CN105758260B - Payingoff mechanism in optical-fibre guidance torpedo and the Guided Torpedo constituted - Google Patents
Payingoff mechanism in optical-fibre guidance torpedo and the Guided Torpedo constituted Download PDFInfo
- Publication number
- CN105758260B CN105758260B CN201610201309.6A CN201610201309A CN105758260B CN 105758260 B CN105758260 B CN 105758260B CN 201610201309 A CN201610201309 A CN 201610201309A CN 105758260 B CN105758260 B CN 105758260B
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- CN
- China
- Prior art keywords
- optical cable
- torpedo
- coil
- payingoff mechanism
- unwrapping wire
- 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.)
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- 230000007246 mechanism Effects 0.000 title claims abstract description 43
- 239000013307 optical fiber Substances 0.000 title claims abstract description 13
- 230000003287 optical effect Effects 0.000 claims abstract description 99
- 239000007767 bonding agent Substances 0.000 claims abstract description 17
- 241000251468 Actinopterygii Species 0.000 claims description 4
- 238000009434 installation Methods 0.000 claims description 3
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims 1
- 238000004804 winding Methods 0.000 description 15
- 239000000835 fiber Substances 0.000 description 8
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical group O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 4
- 230000037237 body shape Effects 0.000 description 4
- 239000000741 silica gel Substances 0.000 description 4
- 229910002027 silica gel Inorganic materials 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 230000033001 locomotion Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000003068 static effect Effects 0.000 description 2
- 238000010923 batch production Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 210000004899 c-terminal region Anatomy 0.000 description 1
- 230000003467 diminishing effect Effects 0.000 description 1
- 239000000686 essence Substances 0.000 description 1
- 238000007667 floating Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G3/00—Aiming or laying means
- F41G3/22—Aiming or laying means for vehicle-borne armament, e.g. on aircraft
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B19/00—Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means
- F42B19/46—Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means adapted to be launched from aircraft
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B19/00—Marine torpedoes, e.g. launched by surface vessels or submarines; Sea mines having self-propulsion means
- F42B19/01—Steering control
- F42B19/10—Steering control remotely controlled, e.g. by sonic or radio control
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Light Guides In General And Applications Therefor (AREA)
Abstract
The invention discloses the payingoff mechanism in a kind of optical-fibre guidance torpedo and the Guided Torpedo constituted, payingoff mechanism includes two baffle plates being parallel to each other, two baffle plates are arranged side by side and form coil space between two baffle plates, coil is installed, coil both ends of the surface are formed with two baffle plates by the corresponding bonding of bonding agent respectively in coil space；If the coil is bonded and formed successively by dried layer optical cable ring element by bonding agent with overlapped way, the optical cable ring element is coiled into the not closed annular with two ends by optical cable, and the optical cable unwrapping wire end of the coil is located at outside payingoff mechanism；Guided Torpedo includes torpedo body and payingoff mechanism, and torpedo body has flight controller and torpedo afterbody.The present invention can solve the problems, such as side outlet, and the confined space inside body is can be suitably used for again and is used.
Description
Technical field
The present invention relates to the payingoff mechanism in optical-fibre guidance torpedo technique field, more particularly to a kind of optical-fibre guidance torpedo and
The Guided Torpedo constituted.
Background technology
Optical-fibre guidance torpedo be it is a kind of the technology that torpedo strikes target is controlled using optical fiber is pulled, it has target identification
The characteristics of ability is strong, guidance precision is high, anti-interference is good.Common Guided Torpedo structure is as shown in figure 1, its payingoff mechanism is usual
Structure is as follows：There is flight controller A102, the torpedo body in flight controller A102 peripheries inside torpedo body A101
There is cavity in A101 inside, fibre tube is provided with outside the cavity, the directly winding optical cable A103 outside fibre tube.Its unwrapping wire
Mechanism principle is described as follows：Optical cable A103 is wound on above fibre tube, when torpedo advances, by the drag force of floating drum by optical cable
A103 is pulled out above fibre tube, and its movement locus is around fibre tube rotation when optical cable A103 is pulled out.Because torpedo afterbody has
Propeller, and need flame to produce thrust, if so the payingoff mechanism in traditional torpedo is put from torpedo body A101 afterbodys
Line is drawn easily by flame burn.If drawn from torpedo body A101 sidepieces unwrapping wire, then its ring when optical cable A103 is pulled out
When being rotated around fibre tube, optical cable A103 is easy for being hindered by fibre tube, torpedo body A101 housings or/and flight controller A102
Hinder, especially when optical cable A103 will be finished by unwrapping wire, be wrapped in the optical cable A103 on fibre tube apart from torpedo body A101
Unwrapping wire oral area just has certain distance, and the optical cable A103 that now unwrapping wire comes out just has certain distance, the optical cable of outlet in the cavities
A103 will be disturbed by torpedo body A101, the flight controller A102 of cavity both sides.Because optical cable A103 is from torpedo body
A101 sidepiece outlets, then optical cable A103 just just has a pull-out angle at torpedo body A101 sidepieces, now flight controller
A102 will influence, limit its pull-out angle so that optical cable A103 outlets are difficult.So traditional sidepiece outlet unwrapping wire torpedo can be limited
Optical cable A103 pull-out angle, causes unwrapping wire difficult.Another unwrapping wire mode in torpedo is that optical cable is coiled into a ball of string,
When inside torpedo without enough spaces, this mode can not be implemented.
