CN107444667A - A kind of carrier-borne aircraft landing system - Google Patents
A kind of carrier-borne aircraft landing system Download PDFInfo
- Publication number
- CN107444667A CN107444667A CN201710734542.5A CN201710734542A CN107444667A CN 107444667 A CN107444667 A CN 107444667A CN 201710734542 A CN201710734542 A CN 201710734542A CN 107444667 A CN107444667 A CN 107444667A
- Authority
- CN
- China
- Prior art keywords
- hook
- carrier
- borne
- slide bar
- hanging cable
- 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
- 230000001681 protective effect Effects 0.000 claims abstract description 12
- 239000000463 material Substances 0.000 claims description 4
- 239000003063 flame retardant Substances 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims description 2
- 239000007787 solid Substances 0.000 claims 1
- 230000006378 damage Effects 0.000 abstract description 9
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 208000027418 Wounds and injury Diseases 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 208000014674 injury Diseases 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 229910052742 iron Inorganic materials 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D9/00—Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
- F03D9/10—Combinations of wind motors with apparatus storing energy
- F03D9/11—Combinations of wind motors with apparatus storing energy storing electrical energy
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E70/00—Other energy conversion or management systems reducing GHG emissions
- Y02E70/30—Systems combining energy storage with energy generation of non-fossil origin
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Power Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Emergency Lowering Means (AREA)
Abstract
The invention discloses a kind of carrier-borne aircraft landing system, including the hanging cable device of carrier-borne drive end unit and the arrester being arranged in type aircraft carrier deck are arranged at, hanging cable device includes hanging cable and the balancing weight being arranged on slip rope, and protective case is also arranged with hanging cable；The slide bar that arrester includes the obstruction hook being arranged in type aircraft carrier deck and is fixedly connected with stopping hook, in type aircraft carrier deck hook and slot is offered along carrier-borne aircraft direct of travel, hook is stopped to be slideably positioned in hook and slot, the bottom for stopping hook is fixedly connected with one end of slide bar, the other end of slide bar is fixedly connected with piston, piston seal is arranged in inflator, is stopped and is provided with expansion link on the position below hook and slot on hook, L-type positive stop hook is fixedly installed on the bottom surface of type aircraft carrier deck afterbody.The present invention can not only prevent carrier-borne aircraft from being damaged during declining to type aircraft carrier deck and carrier-borne aircraft, and can be effectively prevented from the phenomenon that arrester wires fracture damages to the person of staff, protect the personal safety of staff.
Description
Technical field
The present invention relates to carrier-borne aircraft lifting gear field, more particularly to a kind of carrier-borne aircraft landing system.
Background technology
At present, when carrier-borne aircraft lands, using the pintle for being arranged on carrier-borne drive end unit and it is arranged on type aircraft carrier deck
The landing system of arrester wires composition, the landing system have following technical problems in use：Firstly, because carrier-borne drive end unit
Pintle be stiff rod device, collided with type aircraft carrier deck so pintle can occur in descent, to type aircraft carrier deck and carrier-borne aircraft machine
Body causes damage；Secondly, the arrester wires in type aircraft carrier deck is easily broken, and when arrester wires is broken, is not protected and is arranged
Apply, huge injury can be caused to the staff on aircraft carrier.Such as：In the U.S. " Dwight Eisenhower " number heavy nuclear aircraft carrier
On, arrester wires is broken when a frame E2 early warning planes land, and is directly resulted in 8 staff on deck and is swept disconnected both legs.More than in view of
Defect, design a kind of safe and reliable carrier-borne aircraft landing system and be very important.
The content of the invention
It is an object of the invention to provide a kind of carrier-borne aircraft landing system, can prevent carrier-borne aircraft during declining to aircraft carrier
Deck and carrier-borne aircraft damage, and protect the personal safety of staff.
To achieve the above object, the present invention adopts the following technical scheme that：A kind of carrier-borne aircraft landing system, including it is arranged at warship
The hanging cable device of carrier aircraft afterbody and the arrester being arranged in type aircraft carrier deck, the hanging cable device include hanging cable and are arranged at cunning
Balancing weight on rope, the both ends of hanging cable are fixedly installed on the bottom surface of carrier-borne drive end unit, and the balancing weight has two, and two are matched somebody with somebody
Pouring weight is fixedly installed in hanging cable respectively, and protective case is arranged with the hanging cable between described two balancing weights；
The slide bar that the arrester includes the obstruction hook being arranged in type aircraft carrier deck and is fixedly connected with stopping hook, the aircraft carrier
Hook and slot is offered along carrier-borne aircraft direct of travel on deck, hook is stopped and is slideably positioned in hook and slot, the bottom for stopping hook and cunning
One end of bar is fixedly connected, and slide bar is vertically arranged with stopping hook, and the other end of slide bar is fixedly connected with piston, the piston seal
Be arranged in inflator, be provided with expansion link on the position stopped on hook below the hook and slot, the telescopic direction of expansion link with
The direct of travel of carrier-borne aircraft is perpendicular, and positive stop hook is fixedly installed on the bottom surface of the type aircraft carrier deck afterbody, and positive stop hook is L-type,
The positive stop hook has two, is fixedly installed on the both ends of hook and slot respectively.
