CN104314706B - Accurate Solid liquid propellant rocket Protective system peculiar to vessel - Google Patents
Accurate Solid liquid propellant rocket Protective system peculiar to vessel Download PDFInfo
- Publication number
- CN104314706B CN104314706B CN201410574736.XA CN201410574736A CN104314706B CN 104314706 B CN104314706 B CN 104314706B CN 201410574736 A CN201410574736 A CN 201410574736A CN 104314706 B CN104314706 B CN 104314706B
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- Prior art keywords
- peculiar
- propellant rocket
- liquid propellant
- solid liquid
- firing chamber
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- 239000007788 liquid Substances 0.000 title claims abstract description 28
- 230000001681 protective effect Effects 0.000 title claims abstract description 23
- 239000007787 solid Substances 0.000 title claims abstract description 22
- 239000003380 propellant Substances 0.000 title claims abstract description 21
- 238000010304 firing Methods 0.000 claims abstract description 25
- 239000000945 filler Substances 0.000 claims abstract description 14
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims abstract description 7
- 239000001301 oxygen Substances 0.000 claims abstract description 7
- 229910052760 oxygen Inorganic materials 0.000 claims abstract description 7
- 239000004449 solid propellant Substances 0.000 claims abstract description 7
- 239000000843 powder Substances 0.000 claims abstract description 6
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 7
- 239000007789 gas Substances 0.000 claims description 4
- 238000005457 optimization Methods 0.000 description 4
- 239000007800 oxidant agent Substances 0.000 description 2
- 238000006557 surface reaction Methods 0.000 description 2
- 240000007594 Oryza sativa Species 0.000 description 1
- 235000007164 Oryza sativa Nutrition 0.000 description 1
- 238000000889 atomisation Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 235000009566 rice Nutrition 0.000 description 1
Landscapes
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
Accurate Solid liquid propellant rocket Protective system peculiar to vessel; The present invention relates to the hull protective equipment that a kind of ship is special; The invention provides a kind of peculiar to vessel accurate Solid liquid propellant rocket Protective system with safeguard function, comprise ejector filler 1, firing chamber 2, control system 3, supply system 4, jet pipe 5, tank 6, parachute 7, it is characterized in that: described ejector filler 1 connects firing chamber 2 and tank 6, described firing chamber 2 in-built oxygen deprivation solid fuel powder column, described control system 3 connects steamer bridge control system and has wire to connect supply system 4.The present invention has safeguard function, can avoid this steamer by all around or other direction come steamer clash into.
Description
Technical field
The present invention relates to the hull protective equipment that a kind of ship is special, especially belong to a kind of accurate Solid liquid propellant rocket Protective system with safeguard function being used in steamer.
Background technique
Prior art and product lack this steamer of protection carry out by front and back the function that steamer clashes into.As motorboat, speedboat tonnage are little, the speed of a ship or plane is high, runs into ship and the situation be knocked is difficult to timely haul off.
Summary of the invention
For the deficiencies in the prior art, the invention provides a kind of accurate Solid liquid propellant rocket Protective system peculiar to vessel, may be used for protecting this steamer and avoid being clashed into by the steamer at the steamer in front or rear, or avoid this steamer to be clashed into by the steamer of front and back two side simultaneously.
Its technological scheme is: a kind of peculiar to vessel accurate Solid liquid propellant rocket Protective system with safeguard function, comprise ejector filler 1, firing chamber 2, control system 3, supply system 4, jet pipe 5, tank 6, it is characterized in that: described ejector filler 1 connects firing chamber 2 and tank 6, described firing chamber 2 in-built oxygen deprivation solid fuel powder column, described control system 3 connects steamer bridge control system and has wire to connect supply system 4, described supply system 4 connects tank 6, described jet pipe 5 is led to outside by firing chamber, the spout of jet pipe 5 becomes Vertical direction with the water surface, described tank 6 carrying liquid oxygenant.
As optimization, a kind of peculiar to vessel accurate Solid liquid propellant rocket Protective system with safeguard function of the present invention, is characterized in that: described jet pipe has 4.
As optimization, a kind of peculiar to vessel accurate Solid liquid propellant rocket Protective system with safeguard function of the present invention, is characterized in that: also install parachute 7 additional and have wire connection control system 3, has and makes steamer in the buffer function fallen by safety and stability after having sprayed.
As optimization, a kind of peculiar to vessel accurate Solid liquid propellant rocket Protective system with safeguard function of the present invention, is characterized in that: described supply system 4 comprises pressurized gas cylinder and decompressor starts valve.