The content of the invention
Being applied to the outlet of torpedo afterbody or side outlet for the Guided Torpedo drawoff structure that prior art is present needs
The problems such as outlet of larger installing space and payingoff mechanism is difficult, it is an object of the invention to provide a kind of optical-fibre guidance fish
Payingoff mechanism in thunder and the Guided Torpedo constituted, can both solve the problems, such as side outlet, can be suitably used for again limited inside body
Space is used.
The purpose of the present invention is achieved through the following technical solutions：
A kind of payingoff mechanism in optical-fibre guidance torpedo, payingoff mechanism includes two baffle plates being parallel to each other, two baffle plates
Be arranged side by side and formed between two baffle plates and coil is installed in coil space, coil space, coil both ends of the surface respectively with two
Baffle plate is formed by bonding agent correspondence bonding, and currently preferred bonding agent is silica gel；If the coil is by dried layer optical cable ring list
Member is bonded successively by bonding agent with overlapped way to be formed, and the optical cable ring element is coiled into the patent with two ends by optical cable
Annular is closed, the optical cable unwrapping wire end of the coil is located at outside payingoff mechanism.
In order to be better achieved the present invention, the optical cable ring element is coiled into some circles overlapping cable loops successively by optical cable,
The optical cable that each cable loops are coiled between the not closed annular with two ends, adjacent cable loops is bonded by bonding agent
Form, currently preferred bonding agent is silica gel, the center of arc of all cable loops overlaps.
Preferably, the coil matches with coil space shape.
A kind of Guided Torpedo being made up of payingoff mechanism, including torpedo body and payingoff mechanism, torpedo body, which has, to fly
Line control unit and torpedo afterbody, the flight controller are located inside torpedo body, in the torpedo positioned at flight controller periphery
There is the unwrapping wire cavity that cross section is toroidal, torpedo body sidepiece is provided with the unwrapping wire being connected with unwrapping wire cavity inside body
Mouthful, the payingoff mechanism Matching installation is in the unwrapping wire cavity；The optical cable of the payingoff mechanism coil is an optical cable, optical cable
With unwrapping wire end and connection end Liang Ge ends, the unwrapping wire end of optical cable is stretched out from payingoff mechanism, unwrapping wire mouthful and positioned at torpedo body side
Portion, the connection end of optical cable inside flight controller with electrically connecting.
The present invention compared with the prior art, with advantages below and beneficial effect：
The present invention is applied to the side outlet of Guided Torpedo, and can be applied to the fish inside body for the confined space
Thunder；Guided Torpedo passes through unwrapping wire mouthful unwrapping wire and draws, it is to avoid what the unwrapping wire outlet in emission process diminishing and bringing because being moved away from angle
Unwrapping wire is difficult；When coil in torpedo body is drawn out its optical cable will from coil last layer layer ground orderly withdrawal, coil
It is to be carried out along torpedo body circumference to move back line movement locus, and coil is static relative to torpedo body, can prevent in high speed unwinding
The optical cable damage brought because coil is rotated；Meanwhile, coil is static relative to torpedo body, can avoid making for rotary connector
With raising transmission performance；In structure of the present invention rationally, technique is simple, possesses the ability of batch production.
