JPH01173345U - - Google Patents
Info
- Publication number
- JPH01173345U JPH01173345U JP7047188U JP7047188U JPH01173345U JP H01173345 U JPH01173345 U JP H01173345U JP 7047188 U JP7047188 U JP 7047188U JP 7047188 U JP7047188 U JP 7047188U JP H01173345 U JPH01173345 U JP H01173345U
- Authority
- JP
- Japan
- Prior art keywords
- air
- air outlet
- exhaust
- turbine booster
- evacuator
- 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
- 238000002485 combustion reaction Methods 0.000 claims description 6
- 230000005540 biological transmission Effects 0.000 claims description 2
- 238000001816 cooling Methods 0.000 claims 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims 2
- 238000005461 lubrication Methods 0.000 claims 1
- 239000002699 waste material Substances 0.000 claims 1
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 210000003746 feather Anatomy 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
Landscapes
- Supercharger (AREA)
Description
第１図は本考案の伝動式タービン・ブーステイ
ング・エバキユエータの立体透視図。第２図は本
考案のエバキユエータの排気吸気のタービン昇圧
器の立体切開面透視図。第３図は本考案のエバキ
ユエータの加圧助燃焼のタービン昇圧器の立体切
開面透視図。第４図は本考案のエバキユエータの
排気吸収のタービン昇圧エバキユエータの立体透
視図。第５図は本考案のエバキユエータ加圧助燃
焼のタービン昇圧器の立体透視図。第６図は本考
案のエバキユエータの加圧助燃焼の圧力係数スイ
ツチトツプ切開面透視図。第７図は本考案のエバ
キユエータの加圧助燃焼のタービン昇圧器のベア
リング支えと螺形塊の結合状態切開透視図。第８
図は本考案のエバキユエータの加圧助燃焼のター
ビン昇圧器のベアリング支えと螺形塊の断面透視
図。
１，２……タービン昇圧器、３……鉄塊、４…
…圧力スイツチ、１１，２１……ベルト・ホイー
ル、１３，２３……フアン羽根、１２，２２……
フアン羽根軸、１４，２４……螺形塊。
FIG. 1 is a three-dimensional perspective view of the transmission type turbine boosting evacuator of the present invention. FIG. 2 is a three-dimensional cutaway perspective view of the turbine booster for the exhaust and intake air of the evacuator of the present invention. FIG. 3 is a three-dimensional cutaway perspective view of the pressurized auxiliary combustion turbine booster of the evacuator of the present invention. FIG. 4 is a three-dimensional perspective view of the turbine booster evacuator for exhaust gas absorption of the evacuator of the present invention. FIG. 5 is a three-dimensional perspective view of the turbine booster of the evacuator pressurized auxiliary combustion according to the present invention. FIG. 6 is a perspective view of the pressure coefficient switch top for pressurized auxiliary combustion of the evacuator of the present invention. FIG. 7 is a cutaway perspective view of the combined state of the bearing support and the spiral mass of the pressurized auxiliary combustion turbine booster of the evacuator of the present invention. 8th
The figure is a cross-sectional perspective view of the bearing support and spiral block of the pressurized auxiliary combustion turbine booster of the evacuator of the present invention. 1, 2... Turbine booster, 3... Iron ingot, 4...
...Pressure switch, 11,21...Belt wheel, 13,23...Fan blade, 12,22...
Juan feather axis, 14, 24...spiral mass.
Claims (1)
る排気用タービン昇圧器と、直接エアフイルタか
ら吸引した清浄空気をキヤブレタに供給して加圧
助燃焼作用を与える給気用タービン昇圧器とから
なり、排気用タービン昇圧器は螺形塊と風入口と
風出口とを有し、該風入口を直接エンジンの廃気
出口に接続し、該風出口を直接排気パイプに接続
し、前記螺形体内にフアン羽根を回転自在に支持
し、前記給気用タービン昇圧器は螺形塊と風入口
と風出口とを有し、該螺形塊内にフアン羽根を回
転自在に支持し、前記風出口付近に圧力スイツチ
を設け、過大圧力を逃がすことを特徴とした伝動
式タービンブーステイング・エバキユエータ。 (2) 前記排気用タービン昇圧器は二貯油槽の油
冷却と潤滑系統および貯水槽水冷却系統とを有し
、フアン羽根がエンジンより羽根軸上のベルトホ
イールに伝動し、直接空気と接触して冷却用の三
大冷却系統を形成し、該フアン羽根が自転するよ
うに構成したことを特徴とした請求項(1)記載の
エバキユエータ。 (3) 給気用タービン昇圧器の圧力スイツチは風
出口のヘツドに設置し、スプリングを本体内側に
設置したことを特徴とした請求項(1)記載のエバ
キユエータ。[Scope of Claim for Utility Model Registration] (1) An exhaust turbine booster installed at the engine exhaust pipe outlet to suck in waste air, and clean air drawn directly from the air filter to be supplied to the carburetor to provide a pressurized auxiliary combustion effect. The exhaust turbine booster has a spiral block, an air inlet, and an air outlet, the air inlet is directly connected to the exhaust air outlet of the engine, and the air outlet is connected directly to the exhaust air outlet. The air supply turbine booster has a spiral block, an air inlet, and an air outlet, and the fan blade is rotatably supported in the spiral body. A power transmission type turbine boosting evacuator, which is rotatably supported and has a pressure switch near the air outlet to release excessive pressure. (2) The exhaust turbine booster has two oil storage tank oil cooling and lubrication systems and a water storage tank water cooling system, and the fan blades are transmitted from the engine to a belt wheel on the blade shaft and come into direct contact with the air. 2. The evacuator according to claim 1, wherein three major cooling systems are formed for cooling, and the fan blades are configured to rotate on their own axis. (3) The evacuator according to claim 1, wherein the pressure switch of the air supply turbine booster is installed at the head of the air outlet, and the spring is installed inside the main body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7047188U JPH01173345U (en) | 1988-05-30 | 1988-05-30 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7047188U JPH01173345U (en) | 1988-05-30 | 1988-05-30 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH01173345U true JPH01173345U (en) | 1989-12-08 |
Family
ID=31295712
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP7047188U Pending JPH01173345U (en) | 1988-05-30 | 1988-05-30 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH01173345U (en) |
-
1988
- 1988-05-30 JP JP7047188U patent/JPH01173345U/ja active Pending