CN106240835A - Check cable idle Automatic-reset carrier landing stopping device - Google Patents
Check cable idle Automatic-reset carrier landing stopping device Download PDFInfo
- Publication number
- CN106240835A CN106240835A CN201610706023.3A CN201610706023A CN106240835A CN 106240835 A CN106240835 A CN 106240835A CN 201610706023 A CN201610706023 A CN 201610706023A CN 106240835 A CN106240835 A CN 106240835A
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- China
- Prior art keywords
- check cable
- carrier
- capstan winch
- double flute
- housing
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- 210000000080 chela (arthropods) Anatomy 0.000 claims description 5
- 239000000203 mixture Substances 0.000 claims description 3
- 208000019300 CLIPPERS Diseases 0.000 claims description 2
- 208000021930 chronic lymphocytic inflammation with pontine perivascular enhancement responsive to steroids Diseases 0.000 claims description 2
- 238000013016 damping Methods 0.000 abstract description 3
- 230000003139 buffering effect Effects 0.000 abstract description 2
- 238000010276 construction Methods 0.000 abstract description 2
- 230000009977 dual effect Effects 0.000 abstract description 2
- 238000012163 sequencing technique Methods 0.000 abstract description 2
- 238000005516 engineering process Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011982 device technology Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000686 essence Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 238000007363 ring formation reaction Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/02—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables
- B64F1/025—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables using decelerating or arresting beds
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Regulating Braking Force (AREA)
Abstract
nullThe present invention provides a kind of check cable idle Automatic-reset carrier landing stopping device，The ingenious produced rotating speed of change utilizing check cable coiling diameter on coaxial double flute capstan winch and the change of moment of torsion，Control rate of release and the damping drag torque of check cable，Resetting-mechanism provides the elasticity of safety to block buffering by the reverse elasticity moment of torsion of rigidity clockwork spring for carrier landing，Arrestment mechanism can control the rate of release of the rotating speed Based Intelligent Control check cable of brake disc and block carrier-borne aircraft enforcement intelligence，Blocking resetting-mechanism after successfully provides reactive torque to drive double flute capstan winch to rotate check cable withdrawal for double flute capstan winch again，The whole reseting procedure of check cable provides power without outside，There is sequencing and the automatization of height，Use the coaxial capstan winch of double flute for the dual MCU system capstan winch that prior art is arranged on warship runway both sides，Check cable two ends rate of release in double flute reef dish with reclaim that speed is identical ensure that carrier landing line sliding.The advantage of this stopping device is that volume is little, takes up room little, and simple in construction, intelligence degree are high, it is easy to manipulation and high service life.
Description
Technical field
The present invention relates to a kind of military equipment or aircraft carrier warship and blocked technical field, specifically one is blocked
Rope idle Automatic-reset carrier landing stopping device.
Background technology
Stopping device is important equipment on aircraft carrier, is mainly used in the carrier-borne aircraft warship that slows down in type aircraft carrier deck, at present, aviation
The technology of China is sealed by mother ship carrier carrier-borne aircraft stopping device technology due to western countries, and the information obtained seldom cannot make relevant commenting
Valency.Applicant warship stopping device at No. 201210190929.6 patents formerly disclosed reducing electromagnetic damping aircraft carrier, is
A kind of split-type structural, the deficiency in use existed is that volume is big, structure is complicated, is difficult to install and use, and side accounts for belowdecks
With bigger space.
Summary of the invention
The technical assignment of the present invention be to provide a kind of simple in construction, reasonable in design, volume is little, easy to use, safe,
Service life is long, adapt to various aircraft carrier block landing check cable idle Automatic-reset carrier landing block
Resistance device.
