CN103234400A - Lateral cabin opening parachute structure used for anti-hail precipitation-enhancement rocket bomb - Google Patents
Lateral cabin opening parachute structure used for anti-hail precipitation-enhancement rocket bomb Download PDFInfo
- Publication number
- CN103234400A CN103234400A CN2012105182168A CN201210518216A CN103234400A CN 103234400 A CN103234400 A CN 103234400A CN 2012105182168 A CN2012105182168 A CN 2012105182168A CN 201210518216 A CN201210518216 A CN 201210518216A CN 103234400 A CN103234400 A CN 103234400A
- Authority
- CN
- China
- Prior art keywords
- parachute
- umbrella
- canopy
- cabin
- connector
- 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
Images
Abstract
The invention belongs to the technical field of weather modification and particularly relates to a lateral cabin opening parachute structure used for an anti-hail precipitation-enhancement rocket bomb. The lateral cabin opening parachute structure comprises a wind cap, a parachute, a sunk screw, a parachute cabin, a parachute cover, a parachute top rope, a screw, a nut, a steel wire rope connecting piece, an O-shaped seal ring, a semi-round head screw, a push plate, a chemical box body and a thread connecting piece. The technology of opening the parachute by laterally opening the cabin of the rocket bomb in the air has the advantages that the structure is simple, the rocket bomb debris falls on the ground at a lower speed by one parachute, the reliability in the parachute opening process of the rocket bomb is improved, the cost is reduced, and the defects of low reliability and high possibility of personal injury in a secondary parachute system are satisfactorily solved.
Description
Technical field:
The invention belongs to the artificial affecting weather technology field, be specifically related to a kind of hail-proof rain-increasing rocket, particularly a kind of side direction for hail-proof rain-increasing rocket parachuting structure of opening the cabin.
Background technology:
Rocket hail-proof rain-increasing operating system of the prior art is divided into explosion type, burns and sow formula and flame bullet formula by the mode of sowing; Be divided into type self-destroyed, the parachute-type of blast and burning case type by the remains processing mode.
At present shadow rocket ammunition adopts and axially opens the cabin after catalyst action is finished, dish out main parachute and associated parachute, with the rocket projectile remains with less speed safe falling to ground; And two parachutes of the main parachute of this employing and associated parachute two-stage parachute landing system, dish out, winding appears in two-stage parachute easily in parachute-opening and the landing process, causes parachute malfunctioning, whole bullet is dropped and the event that causes hurting sb.'s feelings takes place.
Summary of the invention: purpose of the present invention is exactly in order to solve the deficiencies in the prior art, and proposes a kind of side direction for hail-proof rain-increasing rocket parachuting structure of opening the cabin.
Technical scheme of the present invention is: a kind of side direction for hail-proof rain-increasing rocket parachuting structure of opening the cabin, formed by blast cap, parachute, sunk screw, umbrella cabin, canopy, umbrella top rope, screw, nut, steel wire rope connector, zero RunddichtringO, snap rivet, push pedal, drug cassette body, threaded connector etc.The umbrella cabin is threaded with the rocket projectile housing, be connected by sunk screw with blast cap, canopy is 120 ° of circular arcs, one end of canopy is the step structure on edge in having, the other end of canopy is processed into the inclined-plane and cooperates with the inclined-plane in umbrella cabin, promote canopy until putting in place after an end on edge inserted the umbrella cabin in canopy had, canopy is fixedlyed connected by snap rivet with the umbrella cabin again, the outer surface that makes canopy and umbrella cabin is one flat, the interior edge of canopy forms 120 ° of arc boss at inner surface, and the end face of push pedal contacts cooperation with this boss; One end of umbrella top rope is fixedlyed connected with canopy by screw, nut, the other end connects parachute umbrella top, the steel wire rope connector comprises steel loop, steel wire rope, umbrella connector, steel loop is connected with parachute umbrella rope, the umbrella connector is connected by bolt with body, and push pedal and umbrella connector are by the sealing of zero RunddichtringO.
Beneficial effect of the present invention: rocket projectile aloft side opens the cabin and throws the umbrella technology, simple in structure, adopt a umbrella that the rocket projectile remains are drop to ground with less speed, improved the reliability in the rocket projectile parachute-opening process, and having reduced cost, the present invention has solved the low problem of reliability that secondary parachuting brings well.
Description of drawings: the present invention has 5 width of cloth accompanying drawings, and wherein Fig. 1 is most preferred embodiment of the present invention, also can explain the accompanying drawing of book extract.
