CN207089680U - A kind of carrier-borne aircraft landing system - Google Patents
A kind of carrier-borne aircraft landing system Download PDFInfo
- Publication number
- CN207089680U CN207089680U CN201721065234.XU CN201721065234U CN207089680U CN 207089680 U CN207089680 U CN 207089680U CN 201721065234 U CN201721065234 U CN 201721065234U CN 207089680 U CN207089680 U CN 207089680U
- 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.)
- Expired - Fee Related
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Classifications
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- 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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- Emergency Lowering Means (AREA)
Abstract
The utility model 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 utility model 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
It the utility model is related 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.
Utility model content
The purpose of this utility model is to provide a kind of carrier-borne aircraft landing system, can prevent that carrier-borne aircraft is right during declining
Type aircraft carrier deck and carrier-borne aircraft damage, and protect the personal safety of staff.
To achieve the above object, the utility model adopts the following technical scheme that：A kind of carrier-borne aircraft landing system, including set
Hanging cable device and the arrester that is arranged in type aircraft carrier deck in carrier-borne drive end unit, the hanging cable device include hanging cable and setting
In the balancing weight on slip 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
Individual balancing 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, it is described
Hook and slot is offered along carrier-borne aircraft direct of travel in type aircraft carrier deck, hook is stopped and is slideably positioned in hook and slot, the bottom for stopping hook
It is fixedly connected with one end of slide bar, slide bar is vertically arranged with stopping hook, and the other end of slide bar is fixedly connected with piston, the piston
For sealed set in inflator, described stop is provided with expansion link, the flexible side of expansion link on hook on the position below hook and slot
To perpendicular with the direct of travel of carrier-borne aircraft, positive stop hook, positive stop hook L are fixedly installed on the bottom surface of the type aircraft carrier deck afterbody
Type, the positive stop hook have two, are fixedly installed on the both ends of hook and slot respectively.
Preferably, the width of the hook and slot 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 utility model has the advantages that compared with prior art：
（1）Protective case is arranged with the hanging cable of carrier-borne drive end unit, therefore will not be collided with carrier-borne aircraft descent
Type aircraft carrier deck, it can be effectively prevented from causing damage to type aircraft carrier deck and carrier-borne aircraft fuselage；
（2）The utility model is engaged using positive stop hook, slide bar and inflator, and the deceleration of carrier-borne aircraft is realized using inflator, because
The phenomenon of arrester wires fracture will not occurs in this, prevent from causing huge injury to the staff on aircraft carrier, ensure staff's
Personal safety；
（3）The utility model is also provided with turbogenerator and battery, can be converted into the kinetic energy that carrier-borne aircraft lands
Utilization of power, economize on resources.
Brief description of the drawings
Fig. 1 is the structural representation of hanging cable device described in the utility model；
Fig. 2 is the structural representation of arrester described in the utility model；
Fig. 3 is use state figure of the present utility model.
Embodiment
The technical solution of the utility model is clearly and completely described below in conjunction with accompanying drawing, it is clear that described reality
It is only section Example of the present utility model to apply example, rather than whole embodiments.Based on the embodiment in the utility model,
Other all embodiments that those of ordinary skill in the art are obtained on the premise of creative work is not made, belong to this
The protection domain of utility model.
As shown in Figure 1 to Figure 3, a kind of carrier-borne aircraft landing system described in the utility model, including it is arranged at the tail of carrier-borne aircraft 1
The hanging cable device in portion, the arrester being arranged in type aircraft carrier deck 5 and control device, hanging cable device include hanging cable 2 and are arranged at
Balancing weight 3 on slip rope 2, 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, and two
Individual balancing weight 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 is kept vertically during decline, and balancing weight 3 is arranged at the middle part of hanging cable 2 position on the lower side, and protective case 4 is used in hanging cable 2
Prevent from causing damage to deck 5 when contacting deck 5, in the present embodiment, protective case 4 uses fire-retardant soft protective case, the He of hanging cable 2
Balancing weight 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 utility model is simple in construction, safe and reliable to operation, can not only prevent carrier-borne aircraft during declining to aircraft carrier first
Plate and carrier-borne aircraft damage, and can be effectively prevented from arrester wires fracture and show to what the person of staff damaged
As protecting 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 hook and slot, 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 |
|---|---|---|---|
| CN201721065234.XU CN207089680U (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 |
|---|---|---|---|
| CN201721065234.XU CN207089680U (en) | 2017-08-24 | 2017-08-24 | A kind of carrier-borne aircraft landing system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207089680U true CN207089680U (en) | 2018-03-13 |
Family
ID=61539414
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721065234.XU Expired - Fee Related CN207089680U (en) | 2017-08-24 | 2017-08-24 | A kind of carrier-borne aircraft landing system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207089680U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107444667A (en) * | 2017-08-24 | 2017-12-08 | 河南师范大学 | A kind of carrier-borne aircraft landing system |
-
2017
- 2017-08-24 CN CN201721065234.XU patent/CN207089680U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107444667A (en) * | 2017-08-24 | 2017-12-08 | 河南师范大学 | A kind of carrier-borne aircraft landing system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180313 Termination date: 20200824 |