The technical scheme is that and realize in the following manner: operation principle is as follows:
Including housing, block mechanism, resetting-mechanism, arrestment mechanism, brake disc rotational speed governor and reverse pulley, wherein, housing
It is arranged on below centre, carrier landing runway deck, blocks mechanism and be made up of double flute capstan winch, universal driving shaft and check cable, double flute
Capstan winch is fixed in the middle of housing by universal driving shaft, and the both sides of housing have the through hole passed through for check cable, the both ends of check cable
Being each passed through in the middle of the through hole entrance double flute capstan winch of housing both sides and be fixed together with universal driving shaft, the remainder of check cable is respectively
Among two the independent check cable grooves up and down being wrapped in the same direction in double flute capstan winch, the check cable 7 termination interconnection cyclization of hull outside
Shape, walks around respectively and arranges aircraft carrier and two reverse pulleys of both sides, warship runway deck and be horizontally installed on carrier landing and run
Above deck, road；
Resetting-mechanism is made up of the lower section being arranged on double flute capstan winch, elastic clockwork spring dish curl, termination, center elastic clockwork spring
Fixing with universal driving shaft, outer rounded head is fixed with housing；
Electromagnetic brake is arranged on the bottom of housing, brake disc and electromagnetic braking clamp and form, the center of brake disc and linkage
Axle stretches out the lower end of housing bottom and connects, and the edge of bottom and brake disc that electromagnetic braking pincers are arranged on housing is connected composition braking
Mechanism, brake disc rotational speed governor is arranged on the side of housing and controls brake disc by controlling cable with electromagnetic braking clipper joint
Rotating speed；
The method for arresting of check cable idle Automatic-reset carrier landing stopping device is as follows:
When carrier-borne aircraft pintle hook check cable start check cable from capstan winch to pull out time, check cable winding on double flute capstan winch
Radius is more than universal driving shaft radius, and it is minimum that carrier-borne aircraft is blocked power by stopping device, and the damage to carrier-borne aircraft is minimum, along with blocking of pull-out
Resistance Suo Changdu increases, and check cable winding radius on capstan winch tapers into, when winding radius moves closer to the radius of universal driving shaft
Time, carrier-borne aircraft is blocked moment and is gradually increased until carrier-borne aircraft and is blocked and stop by check cable；By controlling electromagnetic brake control
Double flute capstan winch implemented braking moment by brake disc rotating speed processed intelligence, control realization to carrier-borne aircraft from a high speed to low speed until stopping
Intelligence is blocked；
The auxiliary of resetting-mechanism is blocked: when check cable is not hooked by carrier-borne aircraft pintle, the elastic clockwork spring of resetting-mechanism is in
Loose condition (of surface), once check cable is hooked by carrier-borne aircraft pintle, and check cable affects double flute capstan winch to rotate, and universal driving shaft is moved in double flute reef dribbling
Rotating, universal driving shaft starts to tighten rigidity clockwork spring, and rigidity clockwork spring produces the release of reactive torque tissue check cable to universal driving shaft, blocks
The check cable that rope is pulled out by carrier-borne aircraft is the longest, and the reactive torque that clockwork spring produces is the biggest, until coordinating carrier-borne aircraft with arrestment mechanism
Block and stop；
Carrier-borne aircraft removes pintle after stopping, arrestment mechanism slowly discharges, and the rigidity clockwork spring in reset machine slowly expands reset, simultaneously
Traction double flute capstan winch rotates and again backs up among double flute capstan winch by the check cable discharged, horizontal blocking on warship runway
Rope is tightened up, wait next time warship block.
The excellent effect of the present invention is, ingenious utilizes check cable change of coiling diameter on coaxial double flute capstan winch to be produced
Rotating speed and the change of moment of torsion, control rate of release and the damping drag torque of check cable, resetting-mechanism is by rigidity clockwork spring
Reverse elasticity moment of torsion provides the elasticity of safety to block buffering for carrier landing, and arrestment mechanism can control the rotating speed intelligence of brake disc
Carrier-borne aircraft enforcement intelligence is blocked by the rate of release that can control check cable, and blocking resetting-mechanism after successfully provides for double flute capstan winch again
Reactive torque drives double flute capstan winch to rotate and is regained by check cable, and the whole reseting procedure of check cable provides power without outside, has
The sequencing of height and automatization, use the coaxial capstan winch of double flute to be arranged on the dual MCU system of warship runway both sides relative to prior art
For capstan winch, check cable two ends rate of release in double flute reef dish with reclaim that speed is identical ensure that carrier landing straight line
Slide.Use resetting-mechanism to reclaim check cable, eliminate traditional motor and drive recovery, but equipment is thinning, takes up room more
Little, it is more beneficial for the installation under type aircraft carrier deck.
Accompanying drawing explanation
Fig. 1 is the section structure schematic diagram of stopping device；
Fig. 2 is that stopping device blocks embodiment schematic diagram.
