CN104373249A - Hybrid propellant rocket protective equipment for ship - Google Patents
Hybrid propellant rocket protective equipment for ship Download PDFInfo
- Publication number
- CN104373249A CN104373249A CN201410574717.7A CN201410574717A CN104373249A CN 104373249 A CN104373249 A CN 104373249A CN 201410574717 A CN201410574717 A CN 201410574717A CN 104373249 A CN104373249 A CN 104373249A
- Authority
- CN
- China
- Prior art keywords
- protective equipment
- vessel
- firing chamber
- propellant rocket
- control system
- 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.)
- Granted
Links
- 239000003380 propellant Substances 0.000 title claims abstract description 45
- 230000001681 protective effect Effects 0.000 title claims abstract description 24
- 239000007788 liquid Substances 0.000 claims abstract description 29
- 238000010304 firing Methods 0.000 claims description 27
- 239000000945 filler Substances 0.000 claims description 12
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 7
- 239000004449 solid propellant Substances 0.000 claims description 5
- 238000002485 combustion reaction Methods 0.000 abstract description 4
- 238000002347 injection Methods 0.000 abstract 1
- 239000007924 injection Substances 0.000 abstract 1
- 238000005457 optimization Methods 0.000 description 4
- 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
- 230000007812 deficiency Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000007800 oxidant agent Substances 0.000 description 1
- 235000009566 rice Nutrition 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
Landscapes
- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
Abstract
The invention relates to hybrid propellant rocket protective equipment for a ship. The hybrid propellant rocket protective equipment has the protection function and comprises an injector (1), a combustion chamber (2), a control system (3), a liquid propellant supply system (4), an injection pipe (5) and a storage box (6). The hybrid propellant rocket protective equipment is characterized in that the injector (1) is connected with the combustion chamber (2) and the storage box (6), the combustion chamber (2) is filled with grains, and the control system (3) is connected with a ship cab control system and connected with the liquid propellant supply system (4) through a wire. The hybrid propellant rocket protective equipment for the ship has the protection function and can protect the ship against the collision of a ship in front of the ship or behind the ship.
Description
Technical field
The present invention relates to a kind of rocket protective equipment peculiar to vessel protecting steamer and be knocked, especially belong to a kind of hybrid propellant rocket protective equipment 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 hybrid propellant rocket protective equipment 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 hybrid propellant rocket protective equipment peculiar to vessel with safeguard function, comprise ejector filler 1, firing chamber 2, control system 3, liquid propellant supply system 4, jet pipe 5, tank 6, it is characterized in that: described ejector filler 1 connects firing chamber 2 and tank 6, charge pole in described firing chamber 2, solid fuel is seated in firing chamber 2, described control system 3 connects steamer bridge control system and has wire to connect liquid propellant feed system 4, described liquid propellant 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 hybrid propellant rocket protective equipment peculiar to vessel with safeguard function of the present invention, is characterized in that: described jet pipe 5 has 4.
As optimization, a kind of hybrid propellant rocket protective equipment peculiar to vessel with safeguard function of the present invention, is characterized in that: be also provided with parachute 7 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 hybrid propellant rocket protective equipment peculiar to vessel with safeguard function of the present invention, is characterized in that: described in there is the hybrid propellant rocket protective equipment peculiar to vessel of safeguard function for speedboat.
As optimization, a kind of hybrid propellant rocket protective equipment peculiar to vessel with safeguard function of the present invention, is characterized in that: described liquid propellant supply system 4 comprises pressurized gas cylinder and decompressor starts valve.
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 liquid propellant supply system 4 and decompressor start valve and the liquid oxidizer etc. in tank 6 are injected firing chamber 2 by ejector filler 1, solid-liquid fuel combination is through atomization, mixing, burning generates products of combustion, discharged at a high speed by jet pipe 5 and produce thrust, this steamer is raised more than 2-3 rice by the water surface reaction force produced, avoid 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 carry out the shock of steamer, solve prior art lack this steamer of protection by all around or other direction carry out steamer and clash into and cause steamer to damage and the safety problem that produces; 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.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
In figure: ejector filler 1, firing chamber 2, control system 3, liquid propellant 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 hybrid propellant rocket protective equipment peculiar to vessel with safeguard function, comprise ejector filler 1, firing chamber 2, control system 3, liquid propellant supply system 4, jet pipe 5, tank 6, it is characterized in that: described ejector filler 1 connects firing chamber 2 and tank 6, charge pole in described firing chamber 2, solid fuel is seated in firing chamber 2, described control system 3 connects steamer bridge control system and has wire to connect liquid propellant feed system 4, described liquid propellant 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 hybrid propellant rocket protective equipment peculiar to vessel with safeguard function, comprise ejector filler 1, firing chamber 2, control system 3, liquid propellant supply system 4, jet pipe 5, tank 6, it is characterized in that: described ejector filler 1 connects firing chamber 2 and tank 6, charge pole in described firing chamber 2, solid fuel is seated in firing chamber 2, described control system 3 connects steamer bridge control system and has wire to connect liquid propellant feed system 4, described liquid propellant supply system 4 connects tank 6, described liquid propellant 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 hybrid propellant rocket protective equipment peculiar to vessel with safeguard function, comprise ejector filler 1, firing chamber 2, control system 3, liquid propellant 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, charge pole in described firing chamber 2, solid fuel is seated in firing chamber 2, described control system 3 connects steamer bridge control system and has wire to connect liquid propellant feed system 4, described liquid propellant 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 hybrid propellant rocket protective equipment peculiar to vessel of safeguard function, comprise ejector filler (1), firing chamber (2), control system (3), liquid propellant 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) interior charge pole, solid fuel is seated in firing chamber (2), described control system (3) connects steamer bridge control system and has wire to connect liquid propellant feed system (4), described liquid propellant 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 hybrid propellant rocket protective equipment peculiar to vessel of safeguard function according to claim 1, it is characterized in that: described jet pipe (5) has 4.