Brief description of the drawings
Fig. 1 is the payingoff mechanism structural representation of traditional torpedo body；
Fig. 2 is the structural representation of torpedo body of the present invention；
Fig. 3 is the structural representation of payingoff mechanism of the present invention；
Fig. 4 is the structural representation of Fig. 3 coils；
Fig. 5 is optical cable coiling schematic diagram；
Fig. 6 is the optical cable winding mould structural representation of ancillary cable coiling；
Fig. 7 is the unwrapping wire schematic diagram after a circle cable loops coiling；
Fig. 8 is the unwrapping wire schematic diagram after two circle cable loops coilings.
Wherein, it is entitled corresponding to the reference in accompanying drawing：
101- torpedo body A, 102- flight controller A, 103- optical cable A, 1- torpedo bodies, 11- flight controls
Annular distance in device, 12- torpedo afterbodys, 2- payingoff mechanisms, 3- optical cables, 4- coils, 41- coils, 42- hub of a spools hole, 5-
Baffle plate, 6- optical cable winding moulds.
Embodiment
The present invention is described in further detail with reference to embodiment：
Embodiment
As shown in Fig. 3~Fig. 8, a kind of payingoff mechanism in optical-fibre guidance torpedo, payingoff mechanism 2 is parallel to each other including two
Baffle plate 5, two baffle plates 5, which are arranged side by side and formed between two baffle plates 5, is provided with coil 4, line in coil space, coil space
The both ends of the surface of circle 4 are formed with two baffle plates 5 by the corresponding bonding of bonding agent respectively, as shown in figure 3, the left and right of coil 4 two is held
Face is corresponding with the baffle plate 5 of left and right two respectively to be bonded, and two baffle plates 5 are bonding and the both ends of the surface of coil 4 after the coiling of coil 4 is finished
The effect of gripping is played, to prevent the optical cable 3 of the end face of coil 4 from being come off from coil 4.If coil 4 is by dried layer optical cable ring element
It is bonded and is formed successively with overlapped way by bonding agent, currently preferred bonding agent is silica gel, and one layer of optical cable ring element is by light
Cable 3 is coiled into the not closed annular with two ends, and the unwrapping wire end of optical cable 3 of coil 4 is located at outside payingoff mechanism 2, and coil 4 is just
If being bonded into cylinder body shape by dried layer optical cable ring element.
As shown in figure 4, the optical cable ring element of the present embodiment is coiled into some circles overlapping cable loops, such as Fig. 5 successively by optical cable 3
Shown, the optical cable 3 that each cable loops are coiled between the not closed annular with two ends, adjacent cable loops passes through bonding
Agent bonding is formed, and currently preferred bonding agent is silica gel, and the center of arc of all cable loops overlaps.
The preferred coil 4 of the present embodiment matches with coil space shape.
As shown in Fig. 2 a kind of Guided Torpedo being made up of payingoff mechanism, including torpedo body 1 and payingoff mechanism 2, fish
Thunder body 1 has flight controller 11 and torpedo afterbody 12, and flight controller 11 is located inside torpedo body 1, positioned at flight
The inside of torpedo body 1 of the periphery of controller 11 has the unwrapping wire cavity that cross section is toroidal, and unwrapping wire cavity is empty with coil 4
Between shape, size match, the length of unwrapping wire cavity is highly equal with coil 4, and the section of unwrapping wire cavity is not closed circle
Shape, the section of coil 4 is integrally in not closed round-shaped.The sidepiece of torpedo body 1 is provided with and putting that unwrapping wire cavity is connected
Line mouthful, the length of unwrapping wire mouthful and unwrapping wire cavity matches, and the Matching installation of payingoff mechanism 2 is in the unwrapping wire cavity.As shown in figure 4,
The coil 4 of payingoff mechanism 2 is cylinder body shape, and its center of coil 4 is hub of a spool hole 42, coordinates to be installed in payingoff mechanism 2 and puts
After in line cavity, flight controller 11 is just matched in the hub of a spool hole 42 of coil 4.The light of the coil 4 of payingoff mechanism 2
Cable 3 is optical cable, and optical cable 3 has unwrapping wire end and a connection end Liang Ge ends, and the unwrapping wire end of optical cable 3 is from payingoff mechanism 2, unwrapping wire mouthful
Stretch out and be located at the sidepiece of torpedo body 1, the connection end of optical cable 3 is electrically connected with the inside of flight controller 11.As shown in fig. 6, this hair
Bright to provide optical cable winding mould 6 required during a kind of optical cable coiling, the section of optical cable winding mould 6 is in circular arc as shown in Figure 6