Description of reference numerals: housing 1, universal driving shaft 2, elastic clockwork spring 3, brake disc 4, electromagnetic braking pincers 5, double flute capstan winch 6, block
Resistance rope 7, deck 8, brake disc speed control 9, reverse pulley 10.
Detailed description of the invention
Referring to the drawings check cable idle Automatic-reset carrier landing stopping device is made following detailed description of.
As shown in Figure 1-2, described check cable idle Automatic-reset carrier landing stopping device, its structure is by shell
Body 1, block mechanism, resetting-mechanism, arrestment mechanism, brake disc rotational speed governor 9 and reversely pulley 10 form, wherein, housing 1 sets
Put below centre, carrier landing runway deck 8, block mechanism and be made up of double flute capstan winch 6, universal driving shaft 2 and check cable 7, double
Groove cutter dish 6 is fixed in the middle of housing 1 by universal driving shaft 2, and the both sides of housing 1 have the through hole passed through for check cable, check cable 7
Both ends are each passed through the through hole of housing 1 both sides and enter in the middle of double flute capstan winch 6 and be fixed together with universal driving shaft 2, its of check cable 7
Among two independent check cable grooves up and down that remaining part is wrapped in double flute capstan winch 6 the most in the same direction, the check cable 7 outside housing 1
Termination interconnection circularizes, and walks around respectively and arranges aircraft carrier and two reverse pulleys 10 of both sides, warship runway deck 8 and laterally set
Put on carrier landing runway deck 8；
Resetting-mechanism is made up of elastic clockwork spring 3, and resetting-mechanism is arranged on the lower section of double flute capstan winch 6, and elastic clockwork spring 3 dish becomes spiral
Shape, termination, center is fixing with universal driving shaft 2, and outer rounded head is fixed with housing 1；
Electromagnetic brake is arranged on the bottom of housing 1, brake disc 4 and electromagnetic braking clamp 5 and form, the center of brake disc 4 with
Universal driving shaft 2 stretches out the lower end bottom housing 1 and connects, and the edge of bottom and brake disc 4 that electromagnetic braking pincers 5 are arranged on housing 1 connects
Connecing composition arrestment mechanism, brake disc rotational speed governor 9 is arranged on the side of housing 1 by controlling cable with electromagnetic braking pincers 5 even
Connect the rotating speed controlling brake disc 4.
Embodiment
The method for arresting of check cable idle Automatic-reset carrier landing stopping device is as follows:
When carrier-borne aircraft pintle hook check cable start check cable from capstan winch to pull out time, check cable winding on double flute capstan winch
Radius is more than universal driving shaft radius, and it is minimum that carrier-borne aircraft is blocked power by stopping device, and the damage to carrier-borne aircraft is minimum, along with blocking of pull-out
Resistance Suo Changdu increases, and check cable winding radius on capstan winch tapers into, when winding radius moves closer to the radius of universal driving shaft
Time, carrier-borne aircraft is blocked moment and is gradually increased until carrier-borne aircraft and is blocked and stop by check cable；By controlling electromagnetic brake control
Double flute capstan winch implemented braking moment by brake disc rotating speed processed intelligence, control realization to carrier-borne aircraft from a high speed to low speed until stopping
Intelligence is blocked；
The auxiliary of resetting-mechanism is blocked: when check cable is not hooked by carrier-borne aircraft pintle, the elastic clockwork spring of resetting-mechanism is in
Loose condition (of surface), once check cable is hooked by carrier-borne aircraft pintle, and check cable affects double flute capstan winch to rotate, and universal driving shaft is moved in double flute reef dribbling
Rotating, universal driving shaft starts to tighten rigidity clockwork spring, and rigidity clockwork spring produces the release of reactive torque tissue check cable to universal driving shaft, blocks
The check cable that rope is pulled out by carrier-borne aircraft is the longest, and the reactive torque that clockwork spring produces is the biggest, until coordinating carrier-borne aircraft with arrestment mechanism
Block and stop；
Carrier-borne aircraft removes pintle after stopping, arrestment mechanism slowly discharges, and the rigidity clockwork spring in reset machine slowly expands reset, simultaneously
Traction double flute capstan winch rotates and again backs up among double flute capstan winch by the check cable discharged, horizontal blocking on warship runway
Rope is tightened up, wait next time warship block.
