JPS63148092U - - Google Patents
Info
- Publication number
- JPS63148092U JPS63148092U JP4066887U JP4066887U JPS63148092U JP S63148092 U JPS63148092 U JP S63148092U JP 4066887 U JP4066887 U JP 4066887U JP 4066887 U JP4066887 U JP 4066887U JP S63148092 U JPS63148092 U JP S63148092U
- Authority
- JP
- Japan
- Prior art keywords
- chamber
- fuel
- piston
- combustion
- bolt shaft
- 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 10
- 238000002485 combustion reaction Methods 0.000 claims description 8
- 239000003380 propellant Substances 0.000 claims description 3
- 239000000567 combustion gas Substances 0.000 claims 2
- 239000007788 liquid Substances 0.000 claims 1
Landscapes
- Combustion Methods Of Internal-Combustion Engines (AREA)
Description
第１図は本考案の飛翔体推進薬燃焼装置の一実
施例の断面図である。
１……砲身、２……砲尾環、２ｂ……内筒部、
３……ピストン、４……遊底軸、ｂ……燃料室、
ｃ……ピストン室、２ａ……燃焼室Ｂ、ａ……弁
部、４ａ……ガス流入孔。
FIG. 1 is a sectional view of an embodiment of the projectile propellant combustion device of the present invention. 1... gun barrel, 2... breech ring, 2b... inner cylinder part,
3... Piston, 4... Bolt shaft, b... Fuel chamber,
c... Piston chamber, 2a... Combustion chamber B, a... Valve section, 4a... Gas inflow hole.
Claims (1)
形成すると共にその内筒部にピストンと遊底軸を
摺動すべく嵌合し、このピストンの前側と後側に
は燃料室とピストン室とを形成し、この燃料室に
は１液式の燃料を供給し、この遊底軸の前部には
燃焼室と燃料室間を開閉する弁部を形成すると共
に遊底軸に燃焼ガス流入孔を設けて燃焼室とピス
トン室とを連通させ、燃焼室の燃焼ガスをピスト
ン室に導いてピストンを滑動させて燃料室内の燃
料を断熱圧縮し、次にこの燃料室内の燃料を燃焼
室内に送つて燃焼させることを特徴とする飛翔体
推進薬燃焼装置。 A combustion chamber is formed in the inner cylinder part of the breech ring connected to the gun barrel, and a piston and bolt shaft are slidably fitted into the inner cylinder part, and a fuel chamber and a fuel chamber are provided on the front and rear sides of this piston. A piston chamber is formed, and one-liquid fuel is supplied to this fuel chamber, and a valve part that opens and closes between the combustion chamber and the fuel chamber is formed in the front part of this bolt shaft, and combustion gas flows into the bolt shaft. A hole is provided to communicate the combustion chamber and the piston chamber, and the combustion gas in the combustion chamber is guided to the piston chamber, the piston is slid to adiabatically compress the fuel in the fuel chamber, and then the fuel in the fuel chamber is transferred into the combustion chamber. A projectile propellant combustion device characterized by sending and combusting a flying propellant.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4066887U JPS63148092U (en) | 1987-03-18 | 1987-03-18 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP4066887U JPS63148092U (en) | 1987-03-18 | 1987-03-18 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS63148092U true JPS63148092U (en) | 1988-09-29 |
Family
ID=30854955
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP4066887U Pending JPS63148092U (en) | 1987-03-18 | 1987-03-18 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS63148092U (en) |
-
1987
- 1987-03-18 JP JP4066887U patent/JPS63148092U/ja active Pending