Wire shaped, the i.e. section of optical cable winding mould 6 are not closed round-shaped.Optical cable 3 is just around the cylindrical of optical cable winding mould 6
Then surface, internal circular surfaces coiling successively, optical cable 3 pass through bonding agent first in the outward flange of optical cable winding mould 6 around a circle cable loops
Bonding is overlapping again just to constitute an optical cable ring element around some circle cable loops, and the optical cable ring element just has certain thickness, so
If afterwards further along the length direction of optical cable winding mould 6 successively around dried layer optical cable ring element, material is thus formed cylinder as shown in Figure 4
The coil 4 of shape.Can also coiling in the following way using such as Fig. 6 optical cable winding mould 6：First by optical cable 3 along optical cable
The length direction of winding mould 6 is coiled into one layer of optical cable layer successively, then the coiling second layer optical cable 2 on bottom optical cable layer again, successively
If coiling can coiling dried layer optical cable, be then formed the coil 4 of cylinder body shape as shown in Figure 4.Above two passes through optical cable
The winding mode of winding mould 6, after coiling constitutes coil 4, optical cable winding mould 6 is removed from coil 4, then coil 4 is just
The coil of cylinder body shape as shown in Figure 4 is formd, the center of coil 4 has hub of a spool hole 42, and the edge of coil 4 is formed with coil
Annular distance 41 is exactly that optical cable winding mould 6 is removed annular distance 41 in the hole formed afterwards, coil and is conducive to light in interior annular distance 41, coil
The more quickly unwrapping wire in unwrapping wire of cable 3.
The operation principle of the present invention is as follows：
As shown in Fig. 2 pulling optical cable 3 to be passed successively from payingoff mechanism 2, unwrapping wire mouth and unwrapping wire motion after torpedo-launching
When, because coil 4 is formed by optical cable 3 by bonding agent bonding, then coil 4 is enclosed to be drawn out by one and released by pulling force effect
Put, come off lower optical cable 3, to enable optical cable 3 quickly to be pulled out from unwrapping wire mouthful, unwrapping wire mouthful be it is equal with unwrapping wire cavity length and
The opening matched, point of application when being drawn out optical cable 3 due to coil 4 is always unwrapping wire mouthful and the point of application keeps constant.Such as Fig. 7
It is shown, constituted if coil 4 is one layer of cable loops, this layer of cable loops are by optical cable around integral in not closed toroidal, vacation
Such as the unwrapping wire end that A ends are optical cable 3, B ends are the connection end of optical cable 3, B ends connection flight controller 11, by pulling A ends, annulus
The optical cable 3 of property will come off and be fast released successively according to the direction of arrow as shown in Figure 7.If as shown in figure 8, coil 4
Constituted for two layers of cable loops, then the cable loops of bottom are by optical cable around integral in not closed toroidal, the optical cable on upper strata
Enclosing to be overlapped in above the cable loops of bottom, and C-terminal is the connection end of optical cable 3, D ends connection flight controller 11, by pulling C
End, the optical cable 3 of annulus will come off and be fast released successively according to the direction of arrow as shown in Figure 8.When coil 4 is drawn out
Its optical cable 3 will be from the last layer of coil 4 layer ground orderly withdrawal, and because unwrapping wire mouthful length is equal with unwrapping wire cavity length, coil 4 is drawn
Going out rear remaining optic cable also can be located at unwrapping wire mouthful nearby, can allow optical cable 3 is prompt quickly, uniformly, in an orderly manner move back from coil 4
Go out, finished until coil 4 is rejected.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention
Any modifications, equivalent substitutions and improvements made within refreshing and principle etc., should be included in the scope of the protection.
Claims (4)
1. the payingoff mechanism in a kind of optical-fibre guidance torpedo, it is characterised in that：Payingoff mechanism (2) includes two gears being parallel to each other
Plate (5), two baffle plates (5), which are arranged side by side and formed between two baffle plates (5) in coil space, coil space, is provided with coil
(4), coil (4) both ends of the surface are formed with two baffle plates (5) by the corresponding bonding of bonding agent respectively；The coil (4) is if by dried layer
Optical cable ring element is bonded successively by bonding agent with overlapped way to be formed, and the optical cable ring element is coiled into two by optical cable (3)
The not closed annular of individual end, optical cable (3) unwrapping wire end of the coil (4) is located at payingoff mechanism (2) outside.