Preferably, the width of the groove is more than the width for stopping hook.
Preferably, dovetail guide is provided with below the slide bar, dovetail guide is be arranged in parallel with slide bar, and the sliding bar is set
It is placed in dovetail guide.
Preferably, the inflator is connected with turbogenerator through gas pipeline, is provided with breather line logical for controlling
The magnetic valve of feed channel break-make, the turbogenerator are connected with battery.
Preferably, in addition to control device, the magnetic valve that the control device includes controller and is connected with controller are opened
Close and flexible lever switch, the electromagnetic valve switch control connection magnetic valve, the lever switch that stretches control connection expansion link.
Preferably, the protective case uses fire-retardant soft protective case, and the inflator barrel and breather line use resistance to height
Pressure material is made.
The present invention has the advantages that compared with prior art：
（1）Protective case is arranged with the hanging cable of carrier-borne drive end unit, therefore the aircraft carrier that will not be collided with carrier-borne aircraft descent
Deck, it can be effectively prevented from causing damage to type aircraft carrier deck and carrier-borne aircraft fuselage；
（2）The present invention is engaged using positive stop hook, slide bar and inflator, the deceleration of carrier-borne aircraft is realized using inflator, therefore will not send out
The phenomenon of raw arrester wires fracture, prevents from causing huge injury to the staff on aircraft carrier, ensures the personal safety of staff；
（3）The present invention is also provided with turbogenerator and battery, the kinetic energy that carrier-borne aircraft lands can be converted into utilization of power,
Economize on resources.
Brief description of the drawings
Fig. 1 is the structural representation of hanging cable device of the present invention；
Fig. 2 is the structural representation of arrester of the present invention；
Fig. 3 is the use state figure of the present invention.
Embodiment
Technical scheme is clearly and completely described below in conjunction with accompanying drawing, it is clear that described embodiment
Only section Example of the invention, rather than whole embodiments.Based on the embodiment in the present invention, the common skill in this area
Other all embodiments that art personnel are obtained on the premise of creative work is not made, belong to the protection model of the present invention
Enclose.
As shown in Figure 1 to Figure 3, a kind of carrier-borne aircraft landing system of the present invention, including it is arranged at the afterbody of carrier-borne aircraft 1
Hanging cable device, the arrester being arranged in type aircraft carrier deck 5 and control device, hanging cable device include hanging cable 2 and are arranged at slip rope 2
On balancing weight 3, the both ends of hanging cable 2 are fixedly installed on the bottom surface of the afterbody of carrier-borne aircraft 1, and balancing weight 3 has two, two counterweights
Block 3 is fixedly installed in hanging cable 2 respectively, and is arranged with protective case 4 in the hanging cable 2 between two balancing weights 3.In order that hanging cable 2
Keep vertical during decline, balancing weight 3 is arranged at the middle part of hanging cable 2 position on the lower side, and protective case 4 is used to contact in hanging cable 2
Prevent from causing damage to deck 5 during deck 5, in the present embodiment, protective case 4 uses fire-retardant soft protective case, hanging cable 2 and counterweight
Block 3 is made of the material of iron or equality strength.
The slide bar 8 that arrester includes the obstruction hook 6 being arranged in type aircraft carrier deck 5 and is fixedly connected with stopping hook 6, aircraft carrier
Hook and slot 7 is offered along carrier-borne aircraft direct of travel on deck 5, hook 6 is stopped and is slideably positioned in hook and slot 7, in the present embodiment, hook and slot
7 width is more than the width for stopping hook 6 so that stopping hook 6 can slide in hook and slot 7, stop bottom and the slide bar 8 of hook 6
One end is fixedly connected, and slide bar 8 is vertically arranged with stopping hook 6, and the lower section of slide bar 8 is provided with dovetail guide 9, and dovetail guide 9 and slide bar 8 are flat
Row is set, and slide bar 8 is arranged in dovetail guide 9, so that slide bar 8 drives obstruction hook 6 movable along dovetail guide 9, is stopped
Expansion link 13, the telescopic direction of expansion link 13 and the traveling side of carrier-borne aircraft 1 are provided with hook 6 on the position of the lower section of hook and slot 7
To perpendicular, expansion link 13 is connected with control device, and positive stop hook 12 is fixedly installed on the bottom surface of the afterbody of type aircraft carrier deck 5, spacing
Hook 12 is L-type, and in the present embodiment, positive stop hook 12 has two, is fixedly installed on the both ends of hook and slot 7 respectively, and positive stop hook 12 is used for
It is engaged with expansion link 13, so as to be fixed to stopping hook 6, the other end of slide bar 8 is fixedly connected with piston 11, and piston 11 is close
Envelope is arranged in inflator 10, and inflator 10 is connected through breather line 14 with turbogenerator 15, is provided with and is used on breather line 14
Control the magnetic valve 16 of the break-make of breather line 14, magnetic valve 16 is connected with control device, turbogenerator 15 also with battery 17
It is connected.Turbogenerator 15 is used to the air pressure in inflator 10 being converted into electric energy, and stores to battery 17.In the present embodiment
In, the barrel and breather line 14 of inflator 10 are made of high pressure resistant material.
