CN109050960A - A kind of arresting gear to land for aircraft safety - Google Patents
A kind of arresting gear to land for aircraft safety Download PDFInfo
- Publication number
- CN109050960A CN109050960A CN201810803381.5A CN201810803381A CN109050960A CN 109050960 A CN109050960 A CN 109050960A CN 201810803381 A CN201810803381 A CN 201810803381A CN 109050960 A CN109050960 A CN 109050960A
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- electric
- cable
- stake
- land
- aircraft
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- 238000012806 monitoring device Methods 0.000 claims abstract description 14
- 230000007246 mechanism Effects 0.000 claims description 14
- 230000000903 blocking effect Effects 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims 1
- 230000003028 elevating effect Effects 0.000 claims 1
- 238000004804 winding Methods 0.000 claims 1
- 230000009977 dual effect Effects 0.000 abstract description 3
- 230000006698 induction Effects 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000001105 regulatory effect Effects 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Train Traffic Observation, Control, And Security (AREA)
Abstract
The invention discloses a kind of arresting gears to land for aircraft safety, including deck, the top on the deck is from left to right successively arranged the first electric up-down stake, first monitoring device, second electric up-down stake, first electric lifting rod, second monitoring device, the stake of third electric up-down and the second electric lifting rod, this arresting gear to land for aircraft safety, cable and second is blocked by first to block cable aircraft dual block, substantially increase the ability to work of the arresting gear, it breaks if first blocks cable, fail to stop in the aircraft of high speed slide, first to break blocks cable can be to high speed swinging around, for the safety of periphery personnel, that time that cable breaks is blocked when first, first electric up-down stake can bounce rapidly, it forces break first to block cable to act on above the first electric up-down stake, it protects and around works The safety of personnel.
Description
Technical field
The present invention relates to arresting gear technical field, specially a kind of arresting gear to land for aircraft safety.
Background technique
In the prior art: application publication number be the patent of 103129743 A of CN disclose one kind warship arresting gear, it is main
It is made of left slider, right sliding block, left damper tube cylinder, right damper tube cylinder, sliding gas return pipe, sliding gas return pipe regulating valve etc., using blocking
Resistance rope both ends are respectively connected with left rope winder, the right rope winder in left slider, right sliding block respectively, aircraft warship rear molding hook and block
Rope is hindered, check cable dragging left slider, right sliding block is driven to be gradually increased respectively in left damper tube cylinder and the acquisition of right damper tube cylinder simultaneously
Making aircraft with the resistance forward slip of variation and stop, only having one layer of arrester, safety is low, it is impossible to meet
Use demand.
Summary of the invention
The technical problem to be solved by the present invention is to overcome the existing defects, provides a kind of blocking for aircraft safety landing
Device, it is highly-safe, it can satisfy use demand, can effectively solve the problems in background technique.
To achieve the above object, the invention provides the following technical scheme: it is a kind of for aircraft safety land arresting gear,
Including deck, the top on the deck is from left to right successively arranged the first electric up-down stake, the first monitoring device, the second electronic liter
Stake, the first electric lifting rod, the second monitoring device, the stake of third electric up-down and the second electric lifting rod, the second electric up-down drop
The top of stake is rotatably connected to the first directive wheel by the first rotating mechanism, and the telescopic end of first electric lifting rod is fixed with
First mounting base, the side of the first mounting base are equipped with the first hydraulic bjuffer, the movable end of first hydraulic bjuffer
It is fixed with first and blocks cable, first, which blocks cable, is wrapped on the first directive wheel, and first blocks cable and the first hydraulic bjuffer
Junction is equipped with tension sensor, and the third electric up-down stake is rotatably connected to the second guiding by the second rotating mechanism
Wheel, the telescopic end of the second electric lifting rod are fixed with the second mounting base, and it is hydraulic that the side of second mounting base is equipped with second
Buffer, the movable end of the second hydraulic bjuffer are connected with second and block cable, and second blocks cable and be wrapped in the second directive wheel
On, the output end of the input terminal electrical connection external power supply of the open source single-chip microcontroller, the output end for single-chip microcontroller of increasing income is respectively with first
Electric up-down stake, the second electric up-down stake, the first electric lifting rod, the stake of third electric up-down and the second electric lifting rod input
End electrical connection, the input terminal of the output end electrical connection open source single-chip microcontroller of the tension sensor.
As a preferred technical solution of the present invention, first monitoring device includes the first infrared remote receiver and first
Infrared transmitter, the first infrared remote receiver and the first infrared transmitter are left and right symmetrically arranged red at the top on deck, described first
The output end of outer receiver and the first infrared transmitter is electrically connected with the input terminal of open source single-chip microcontroller.