Fig. 1, be the side of the present invention parachuting structural representation that opens the cabin;
Fig. 2, for the cross-sectional structure schematic diagram in umbrella of the present invention cabin;
Fig. 3, for the structural representation of canopy of the present invention;
Fig. 4, for the cross-sectional structure schematic diagram of canopy of the present invention;
Fig. 5, for the structural representation of steel wire rope connector of the present invention.
The specific embodiment: most preferred embodiment of the present invention is further described below in conjunction with accompanying drawing.
As shown in Figure 1 and Figure 2, a kind of side direction for hail-proof rain-increasing rocket parachuting structure of opening the cabin is made up of blast cap 1, parachute 2, sunk screw 3, umbrella cabin 4, canopy 5, umbrella top rope 6, screw 7, nut 8, steel wire rope connector 9, zero RunddichtringO 10, button-headed screw 11, push pedal 12, drug cassette body 13, threaded connector 14 etc.Umbrella cabin 4 is threaded with the rocket projectile housing, be connected by sunk screw 3 with blast cap, as Fig. 3, shown in Figure 4, canopy 5 is 120 ° of circular arcs, one end of canopy is along 20 step structure in having, the other end of canopy is processed into inclined-plane 18 and cooperates with the inclined-plane in umbrella cabin, promote canopy 5 until putting in place after an end on edge inserted the umbrella cabin in canopy had, canopy 5 is fixedlyed connected by snap rivet 11 with umbrella cabin 4 again, the outer surface that makes canopy and umbrella cabin is one flat, the interior of canopy forms 120 ° of arc boss along 20 at inner surface, and the end face of push pedal 12 contacts cooperation with this boss; One end 6 of umbrella top rope is fixedlyed connected with canopy by screw 7, nut 8, the other end connects parachute 2 umbrellas top, as shown in Figure 5, steel wire rope connector 9 comprises steel loop 15, steel wire rope 16, umbrella connector 17, steel loop 15 is connected with parachute umbrella rope, umbrella connector 17 is connected by bolt with body, and push pedal 12 seals by zero RunddichtringO 10 with umbrella connector 17.After the rocket projectile emission, when rocket projectile flies to predetermined altitude, the agent of AgI flame is lighted in the delay igniter effect, AgI flame agent burning is shed in the cloud by 4 oblique spray orifices, after flame agent burning is finished, parachute-opening medicine in the ignition powder box body 13 under parachute-opening impetus axial action, promotes push pedal 11, push pedal 11 promotes the interior along 20 of canopy 5, canopy 5 is moved forward with respect to umbrella cabin 4, form shearing force, shear snap rivet 11, impelling goes out canopy 5, canopy 5 is taken parachute 2 out of by umbrella top rope 6 side direction that connect, and parachute 2 is opened the back by steel wire rope connector 9 towing rocket bullet remains, and the rocket projectile remains are drop to ground with less speed.
Claims (1)
1. a side direction that is used for hail-proof rain-increasing rocket parachuting structure of opening the cabin is made up of blast cap (1), parachute (2), sunk screw (3), umbrella cabin (4), canopy (5), umbrella top rope (6), screw (7), nut (8), steel wire rope connector (9), zero RunddichtringO (10), button-headed screw (11), push pedal (12), drug cassette body (13), threaded connector (14) etc.It is characterized in that: umbrella cabin (4) are threaded with the rocket projectile housing, be connected by sunk screw (3) with blast cap (1), canopy (5) is 120 ° of circular arcs, one end of canopy is for having the step structure of interior edge (20), the other end of canopy is processed into inclined-plane (18) and cooperates with the inclined-plane in umbrella cabin, after inserting the umbrella cabin, the end that canopy is had an interior edge (20) promotes canopy (5) until putting in place, canopy (5) is fixedlyed connected by snap rivet (11) with umbrella cabin (4) again, the outer surface that makes canopy and umbrella cabin is one flat, the interior edge (20) of canopy forms 120 ° of arc boss at inner surface, and 120 ° of arc boss of the end face of push pedal (12) and this contact cooperation; One end (6) of umbrella top rope is fixedlyed connected with canopy by screw (7), nut (8), the other end connects the umbrella top of parachute (2), steel wire rope connector (9) comprises steel loop (15), steel wire rope (16), umbrella connector (17), steel loop (15) is connected with parachute umbrella rope, umbrella connector (17) is connected by bolt with body, and push pedal and umbrella connector are by the sealing of zero RunddichtringO.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012105182168A CN103234400A (en) | 2012-12-06 | 2012-12-06 | Lateral cabin opening parachute structure used for anti-hail precipitation-enhancement rocket bomb |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012105182168A CN103234400A (en) | 2012-12-06 | 2012-12-06 | Lateral cabin opening parachute structure used for anti-hail precipitation-enhancement rocket bomb |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103234400A true CN103234400A (en) | 2013-08-07 |