As optimization, a kind of peculiar to vessel accurate Solid liquid propellant rocket Protective system with safeguard function of the present invention, is characterized in that: described in there is the peculiar to vessel accurate Solid liquid propellant rocket Protective system of safeguard function for speedboat.
Working principle of the present invention: 1, when finding that front or rear have steamer will clash into epicycle ship time in traveling way, driver starts control system 3 of the present invention in time, the pressurized gas cylinder of supply system 4 and decompressor start valve and the liquid oxidizer etc. in tank 6 are injected firing chamber 2 by ejector filler 1, liquid-solid body fuel combination generates products of combustion through atomization, mixing, burning, discharged at a high speed by jet pipe 5 and produce thrust, this steamer is raised more than 2-10 rice by the water surface reaction force produced, and avoids being clashed into by the steamer at front or rear and causing security incident; 2, after this steamer raises by water surface reaction force, driver releases a parachute 7 by control system, allows the gently stable landing of this steamer.
Advantage of the present invention: 1, there is safeguard function, can avoid this steamer by all around or other direction come steamer clash into, solve prior art lack protection this steamer by all around or other direction come steamer clash into cause steamer damage and produce safety problem; 2, safety coefficient is higher, and this steamer can be avoided to be clashed into simultaneously by the steamer at steamer front and rear; 3, parachute is installed, can allows the stable landing of this steamer; 4, use oxygen deprivation solid fuel, still can maintain burning when liquid oxidizer stops completely, produce thrust.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
In figure: ejector filler 1, firing chamber 2, control system 3, supply system 4, jet pipe 5 and tank 6, parachute 7.
Embodiment
Below embodiments of the invention are described in detail by reference to the accompanying drawings.
embodiment 1:as shown in Figure 1, a kind of peculiar to vessel accurate Solid liquid propellant rocket Protective system with safeguard function, comprise ejector filler 1, firing chamber 2, control system 3, supply system 4, jet pipe 5, tank 6, it is characterized in that: described ejector filler 1 connects firing chamber 2 and tank 6, described firing chamber 2 in-built oxygen deprivation solid fuel powder column, described control system 3 connects steamer bridge control system and has wire to connect supply system 4, described supply system 4 connects tank 6, described jet pipe 5 is led to outside by firing chamber, the spout of jet pipe 5 becomes Vertical direction with the water surface, described tank 6 carrying liquid oxygenant.
embodiment 2:as shown in Figure 1, a kind of peculiar to vessel accurate Solid liquid propellant rocket Protective system with safeguard function, comprise ejector filler 1, firing chamber 2, control system 3, supply system 4, jet pipe 5, tank 6, it is characterized in that: described ejector filler 1 connects firing chamber 2 and tank 6, described firing chamber 2 in-built oxygen deprivation solid fuel powder column, described control system 3 connects steamer bridge control system and has wire to connect supply system 4, described supply system 4 connects tank 6, supply system 4 comprises pressurized gas cylinder and decompressor starts valve, described jet pipe 5 is led to outside by firing chamber, the spout of jet pipe 5 becomes Vertical direction with the water surface, described tank 6 carrying liquid oxygenant.
embodiment 3:a kind of peculiar to vessel accurate Solid liquid propellant rocket Protective system with safeguard function, comprise ejector filler 1, firing chamber 2, control system 3, supply system 4, jet pipe 5, tank 6, parachute 7, it is characterized in that: described ejector filler 1 connects firing chamber 2 and tank 6, described firing chamber 2 in-built oxygen deprivation solid fuel powder column, described control system 3 connects steamer bridge control system and has wire to connect supply system 4, described supply system 4 connects tank 6, described jet pipe 5 is led to outside by firing chamber, the spout of jet pipe 5 becomes Vertical direction with the water surface, described tank 6 carrying liquid oxygenant, described parachute 7 is arranged on ship top and has wire connection control system 3.
Claims (5)
1. one kind has the peculiar to vessel accurate Solid liquid propellant rocket Protective system of safeguard function, comprise ejector filler (1), firing chamber (2), control system (3), supply system (4), jet pipe (5), tank (6), it is characterized in that: described ejector filler (1) connects firing chamber (2) and tank (6), described firing chamber (2) in-built oxygen deprivation solid fuel powder column, described control system (3) connects steamer bridge control system and has wire to connect supply system (4), described supply system (4) connects tank (6), described jet pipe (5) is led to outside by firing chamber, the spout of jet pipe (5) becomes Vertical direction with the water surface, described tank (6) carrying liquid oxygenant.