Control device includes controller and the electromagnetic valve switch being connected with controller and flexible lever switch, electromagnetic valve switch control
System connection magnetic valve 16, stretch lever switch control connection expansion link 13.Wherein, controller with electromagnetic valve switch, controller with stretching
Annexation between contracting lever switch, electromagnetic valve switch and magnetic valve and flexible lever switch and expansion link is prior art, no
Repeat again.
In carrier-borne aircraft descent, carrier-borne aircraft pilot controls flying height, makes the bottom of hanging cable 2 of the afterbody of carrier-borne aircraft 1
Protective case 4 contact deck 5 and slide, when stopping hook 6 on the hook of hanging cable 2, led with stopping the slide bar 8 that is fixedly connected of hook 6 in dovetail
Linear slide on rail 9, the piston 11 that the rear end of slide bar 8 is fixed moves into inflator 10, when the air pressure in inflator 10 is to piston 11
When active force is more than carrier-borne aircraft 1 to the active force of piston 11, carrier-borne aircraft 1 reduces speed now, when carrier-borne aircraft 1 stops, ground handling
Personnel press expansion link control button, and expansion link 13, which stretches out to coordinate to complete to fix with positive stop hook 12, stops hook 6, surface personnel
Electromagnetic valve switch button is pressed, opens breather line 14, turbogenerator 15, which is started working, to generate electricity, and then deposits the electric energy of acquisition
Store up in battery 17.
The present invention is simple in construction, safe and reliable to operation, can not only prevent carrier-borne aircraft decline during to type aircraft carrier deck and
Carrier-borne aircraft damages, and can be effectively prevented from the phenomenon that arrester wires fracture damages to the person of staff, protects
Protect the personal safety of staff.
Claims (6)
- A kind of 1. carrier-borne aircraft landing system, it is characterised in that：Including being arranged at the hanging cable device of carrier-borne drive end unit and being arranged at boat Arrester on female deck, the hanging cable device includes hanging cable and the balancing weight being arranged on slip rope, the both ends of hanging cable are solid Surely it is arranged on the bottom surface of carrier-borne drive end unit, the balancing weight there are two, and two balancing weights are fixedly installed in hanging cable respectively, institute State and be arranged with protective case in the hanging cable between two balancing weights；The arrester includes the obstruction hook being arranged in type aircraft carrier deck And with stopping the slide bar that is fixedly connected of hook, hook and slot is offered along carrier-borne aircraft direct of travel in the type aircraft carrier deck, hook is stopped and slides It is arranged in hook and slot, the bottom for stopping hook is fixedly connected with one end of slide bar, and slide bar is vertically arranged with stopping hook, slide bar The other end is fixedly connected with piston, and the piston seal is arranged in inflator, the position stopped on hook below hook and slot On be provided with expansion link, the telescopic direction of expansion link and the direct of travel of carrier-borne aircraft are perpendicular, the bottom of the type aircraft carrier deck afterbody Positive stop hook is fixedly installed on face, positive stop hook is L-type, and the positive stop hook there are two, is fixedly installed on the both ends of hook and slot respectively.
- A kind of 2. carrier-borne aircraft landing system as claimed in claim 1, it is characterised in that：The width of the groove, which is more than, stops hook Width.
- A kind of 3. carrier-borne aircraft landing system as claimed in claim 1, it is characterised in that：Led below the slide bar provided with dovetail Rail, dovetail guide are be arranged in parallel with slide bar, and the sliding bar is arranged in dovetail guide.
- A kind of 4. carrier-borne aircraft landing system as described in claim 1 or 3, it is characterised in that：The inflator connects through gas pipeline Be connected to turbogenerator, be provided with the magnetic valve for controlling breather line break-make on breather line, the turbogenerator with Battery is connected.
- A kind of 5. carrier-borne aircraft landing system as claimed in claim 4, it is characterised in that：Also include control device, the control Device includes controller and the electromagnetic valve switch being connected with controller and flexible lever switch, the electromagnetic valve switch control connection electricity Magnet valve, stretch lever switch control connection expansion link.