Brake disc rotational speed governor, by Single-chip Controlling, controls the rotating speed of brake disc according to pre-set programs and then controls carrier-borne
Warship pull-out distance by machine.
The foregoing is only the preferred embodiments of the present invention, be not limited to the present invention, although with reference to aforementioned reality
Executing example to be described in detail the present invention, for a person skilled in the art, it still can be to aforementioned each enforcement
Technical scheme described in example is modified, or wherein portion of techniques feature is carried out equivalent.All essences in the present invention
Any amendment, equivalent or the improvement etc. made within god and principle, should be included within the scope of the present invention.
The known technology of those skilled in the art it is in addition to technical characteristic disclosed in the description of the present invention.
Claims (1)
1. check cable idle Automatic-reset carrier landing stopping device, it is characterised in that include housing, block mechanism, multiple
Position mechanism, arrestment mechanism, brake disc rotational speed governor and reverse pulley, wherein, housing is arranged on carrier landing runway deck
Below centre, blocking mechanism and be made up of double flute capstan winch, universal driving shaft and check cable, double flute capstan winch is fixed on housing by universal driving shaft
Centre, the both sides of housing have the through hole passed through for check cable, and the both ends of check cable are each passed through the through hole of housing both sides and enter
Entering and be fixed together with universal driving shaft in the middle of double flute capstan winch, it is upper that the remainder of check cable is wrapped in double flute capstan winch the most in the same direction
Among lower two independent check cable grooves, the check cable termination interconnection of hull outside circularizes, and walks around respectively and arranges aircraft carrier
Two the reverse pulleys both sides, warship runway deck are horizontally installed on above carrier landing runway deck；
Resetting-mechanism is made up of the lower section being arranged on double flute capstan winch, elastic clockwork spring dish curl, termination, center elastic clockwork spring
Fixing with universal driving shaft, outer rounded head is fixed with housing；
Electromagnetic brake is arranged on the bottom of housing, brake disc and electromagnetic braking clamp and form, the center of brake disc and linkage
Axle stretches out the lower end of housing bottom and connects, and the edge of bottom and brake disc that electromagnetic braking pincers are arranged on housing is connected composition braking
Mechanism, brake disc rotational speed governor is arranged on the side of housing and controls brake disc by controlling cable with electromagnetic braking clipper joint
Rotating speed；
The method for arresting of check cable idle Automatic-reset carrier landing stopping device is as follows:
When carrier-borne aircraft pintle hook check cable start check cable from capstan winch to pull out time, check cable winding on double flute capstan winch
Radius is more than universal driving shaft radius, and it is minimum that carrier-borne aircraft is blocked power by stopping device, and the damage to carrier-borne aircraft is minimum, along with blocking of pull-out
Resistance Suo Changdu increases, and check cable winding radius on capstan winch tapers into, when winding radius moves closer to the radius of universal driving shaft
Time, carrier-borne aircraft is blocked moment and is gradually increased until carrier-borne aircraft and is blocked and stop by check cable；By controlling electromagnetic brake control
Double flute capstan winch implemented braking moment by brake disc rotating speed processed intelligence, control realization to carrier-borne aircraft from a high speed to low speed until stopping
Intelligence is blocked；
The auxiliary of resetting-mechanism is blocked: when check cable is not hooked by carrier-borne aircraft pintle, the elastic clockwork spring of resetting-mechanism is in
Loose condition (of surface), once check cable is hooked by carrier-borne aircraft pintle, and check cable affects double flute capstan winch to rotate, and universal driving shaft is moved in double flute reef dribbling
Rotating, universal driving shaft starts to tighten rigidity clockwork spring, and rigidity clockwork spring produces the release of reactive torque tissue check cable to universal driving shaft, blocks
The check cable that rope is pulled out by carrier-borne aircraft is the longest, and the reactive torque that clockwork spring produces is the biggest, until coordinating carrier-borne aircraft with arrestment mechanism
