embodiment, as shown by the arrows in FIGS. ,
Bottom surface 1a and 111I walls 1b on both sides.

10に案内さ几て同パケット状体1円に入り更に流路2
0内へ導入される。
10 and enters the same packet-like body 1 yen and further flows through channel 2.
Introduced into 0.

一方、第1図(a) 、 (cl K矢印で示すように
、流路20FP3ftRれる気l513は、第2のパケ
ット状体2の底面2aと両側の側壁2b、2bに案内さ
れて同パケット状体2内へ入り、更に流路2゜の外方へ
送られる。
On the other hand, as shown by the arrows in FIG. 1(a), (cl K), the air 513 flowing through the flow path 20FP3ftR is guided by the bottom surface 2a of the second packet-shaped body 2 and the side walls 2b, 2b on both sides, and flows into the same packet-shaped body 2. It enters the body 2 and is further sent to the outside of the flow path 2°.

このように、本実施例では、流路20内の気流を流路2
0外へ1次回時に流路2o外の気流を流路20内へ導い
て、流路の切換えを行なうことができる。しかも、第1
.第2のパケット状体1,2は、流れの障害となる部分
はなく、流れの圧力損失と乱れの発生を抑えることがで
きる。
In this way, in this embodiment, the airflow in the flow path 20 is
The airflow outside the flow path 2o can be guided into the flow path 20 at the primary time to switch the flow path. Moreover, the first
.. The second packet-like bodies 1 and 2 have no portions that obstruct the flow, and can suppress pressure loss and turbulence in the flow.

前記の流路の切換えを行なわない時とは、第2図に示す
ように、第1のパケット状体1をその上流側の端部のヒ
ンジライン7まわりに、第2のパケット状体2をその下
流側の端部のヒンジライン8まわりに上方へ回動して、
その底面la、lb’iエンジン外壁6の面と一致させ
る。
When the flow path is not switched, as shown in FIG. Rotate upward around the hinge line 8 at the downstream end,
Its bottom surface la and lb'i are made to coincide with the surface of the engine outer wall 6.

これによって、流路20を流れる気流は、矢印に示すよ
うに、七のま\両パケット状体1.2の設けられ九部分
全流遇して流路20の下流側へ流れる。
As a result, the airflow flowing through the flow path 20 flows toward the downstream side of the flow path 20, as shown by the arrow, with the entire nine portions of the seven packet-like bodies 1.2 being provided.

なお、前記の実施列は、タンデムファン式のジェットエ
ンジンの流路の切換え装置に係るが、本発明はこれに限
らず、ひろ〈流路を切換える必要のある場合に適用する
ことができる。
Although the above-mentioned embodiment relates to a flow path switching device for a tandem fan type jet engine, the present invention is not limited to this, and can be applied to any case where it is necessary to switch the flow path.

〔発明の効果〕〔Effect of the invention〕

以上説明し次ように、本発明では昇許請求の範囲に配板
し次構成をもつ第1及び第2のパケット状体を用いるこ
とによって、流路内の流れを流路外へ、″tfc流路外
の流れ全流路内へ案内することKよって流路の切換え全
円滑かつ確実と行なうことができ、しかもこの際におす
る鬼れの圧力損失と乱れの発生を抑えることができる。
As explained above and as follows, in the present invention, by using the first and second packet-like bodies arranged within the scope of the claims and having the following configuration, the flow within the flow path is directed to the outside of the flow path. By guiding the flow outside the flow path into the entire flow path, the flow path switching can be carried out completely smoothly and reliably, and furthermore, the pressure loss and turbulence caused at this time can be suppressed.