Family
ID=48882452
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012105182168A Pending CN103234400A (en) | 2012-12-06 | 2012-12-06 | Lateral cabin opening parachute structure used for anti-hail precipitation-enhancement rocket bomb |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103234400A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106839900A (en) * | 2017-03-28 | 2017-06-13 | 北京厚力德仪器设备有限公司 | A kind of hail-proof rain-increasing rocket based on warm cloud catalyst |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB181037A (en) * | 1920-12-08 | 1922-06-08 | M L Ex Ltd | Improvements in or relating to shells |
| SE347347B (en) * | 1967-07-30 | 1972-07-31 | Israel State | |
| CN101407252A (en) * | 2008-10-30 | 2009-04-15 | 航宇救生装备有限公司 | Parachute assembly suitable for rocket |
| CN102168937A (en) * | 2011-01-28 | 2011-08-31 | 晋西工业集团有限责任公司 | Hail-suppression and rainfall-increment rocket bomb |
| CN201993047U (en) * | 2011-01-28 | 2011-09-28 | 晋西工业集团有限责任公司 | Civil anti-hail and rainfall-enhancement rocket recovery device |
-
2012
- 2012-12-06 CN CN2012105182168A patent/CN103234400A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB181037A (en) * | 1920-12-08 | 1922-06-08 | M L Ex Ltd | Improvements in or relating to shells |
| SE347347B (en) * | 1967-07-30 | 1972-07-31 | Israel State | |
| CN101407252A (en) * | 2008-10-30 | 2009-04-15 | 航宇救生装备有限公司 | Parachute assembly suitable for rocket |
| CN102168937A (en) * | 2011-01-28 | 2011-08-31 | 晋西工业集团有限责任公司 | Hail-suppression and rainfall-increment rocket bomb |
| CN201993047U (en) * | 2011-01-28 | 2011-09-28 | 晋西工业集团有限责任公司 | Civil anti-hail and rainfall-enhancement rocket recovery device |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106839900A (en) * | 2017-03-28 | 2017-06-13 | 北京厚力德仪器设备有限公司 | A kind of hail-proof rain-increasing rocket based on warm cloud catalyst |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN201488656U (en) | Locking and separating device | |
| CN102168937B (en) | Hail-suppression and rainfall-increment rocket bomb | |
| CN106839900B (en) | A kind of hail-proof rain-increasing rocket based on warm cloud catalyst | |
| CN203323620U (en) | Rain-increasing hail-suppressing rocket projectile recycling device | |
| CN101843962B (en) | Whole-pneumatic air burst fire extinguishing bomb | |
| CN102878870A (en) | Extinguishment shrapnel type rocket bomb | |
| CN109579638A (en) | A kind of high security a ten thousandth misfire rate artificial rain bomb | |
| CN109250154A (en) | A kind of secondary parachute-opening safety landing system in side | |
| CN103452704A (en) | Miniature turbojet midair windmill ignition device | |
| CN102514714B (en) | Reduce the apparatus and method of rotor unmanned helicopter harm out of control | |
| CN103234400A (en) | Lateral cabin opening parachute structure used for anti-hail precipitation-enhancement rocket bomb | |
| CN203740130U (en) | Unmanned aerial vehicle recycling landing system | |
| CN207886550U (en) | A kind of fire extinguisher bomb power and stabilising arrangement | |
| CN205561674U (en) | Rocket dummy round of laying mines | |
| CN2784872Y (en) | Two-way fire-transferring fuse of precipitation stimulation bomb | |
| CN201569371U (en) | Rocket bomb used for forest fire extinction | |
| CN206950502U (en) | A kind of fire extinguisher bomb, transmitter and extinguishing device | |
| CN203489792U (en) | Rain-increasing/hail-suppressing rocket-powered missile accurate in timing and reliable in running | |
| CN201993047U (en) | Civil anti-hail and rainfall-enhancement rocket recovery device | |
| CN201799035U (en) | Fire extinguishing bomb used for supported launcher | |
| CN201993048U (en) | Hail-suppression and rain-enhancement rocket projectile | |
| CN202974074U (en) | Fire extinguishing cluster rocket bomb | |
| CN207274995U (en) | A kind of aircraft sliding block separating mechanism | |
| CN203203480U (en) | Shear type opening connecting screw structure of cluster bomb bullet | |
| CN204193362U (en) | Individual soldier's portable balance emission-type skyscraper fire extinguisher bomb |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C05 | Deemed withdrawal (patent law before 1993) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20130807 |