JPH0228923U - - Google Patents
Info
- Publication number
- JPH0228923U JPH0228923U JP10272988U JP10272988U JPH0228923U JP H0228923 U JPH0228923 U JP H0228923U JP 10272988 U JP10272988 U JP 10272988U JP 10272988 U JP10272988 U JP 10272988U JP H0228923 U JPH0228923 U JP H0228923U
- Authority
- JP
- Japan
- Prior art keywords
- tip
- piston
- fuel
- nozzle body
- conical hole
- 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
- 239000000446 fuel Substances 0.000 claims description 6
- 238000002347 injection Methods 0.000 claims 1
- 239000007924 injection Substances 0.000 claims 1
- 230000002093 peripheral effect Effects 0.000 claims 1
Landscapes
- Spray-Type Burners (AREA)
Description
第1図は本考案に係る一実施例を示す断面図、
第2図は第1図の部分拡大図、第3図は第1図の
―断面図、第4図は第1図の―断面図、
第5図は第1図の―断面図、第6図は従来例
を示す断面図、第7図は第6図の部分側面図であ
る。
3……シリンダ、6……円錐状の孔部、7……
オリフイス、9……針弁、10……テーパ部、1
1……筒状部、12……ピストン、16……燃料
旋回スリツト。
FIG. 1 is a sectional view showing an embodiment of the present invention;
Figure 2 is a partially enlarged view of Figure 1, Figure 3 is a sectional view of Figure 1, Figure 4 is a sectional view of Figure 1,
5 is a cross-sectional view of FIG. 1, FIG. 6 is a cross-sectional view of a conventional example, and FIG. 7 is a partial side view of FIG. 6. 3... Cylinder, 6... Conical hole, 7...
Orifice, 9...needle valve, 10...tapered part, 1
1... Cylindrical part, 12... Piston, 16... Fuel swirl slit.
Claims (1)
トン先端に延設された針弁の先端のテーパ部を、
ノズルボデイ先端に先窄まりの円錐状の孔部に連
ねて形成されたオリフイスに挿入配置し、燃料溜
まりから円錐状の孔部の内周面に、斜弁の先端の
テーパ部と基端の筒状部との境界付近に向かい且
つ斜めに開口する燃料旋回スリツトを形成する一
方、ピストンに対し針弁開方向に燃料溜まりの燃
料圧力を作用させる構成としたことを特徴とする
燃料噴射弁。 A piston is installed inside the nozzle body, and the tapered part at the tip of the needle valve extends from the tip of the piston.
It is inserted into an orifice formed in series with a tapered conical hole at the tip of the nozzle body, and the tapered part at the tip of the slanted valve and the cylinder at the base end are inserted from the fuel reservoir to the inner peripheral surface of the conical hole. What is claimed is: 1. A fuel injection valve characterized in that a fuel swirl slit is formed that opens diagonally toward the vicinity of a boundary with a shaped portion, and the fuel pressure of a fuel reservoir is applied to a piston in a direction in which a needle valve opens.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10272988U JPH0228923U (en) | 1988-08-04 | 1988-08-04 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10272988U JPH0228923U (en) | 1988-08-04 | 1988-08-04 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH0228923U true JPH0228923U (en) | 1990-02-23 |
Family
ID=31332904
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP10272988U Pending JPH0228923U (en) | 1988-08-04 | 1988-08-04 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0228923U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2000017578A1 (en) * | 1998-09-17 | 2000-03-30 | Mitsubishi Heavy Industries, Ltd. | Combustor for gas turbine |
| JP2007155170A (en) * | 2005-12-02 | 2007-06-21 | Hitachi Ltd | Fuel nozzle, gas turbine combustor, fuel nozzle for gas turbine combustor, and modification method for gas turbine combustor |
| EP2634490A1 (en) | 2012-02-28 | 2013-09-04 | Hitachi Ltd. | Gas turbine combustor |
-
1988
- 1988-08-04 JP JP10272988U patent/JPH0228923U/ja active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2000017578A1 (en) * | 1998-09-17 | 2000-03-30 | Mitsubishi Heavy Industries, Ltd. | Combustor for gas turbine |
| US6301900B1 (en) | 1998-09-17 | 2001-10-16 | Mitsubishi Heavy Industries, Ltd. | Gas turbine combustor with fuel and air swirler |
| JP2007155170A (en) * | 2005-12-02 | 2007-06-21 | Hitachi Ltd | Fuel nozzle, gas turbine combustor, fuel nozzle for gas turbine combustor, and modification method for gas turbine combustor |
| EP2634490A1 (en) | 2012-02-28 | 2013-09-04 | Hitachi Ltd. | Gas turbine combustor |
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