ま之、第1及び第2のパケット状体を枢着点まわりに回
動してTyt路外へ移動さぜることに工って、流路の切
換えを行なわす流路内の流f′Lをそのま\下流側へ流
すこともできる。
However, by rotating the first and second packet-shaped bodies around the pivot point and moving them out of the Tyt passage, the flow f' in the passage is changed. It is also possible to directly flow L to the downstream side.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は本発明の一実施例を示し、第1図(alはその
斜視図、第1図(b)及び第1図(C)はそれぞれ第1
図(alのA−A天視断面茗及びB−B矢視断面図、第
2図は同実施例のパケット状体を流路外に移動させ之場
合を示し、:1IJz図(3)はその斜視図、第2図(
bl及び(c)はそnぞれ第2図(alのC−C*視折
断面図びD−D矢視断面図、第3図は同実施例が適用さ
几るメンデムファ7式ジェットエンジンの流路の説明図
である。 1・−・第1のパケット状体、1a・・・底面、1b・
・・側壁、2・・・第2のパケット状体、2a・−・底
面2b・・・側壁、3,4・−・気流、5・・・エンジ
ン内壁6・−・エンジン外壁、7.8・・・ヒンジライ
ン、10・・・第1フアン、11・・−第2フアン、2
o・・・流路。 第10 (a)
Figure 1 shows one embodiment of the present invention, Figure 1 (al is a perspective view thereof, Figure 1 (b) and Figure 1 (C) are respectively
Figures (A-A celestial cross-section and B-B arrow cross-sectional view of al, Figure 2 shows the case where the packet-like body of the same embodiment is moved out of the flow path, Figure 1IJz (3) is Its perspective view, Figure 2 (
BL and (c) are respectively a C-C* cross-sectional view and a D-D arrow cross-sectional view of FIG. 1 is an explanatory diagram of the flow path. 1.--First packet-shaped body, 1a.. Bottom surface, 1b.
... Side wall, 2... Second packet-shaped body, 2a... Bottom surface 2b... Side wall, 3, 4... Airflow, 5... Engine inner wall 6... Engine outer wall, 7.8 ...Hinge line, 10...1st fan, 11...-2nd fan, 2
o...Flow path. Section 10 (a)

Claims (1)

【特許請求の範囲】[Claims] 下流側へ行くに従って流路内へ向うように傾斜した底面
とこの底面の両側に設けられた側壁を備え下流側へ向っ
て開放された第1のパケット状体の上流側の端部を流路
壁に枢支し、下流側へ行くに従って流路内から流路外へ
向うように傾斜した底面とこの底面の両側に設けられた
側壁を備え下流側へ向って開放された第2のパケット状
体の上流側の端部を流路壁に枢着し、前記第1及び第2
のパケット状体を流路を横切る方向に並んで配置したこ
とを特徴とする流路の切換え装置。
The upstream end of the first packet-like body, which is open toward the downstream side and has a bottom surface that slopes toward the inside of the flow path as it goes downstream, and side walls provided on both sides of this bottom surface, is defined as a flow path. A second packet-shaped second packet is pivotably supported on the wall and has a bottom surface that slopes from inside the flow path to outside the flow path as it goes downstream, and side walls provided on both sides of this bottom surface, and is open toward the downstream side. The upstream end of the body is pivotally connected to the channel wall, and the first and second
A flow path switching device characterized in that packet-like bodies are arranged side by side in a direction across the flow path.
JP19772290A 1990-07-27 1990-07-27 Passage changeover device Pending JPH0483911A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP19772290A JPH0483911A (en) 1990-07-27 1990-07-27 Passage changeover device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP19772290A JPH0483911A (en) 1990-07-27 1990-07-27 Passage changeover device

Publications (1)

Publication Number Publication Date
JPH0483911A true JPH0483911A (en) 1992-03-17

Family

ID=16379264

Family Applications (1)

Application Number Title Priority Date Filing Date
JP19772290A Pending JPH0483911A (en) 1990-07-27 1990-07-27 Passage changeover device

Country Status (1)

Country Link
JP (1) JPH0483911A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103032424A (en) * 2012-12-31 2013-04-10 中国人民解放军国防科学技术大学 Supersonic flow distribution channel and wall surface determination method thereof
CN103032423A (en) * 2012-12-31 2013-04-10 中国人民解放军国防科学技术大学 Supersonic intersecting flow channel and wall surface determination method thereof

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103032424A (en) * 2012-12-31 2013-04-10 中国人民解放军国防科学技术大学 Supersonic flow distribution channel and wall surface determination method thereof
CN103032423A (en) * 2012-12-31 2013-04-10 中国人民解放军国防科学技术大学 Supersonic intersecting flow channel and wall surface determination method thereof

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