- A kind of 6. carrier-borne aircraft landing system as claimed in claim 5, it is characterised in that：The protective case uses fire-retardant soft guarantor Sheath, the inflator barrel and breather line are made of high pressure resistant material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710734542.5A CN107444667A (en) | 2017-08-24 | 2017-08-24 | A kind of carrier-borne aircraft landing system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710734542.5A CN107444667A (en) | 2017-08-24 | 2017-08-24 | A kind of carrier-borne aircraft landing system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107444667A true CN107444667A (en) | 2017-12-08 |
Family
ID=60493063
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710734542.5A Pending CN107444667A (en) | 2017-08-24 | 2017-08-24 | A kind of carrier-borne aircraft landing system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107444667A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112340048A (en) * | 2020-10-22 | 2021-02-09 | 燕山大学 | Quick fixing and transverse moving system of electrically-driven ship-based helicopter |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1536480A (en) * | 1966-07-05 | 1968-08-16 | Bliss E W Co | Aircraft stop system |
| CN102358430A (en) * | 2011-07-27 | 2012-02-22 | 南京航空航天大学 | Ship-borne aircraft capturing and arresting device |
| DE102011111764A1 (en) * | 2011-08-24 | 2013-02-28 | Fischer-Richter Gbr (Vertretungsberechtigter Gesellschafter: Herr Christian Fischer, 01445 Radebeul) | Automatic landing device for landing e.g. aircraft on aircraft carrier, has extendable and hinged device extending arresting cable directly on equal height of hooks of aircraft to be landed, where cable is hooked in hooks up to height |
| CN103204245A (en) * | 2013-04-11 | 2013-07-17 | 西南交通大学 | Auxiliary landing device for shipboard aircraft of aircraft carrier |
| CN203428025U (en) * | 2013-07-31 | 2014-02-12 | 张大川 | Aircraft carrier-based aircraft landing stern hook and accessory device thereof |
| AU2015252128A1 (en) * | 2003-01-17 | 2015-12-03 | Insitu, Inc. | Methods and apparatuses for capturing unmanned aircraft and constraining motion of the captured aircraft |
| KR101726858B1 (en) * | 2016-10-05 | 2017-04-26 | 최재도 | Device for fixing and moving helicopter on shipboard |
| CN106828812A (en) * | 2016-12-29 | 2017-06-13 | 泰州职业技术学院 | Semi-submersible type deep-sea wind-powered electricity generation mounting platform and its wind power generating set integral installation method |
| CN207089680U (en) * | 2017-08-24 | 2018-03-13 | 河南师范大学 | A kind of carrier-borne aircraft landing system |
-
2017
- 2017-08-24 CN CN201710734542.5A patent/CN107444667A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1536480A (en) * | 1966-07-05 | 1968-08-16 | Bliss E W Co | Aircraft stop system |
| AU2015252128A1 (en) * | 2003-01-17 | 2015-12-03 | Insitu, Inc. | Methods and apparatuses for capturing unmanned aircraft and constraining motion of the captured aircraft |
| CN102358430A (en) * | 2011-07-27 | 2012-02-22 | 南京航空航天大学 | Ship-borne aircraft capturing and arresting device |
| DE102011111764A1 (en) * | 2011-08-24 | 2013-02-28 | Fischer-Richter Gbr (Vertretungsberechtigter Gesellschafter: Herr Christian Fischer, 01445 Radebeul) | Automatic landing device for landing e.g. aircraft on aircraft carrier, has extendable and hinged device extending arresting cable directly on equal height of hooks of aircraft to be landed, where cable is hooked in hooks up to height |
| CN103204245A (en) * | 2013-04-11 | 2013-07-17 | 西南交通大学 | Auxiliary landing device for shipboard aircraft of aircraft carrier |
| CN203428025U (en) * | 2013-07-31 | 2014-02-12 | 张大川 | Aircraft carrier-based aircraft landing stern hook and accessory device thereof |
| KR101726858B1 (en) * | 2016-10-05 | 2017-04-26 | 최재도 | Device for fixing and moving helicopter on shipboard |
| CN106828812A (en) * | 2016-12-29 | 2017-06-13 | 泰州职业技术学院 | Semi-submersible type deep-sea wind-powered electricity generation mounting platform and its wind power generating set integral installation method |
| CN207089680U (en) * | 2017-08-24 | 2018-03-13 | 河南师范大学 | A kind of carrier-borne aircraft landing system |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112340048A (en) * | 2020-10-22 | 2021-02-09 | 燕山大学 | Quick fixing and transverse moving system of electrically-driven ship-based helicopter |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| AD01 | Patent right deemed abandoned |
Effective date of abandoning: 20240607 |