2. according to the payingoff mechanism in the optical-fibre guidance torpedo described in claim 1, it is characterised in that：The optical cable ring element by
Optical cable (3) is coiled into some circles overlapping cable loops successively, and each cable loops are coiled into the not closed annular with two ends,
Optical cable (3) between adjacent cable loops is formed by bonding agent bonding, and the center of arc of all cable loops overlaps.
3. according to the payingoff mechanism in the optical-fibre guidance torpedo described in claim 1, it is characterised in that：The coil (4) and line
Cycle space shape matches.
4. a kind of Guided Torpedo being made up of any described payingoff mechanism of claims 1 to 3, it is characterised in that：Including fish
Thunder body (1) and payingoff mechanism (2), torpedo body (1) have flight controller (11) and torpedo afterbody (12), the flight control
Device (11) processed is located at torpedo body (1) inside, has inside the torpedo body (1) positioned at flight controller (11) periphery transversal
Face is the unwrapping wire cavity of toroidal, and torpedo body (1) sidepiece is provided with the unwrapping wire mouthful being connected with unwrapping wire cavity, the paying out machine
Structure (2) Matching installation is in the unwrapping wire cavity；The optical cable (3) of payingoff mechanism (2) coil (4) is an optical cable, optical cable
(3) there is unwrapping wire end and connection end Liang Ge ends, the unwrapping wire end of optical cable (3) is stretched out and is located at from payingoff mechanism (2) and unwrapping wire mouthful
Torpedo body (1) sidepiece, the connection end of optical cable (3) inside flight controller (11) with electrically connecting.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610201309.6A CN105758260B (en) | 2016-04-01 | 2016-04-01 | Payingoff mechanism in optical-fibre guidance torpedo and the Guided Torpedo constituted |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610201309.6A CN105758260B (en) | 2016-04-01 | 2016-04-01 | Payingoff mechanism in optical-fibre guidance torpedo and the Guided Torpedo constituted |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105758260A CN105758260A (en) | 2016-07-13 |
| CN105758260B true CN105758260B (en) | 2017-10-13 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610201309.6A Active CN105758260B (en) | 2016-04-01 | 2016-04-01 | Payingoff mechanism in optical-fibre guidance torpedo and the Guided Torpedo constituted |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105758260B (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2654204B1 (en) * | 1989-11-09 | 1994-06-03 | France Etat Armement | DEVICE FOR UNWINDING A FILOTRANSMISSION CABLE OF A MACHINE MOVING AT HIGH SPEED IN A FLUID. |
| CN2540643Y (en) * | 2002-03-29 | 2003-03-19 | 信息产业部电子第八研究所 | Guidance optical cable |
| CN204462473U (en) * | 2015-01-28 | 2015-07-08 | 长飞光纤光缆股份有限公司 | A kind of micro-cable stays box from draw drum |
| CN205482593U (en) * | 2016-04-01 | 2016-08-17 | 四川永贵科技有限公司 | Paying out machine structure in optic fibre guidance torpedo and guidance torpedo that constitutes |
-
2016
- 2016-04-01 CN CN201610201309.6A patent/CN105758260B/en active Active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2654204B1 (en) * | 1989-11-09 | 1994-06-03 | France Etat Armement | DEVICE FOR UNWINDING A FILOTRANSMISSION CABLE OF A MACHINE MOVING AT HIGH SPEED IN A FLUID. |
| CN2540643Y (en) * | 2002-03-29 | 2003-03-19 | 信息产业部电子第八研究所 | Guidance optical cable |
| CN204462473U (en) * | 2015-01-28 | 2015-07-08 | 长飞光纤光缆股份有限公司 | A kind of micro-cable stays box from draw drum |
| CN205482593U (en) * | 2016-04-01 | 2016-08-17 | 四川永贵科技有限公司 | Paying out machine structure in optic fibre guidance torpedo and guidance torpedo that constitutes |
Non-Patent Citations (1)
| Title |
|---|
| 鱼雷光纤线导光传输技术研究;刘雪辰等;《鱼雷技术》;20130215;第21卷(第1期);第34-38页 * |
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| CN105758260A (en) | 2016-07-13 |
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