JPS6367680U - - Google Patents
Info
- Publication number
- JPS6367680U JPS6367680U JP16135086U JP16135086U JPS6367680U JP S6367680 U JPS6367680 U JP S6367680U JP 16135086 U JP16135086 U JP 16135086U JP 16135086 U JP16135086 U JP 16135086U JP S6367680 U JPS6367680 U JP S6367680U
- Authority
- JP
- Japan
- Prior art keywords
- engine
- compressor
- conduit
- fan case
- driven
- 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
- 238000001816 cooling Methods 0.000 claims description 3
Landscapes
- Compressor (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
Description
第１図は本考案に係るエンジンコンプレツサー
の一実施例を示す平面図であり、第２図は第１図
の実施例の要部断面図である。
１…機体、２…エンジン、３…コンプレツサー
、１８…エンジン冷却用フアン装置、１９…フア
ンケース、２５…導管、２６…サージタンク、２
７…中間部分。
FIG. 1 is a plan view showing an embodiment of an engine compressor according to the present invention, and FIG. 2 is a sectional view of a main part of the embodiment shown in FIG. DESCRIPTION OF SYMBOLS 1... Airframe, 2... Engine, 3... Compressor, 18... Engine cooling fan device, 19... Fan case, 25... Conduit, 26... Surge tank, 2
7...Middle part.
Claims (1)
駆動されるコンプレツサー３と、前記エンジンに
よつて駆動されるエンジン冷却用フアン装置１８
と、前記コンプレツサーから圧縮空気の供給を受
けるサージタンク２６と、前記コンプレツサーか
ら前記サージタンクへ圧縮空気を供給する導管２
５とを有するエンジンコンプレツサーにおいて、
前記導管２５を前記エンジン冷却用フアン装置１
８のフアンケース１９に貫通させて前記導管の中
間部分２７を前記フアンケース内の空気流路内に
延在するように配置したことを特徴とするエンジ
ンコンプレツサー。 A fuselage 1, an engine 2, a compressor 3 driven by the engine, and an engine cooling fan device 18 driven by the engine.
, a surge tank 26 that receives compressed air from the compressor, and a conduit 2 that supplies compressed air from the compressor to the surge tank.
In an engine compressor having 5,
The conduit 25 is connected to the engine cooling fan device 1.
An engine compressor characterized in that the intermediate portion 27 of the conduit is disposed so as to extend through the fan case 19 of the fan case 8 so that the intermediate portion 27 of the conduit extends into the air flow path within the fan case.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16135086U JPS6367680U (en) | 1986-10-21 | 1986-10-21 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16135086U JPS6367680U (en) | 1986-10-21 | 1986-10-21 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6367680U true JPS6367680U (en) | 1988-05-07 |
Family
ID=31087581
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP16135086U Pending JPS6367680U (en) | 1986-10-21 | 1986-10-21 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6367680U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0424680U (en) * | 1990-06-20 | 1992-02-27 |
-
1986
- 1986-10-21 JP JP16135086U patent/JPS6367680U/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0424680U (en) * | 1990-06-20 | 1992-02-27 |
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