3. there is the hybrid propellant rocket protective equipment peculiar to vessel of safeguard function according to claim 1, it is characterized in that: parachute (7) is also installed and has wire connection control system (3).
4. there is the hybrid propellant rocket protective equipment peculiar to vessel of safeguard function according to claim 1, it is characterized in that: described liquid propellant supply system (4) comprises pressurized gas cylinder and decompressor starts valve.
5. there is the hybrid propellant rocket protective equipment peculiar to vessel of safeguard function according to claim 1, it is characterized in that: described in there is the hybrid propellant rocket protective equipment peculiar to vessel of safeguard function for speedboat.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410574717.7A CN104373249B (en) | 2014-10-25 | 2014-10-25 | A kind of hybrid propellant rocket protective equipment peculiar to vessel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410574717.7A CN104373249B (en) | 2014-10-25 | 2014-10-25 | A kind of hybrid propellant rocket protective equipment peculiar to vessel |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104373249A true CN104373249A (en) | 2015-02-25 |
| CN104373249B CN104373249B (en) | 2016-03-30 |
Family
ID=52552372
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410574717.7A Active CN104373249B (en) | 2014-10-25 | 2014-10-25 | A kind of hybrid propellant rocket protective equipment peculiar to vessel |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104373249B (en) |
Citations (5)
| 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 |
| DE4429860A1 (en) * | 1994-08-23 | 1995-03-02 | Thomas Dr Stinnesbeck | Injection system for hybrid rocket engines |
| CN2424074Y (en) * | 1999-11-05 | 2001-03-21 | 邱刚 | Hover marine with side puff port on its hull |
| US6394015B1 (en) * | 2000-12-08 | 2002-05-28 | Edwin Zenith Gabriel | Boat collision avoidance system using blasts of water |
| CN2548902Y (en) * | 2002-06-11 | 2003-05-07 | 张弘迅 | Hovercraft boat |
-
2014
- 2014-10-25 CN CN201410574717.7A patent/CN104373249B/en active Active
Patent Citations (5)
| 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 |
| DE4429860A1 (en) * | 1994-08-23 | 1995-03-02 | Thomas Dr Stinnesbeck | Injection system for hybrid rocket engines |
| CN2424074Y (en) * | 1999-11-05 | 2001-03-21 | 邱刚 | Hover marine with side puff port on its hull |
| US6394015B1 (en) * | 2000-12-08 | 2002-05-28 | Edwin Zenith Gabriel | Boat collision avoidance system using blasts of water |
| CN2548902Y (en) * | 2002-06-11 | 2003-05-07 | 张弘迅 | Hovercraft boat |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104373249B (en) | 2016-03-30 |
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Legal Events
| Date | Code | Title | Description |
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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: Chen Jianhong Inventor after: Deng Ruiping Inventor before: Luo Hua Inventor before: Luo Shizhuo Inventor before: Deng Ruiping |
|
| COR | Change of bibliographic data | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20160218 Address after: 542600 the Guangxi Zhuang Autonomous Region, Zijin Mountain, Zijin Mountain, town, Xing Zhong Road, No. 22 Applicant after: Chen Jianhong 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: Ni Weiyong Address before: 542600 No. 22 Xingzhong South Road, Zhongshan Town, Zhongshan County, Hezhou City, Guangxi Zhuang Autonomous Region Patentee before: Chen Jianhong |
|
| TR01 | Transfer of patent right | ||
| CP02 | Change in the address of a patent holder |
Address after: 38 Gangcheng Road, Gangcheng street, Gaogang District, Taizhou City, Jiangsu Province Patentee after: Ni Weiyong Address before: 225321 No. 11 Xuzhuang Xingwang Road, Gaogang District, Taizhou City, Jiangsu Province Patentee before: Ni Weiyong |
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| CP02 | Change in the address of a patent holder | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20221230 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: No.38 Gangcheng Road, Gangkou street, Gaogang District, Taizhou City, Jiangsu Province Patentee before: Ni Weiyong |
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| TR01 | Transfer of patent right |