As a preferred technical solution of the present invention, first rotating mechanism includes first bearing, first bearing peace
Mounted in the top of the second electric up-down stake, the first bearing is rotatablely connected by the first rotary shaft and the first directive wheel.
As a preferred technical solution of the present invention, second monitoring device includes the second infrared transmitter and second
Infrared remote receiver, the second infrared transmitter and the second infrared remote receiver are left and right symmetrically arranged red at the top on deck, described second
The output end of external transmitter and the second infrared remote receiver is electrically connected with the input terminal of open source single-chip microcontroller.
As a preferred technical solution of the present invention, second rotating mechanism includes second bearing, second bearing peace
Mounted in the retractable ends of third electric up-down stake, the second bearing is rotatablely connected by the second rotary shaft and the second directive wheel.
Compared with prior art, the beneficial effects of the present invention are: this arresting gear for landing for aircraft safety, by the
One block cable and second block cable to aircraft carry out it is dual block, substantially increase the ability to work of the arresting gear, if the
One, which blocks cable, breaks, and fails to stop in the aircraft of high speed slide, first to break blocks cable can be to high speed swinging around, for week
The safety of side personnel, when first blocks that time that cable breaks, the first electric up-down stake can be bounced rapidly, force first to break
It blocks cable to act on above the first electric up-down stake, protects the safety of staff around.
Detailed description of the invention
Fig. 1 is schematic structural view of the invention.
In figure: 1 deck, 2 first electric up-down stakes, 3 first infrared remote receivers, 4 first infrared transmitters, 5 second electronic
Lifting pole, 6 first electric lifting rods, 7 third electric up-down stakes, 8 second electric lifting rods, 9 second hydraulic bjuffers, 10 open sources
Cable, 15 second mounting bases, 16 second are blocked in single-chip microcontroller, 11 second bearings, 12 second rotary shafts, 13 second directive wheels, 14 second
Infrared transmitter, 17 second infrared remote receivers, 18 first mounting bases, 19 first hydraulic bjuffers, 20 tension sensors, 21 first
Block cable, 22 first rotary shafts, 23 first bearings, 24 first directive wheels, 25 first monitoring devices, 26 second rotating mechanisms, 27
Second monitoring device, 28 first rotating mechanisms.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Referring to Fig. 1, the present invention provides a kind of technical solution: a kind of arresting gear to land for aircraft safety, including
Deck 1, the top on deck 1 are from left to right successively arranged the first electric up-down stake 2, the first monitoring device 25, the second electric up-down
The 5, first electric lifting rod 6 of stake, the second monitoring device 27, the stake 7 of third electric up-down and the second electric lifting rod 8, second is electronic
The top of lifting pole 5 is rotatably connected to the first directive wheel 24, the telescopic end of the first electric lifting rod 6 by the first rotating mechanism 28
It is fixed with the first mounting base 18, the side of the first mounting base 18 is equipped with the first hydraulic bjuffer 19, the first hydraulic bjuffer 19
Movable end be fixed with first and block cable 21, first, which blocks cable 21, is wrapped on the first directive wheel 24, and first blocks cable 21
Tension sensor 20 is installed with the junction of the first hydraulic bjuffer 19, third electric up-down stake 7 passes through the second rotating mechanism
26 are rotatably connected to the second directive wheel 13, and the telescopic end of the second electric lifting rod 8 is fixed with the second mounting base 15, the second mounting base
15 side is equipped with the second hydraulic bjuffer 9, and the movable end of the second hydraulic bjuffer 9 is connected with second and blocks cable 14, and
Second, which blocks cable 14, is wrapped on the second directive wheel 13, the output end of the input terminal electrical connection external power supply of open source single-chip microcontroller 10,
Increase income single-chip microcontroller 10 output end respectively with the first electric up-down stake 2, the second electric up-down stake 5, the first electric lifting rod 6, the
The output end electrical connection open source of the electrical connection of the input terminal of three electric up-down stakes 7 and the second electric lifting rod 8, tension sensor 20 is single
The input terminal of piece machine 10.
First monitoring device 25 includes the first infrared remote receiver 3 and the first infrared transmitter 4,3 He of the first infrared remote receiver
First infrared transmitter 4 is left and right symmetrically arranged at the top on deck 1, the first infrared remote receiver 3 and the first infrared transmitter 4 it is defeated
Outlet is electrically connected with the input terminal of open source single-chip microcontroller 10, and open source single-chip microcontroller 10 controls the first infrared remote receiver 3 and emits signal, control
It makes the first infrared transmitter 4 and carries out reception signal, the transmission of disabling signal when aircraft taxi is to infrared induction region, first is red
Outer receiver 3 and the first infrared transmitter 4 will block information to pass to open source single-chip microcontroller 10, and open source single-chip microcontroller 10 carries out information
Analysis processing, controls the second electric up-down stake 5 and the first electric lifting rod 6 rises, and holds up to block cable 21 for first, aircraft
Empennage blocks hook and can block cable 21 with the first of picking-up and tangle, and first to block cable 21 to pull the first hydraulic bjuffer 19 be winged
Machine provides decelerating drag, and aircraft is promoted to stop.