Block and stop；
Carrier-borne aircraft removes pintle after stopping, arrestment mechanism slowly discharges, and the rigidity clockwork spring in reset machine slowly expands reset, simultaneously
Traction double flute capstan winch rotates and again backs up among double flute capstan winch by the check cable discharged, horizontal blocking on warship runway
Rope is tightened up, wait next time warship block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610706023.3A CN106240835B (en) | 2016-08-23 | 2016-08-23 | Check cable Automatic-reset carrier landing stopping device and its method for arresting |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610706023.3A CN106240835B (en) | 2016-08-23 | 2016-08-23 | Check cable Automatic-reset carrier landing stopping device and its method for arresting |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106240835A true CN106240835A (en) | 2016-12-21 |
| CN106240835B CN106240835B (en) | 2019-02-26 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610706023.3A Active CN106240835B (en) | 2016-08-23 | 2016-08-23 | Check cable Automatic-reset carrier landing stopping device and its method for arresting |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110510063A (en) * | 2019-07-19 | 2019-11-29 | 南京拓恒无人系统研究院有限公司 | A kind of unmanned boat berths fixed system |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060131462A1 (en) * | 2004-12-20 | 2006-06-22 | Holland Leo D | Turboelectric arresting gear |
| CN103482077A (en) * | 2012-06-12 | 2014-01-01 | 济南高达信息技术有限公司 | Variable-torque electromagnetic damping type carrier-based aircraft landing arrester |
| CN105584639A (en) * | 2016-03-14 | 2016-05-18 | 济南环太机电技术有限公司 | Integrated disc type shipboard aircraft landing stopper with clutch and stopping method of integrated disc type shipboard aircraft landing stopper |
| CN105584638A (en) * | 2016-03-14 | 2016-05-18 | 济南环太机电技术有限公司 | Integrated disc-type carrier aircraft landing arresting device and arresting method thereof |
| CN206068189U (en) * | 2016-08-23 | 2017-04-05 | 邹城众达知识产权咨询服务有限公司 | Check cable idle Automatic-reset carrier landing stopping device |
-
2016
- 2016-08-23 CN CN201610706023.3A patent/CN106240835B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060131462A1 (en) * | 2004-12-20 | 2006-06-22 | Holland Leo D | Turboelectric arresting gear |
| CN103482077A (en) * | 2012-06-12 | 2014-01-01 | 济南高达信息技术有限公司 | Variable-torque electromagnetic damping type carrier-based aircraft landing arrester |
| CN105584639A (en) * | 2016-03-14 | 2016-05-18 | 济南环太机电技术有限公司 | Integrated disc type shipboard aircraft landing stopper with clutch and stopping method of integrated disc type shipboard aircraft landing stopper |
| CN105584638A (en) * | 2016-03-14 | 2016-05-18 | 济南环太机电技术有限公司 | Integrated disc-type carrier aircraft landing arresting device and arresting method thereof |
| CN206068189U (en) * | 2016-08-23 | 2017-04-05 | 邹城众达知识产权咨询服务有限公司 | Check cable idle Automatic-reset carrier landing stopping device |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110510063A (en) * | 2019-07-19 | 2019-11-29 | 南京拓恒无人系统研究院有限公司 | A kind of unmanned boat berths fixed system |
| CN110510063B (en) * | 2019-07-19 | 2023-09-26 | 南京拓恒无人系统研究院有限公司 | Unmanned ship berthing fixing system |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106240835B (en) | 2019-02-26 |
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Effective date of registration: 20191125 Address after: 210000 Southern District of Lishui Economic Development Zone, Nanjing, Jiangsu Patentee after: Nanjing All Delight Refrigeration Equipment Co., Ltd. Address before: 250014, Ji'nan, Shandong Province, No. 18 West Hill Road, Holland manor 5-4-601 Patentee before: Jinan Huantai Electromechanical Technology Co., Ltd. |
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Effective date of registration: 20210409 Address after: 366 Chicheng Road, Tiantai County, Taizhou City, Zhejiang Province Patentee after: Jiang Jiping Address before: 210000 Southern District of Lishui Economic Development Zone, Nanjing, Jiangsu Patentee before: NANJING ALL DELIGHT REFRIGERATION EQUIPMENT Co.,Ltd. |
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Effective date of registration: 20211229 Address after: 313000 1-D, building 1, No. 656, Qixing Road, high tech Zone, Wuxing District, Huzhou City, Zhejiang Province Patentee after: Huzhou Dali Intelligent Equipment Manufacturing Co., Ltd Address before: 366 Chicheng Road, Tiantai County, Taizhou City, Zhejiang Province Patentee before: Jiang Jiping |
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| TR01 | Transfer of patent right |