2. there is the peculiar to vessel accurate Solid liquid propellant rocket Protective system of safeguard function according to claim 1, it is characterized in that: described jet pipe (5) has 4.
3. there is the peculiar to vessel accurate Solid liquid propellant rocket Protective system of safeguard function according to claim 1, it is characterized in that: also install parachute (7) additional and have wire connection control system (3).
4. there is the peculiar to vessel accurate Solid liquid propellant rocket Protective system of safeguard function according to claim 1, it is characterized in that: described supply system (4) comprises pressurized gas cylinder and decompressor starts valve.
5. there is the peculiar to vessel accurate Solid liquid propellant rocket Protective system of safeguard function according to claim 1, it is characterized in that: described in there is the peculiar to vessel accurate Solid liquid propellant rocket Protective system of safeguard function for speedboat.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410574736.XA CN104314706B (en) | 2014-10-25 | 2014-10-25 | Accurate Solid liquid propellant rocket Protective system peculiar to vessel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410574736.XA CN104314706B (en) | 2014-10-25 | 2014-10-25 | Accurate Solid liquid propellant rocket Protective system peculiar to vessel |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104314706A CN104314706A (en) | 2015-01-28 |
| CN104314706B true CN104314706B (en) | 2016-03-30 |
Family
ID=52369998
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410574736.XA Active CN104314706B (en) | 2014-10-25 | 2014-10-25 | Accurate Solid liquid propellant rocket Protective system peculiar to vessel |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104314706B (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2187585Y (en) * | 1993-05-18 | 1995-01-18 | 胡文宇 | Air jet bump-proof device for ship |
| US5797260A (en) * | 1995-05-11 | 1998-08-25 | Societe Europeenne De Propulsion | Pulse rocket engine |
| CN2424074Y (en) * | 1999-11-05 | 2001-03-21 | 邱刚 | Hover marine with side puff port on its hull |
| CN2548902Y (en) * | 2002-06-11 | 2003-05-07 | 张弘迅 | Hovercraft boat |
-
2014
- 2014-10-25 CN CN201410574736.XA patent/CN104314706B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2187585Y (en) * | 1993-05-18 | 1995-01-18 | 胡文宇 | Air jet bump-proof device for ship |
| US5797260A (en) * | 1995-05-11 | 1998-08-25 | Societe Europeenne De Propulsion | Pulse rocket engine |
| CN2424074Y (en) * | 1999-11-05 | 2001-03-21 | 邱刚 | Hover marine with side puff port on its hull |
| CN2548902Y (en) * | 2002-06-11 | 2003-05-07 | 张弘迅 | Hovercraft boat |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104314706A (en) | 2015-01-28 |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| CB03 | Change of inventor or designer information |
Inventor after: Luo Hua Inventor after: Luo Shizhuo Inventor after: Li Weijun Inventor before: Luo Hua Inventor before: Luo Shizhuo Inventor before: Deng Ruiping |
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| COR | Change of bibliographic data | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20160218 Address after: 542600 the Guangxi Zhuang Autonomous Region City, Zijin Mountain, Zijin Mountain Town, South Hing Road, No., science and Technology Bureau, building 2, building 22 Applicant after: Li Weijun Address before: 542600 the Guangxi Zhuang Autonomous Region, Zijin Mountain, Zijin Mountain, town, Xing Zhong Road, No. 22 Applicant before: Luo Hua |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190228 Address after: 225321 No. 11 Xuzhuang Xingwang Road, Gaogang District, Taizhou City, Jiangsu Province Patentee after: Sun Jianchun Address before: 542600 2nd Floor, Science and Technology Bureau, 22 Xingzhong South Road, Zhongshan Town, Zhongshan County, Hezhou City, Guangxi Zhuang Autonomous Region Patentee before: Li Weijun |
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| TR01 | Transfer of patent right | ||
| CP02 | Change in the address of a patent holder |
Address after: 225321 Jiangsu city of Taizhou province high port Street City Road No. 21 Patentee after: Sun Jianchun Address before: 225321 No. 11 Xuzhuang Xingwang Road, Gaogang District, Taizhou City, Jiangsu Province Patentee before: Sun Jianchun |
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| CP02 | Change in the address of a patent holder | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20221228 Address after: 276000 NO.119 Jinhu Industrial Park, West Jiefang Road, high tech Zone, Linyi City, Shandong Province Patentee after: Luyake Fire Vehicle Manufacturing Co.,Ltd. Address before: 21 Gangcheng Road, Gangkou street, Gaogang District, Taizhou City, Jiangsu Province Patentee before: Sun Jianchun |
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| TR01 | Transfer of patent right |