First rotating mechanism 28 includes first bearing 23, and first bearing 23 is mounted on the top of the second electric up-down stake 5, the
One bearing 23 is rotatablely connected by the first rotary shaft 22 and the first directive wheel 24, and first, which blocks cable 21, passes through 24 band of the first directive wheel
Dynamic first rotary shaft 22 rotates in first bearing 23.
Tension sensor 20 is blocked the pulling force between cable 21 and the first hydraulic bjuffer 19 to first and is monitored, monitoring
Information passes to open source single-chip microcontroller 10, and open source single-chip microcontroller 10 is analyzed and processed information, blocks cable 21 in judgement first and snap
When, the first electric up-down stake 2 of control is risen, and is forced break first to block cable 21 and is acted on above the first electric up-down stake 2, is protected
The safety of surrounding staff is protected
Second monitoring device 27 includes the second infrared transmitter 16 and the second infrared remote receiver 17, the second infrared transmitter 16
It is left and right symmetrically arranged with the second infrared remote receiver 17 in the top on deck 1, the second infrared transmitter 16 and the second infrared remote receiver
17 output end is electrically connected with the input terminal of open source single-chip microcontroller 10, and open source single-chip microcontroller 10 controls the transmitting of the second infrared transmitter 16
Signal, the second infrared remote receiver 17 of control carry out reception signal, the biography of disabling signal when aircraft taxi is to infrared induction region
Defeated, the second infrared transmitter 16 and the second infrared remote receiver 17 will block information to pass to open source single-chip microcontroller 10, single-chip microcontroller of increasing income
10 pairs of information are analyzed and processed, and control the stake 7 of third electric up-down and the second electric lifting rod 8 rises, so that second be blocked
Cable 14 is held up, and aircraft tail blocks hook and can block cable 14 with the second of picking-up and tangle, and second, which blocks cable 14, pulls the second liquid
Compression buffer 9 provides decelerating drag for aircraft, and aircraft is promoted to stop.
Second rotating mechanism 26 includes second bearing 11, and second bearing 11 is mounted on the telescopic end of third electric up-down stake 7
Portion, second bearing 11 are rotatablely connected by the second rotary shaft 12 and the second directive wheel 13, and second, which blocks cable 14, passes through the second guiding
13 the second rotary shaft 12 of drive of wheel rotates in second bearing 11.
Single-chip microcontroller 10 of increasing income controls the first electric up-down stake 2, the second electric up-down stake 5, the first electric lifting rod 6, third
Electric up-down stake 7, the second electric lifting rod 8, tension sensor 20, the first infrared remote receiver 3, the first infrared transmitter 4, second
Infrared transmitter 16 and the second infrared remote receiver 17 are method commonly used in the prior art.
When in use: open source single-chip microcontroller 10 controls the first infrared remote receiver 3 and emits signal, controls the first infrared transmitter 4
Reception signal is carried out, the transmission of disabling signal when aircraft taxi is to infrared induction region, the first infrared remote receiver 3 and first red
External transmitter 4 will block information to pass to open source single-chip microcontroller 10, and open source single-chip microcontroller 10 is analyzed and processed information, control second
Electric up-down stake 5 and the first electric lifting rod 6 rise, and hold up to block cable 21 for first, and aircraft tail blocks hook meeting
Cable 21 is blocked with the first of picking-up to tangle, first, which blocks cable 21, pulls the first hydraulic bjuffer 19 to provide decelerating drag for aircraft,
Aircraft is promoted to stop.
Tension sensor 20 is blocked the pulling force between cable 21 and the first hydraulic bjuffer 19 to first and is monitored, monitoring
Information passes to open source single-chip microcontroller 10, and open source single-chip microcontroller 10 is analyzed and processed information, blocks cable 21 in judgement first and snap
When, the first electric up-down stake 2 of control is risen, and is forced break first to block cable 21 and is acted on above the first electric up-down stake 2.
Single-chip microcontroller 10 of increasing income controls the second infrared transmitter 16 and emits signal, and the second infrared remote receiver 17 of control is received
Signal, the transmission of disabling signal, the second infrared transmitter 16 and the second infrared receiver when aircraft taxi is to infrared induction region
Device 17 will block information to pass to open source single-chip microcontroller 10, and open source single-chip microcontroller 10 is analyzed and processed information, and control third is electronic
Lifting pole 7 and the second electric lifting rod 8 rise, and hold up to block cable 14 for second, the hook that blocks of aircraft tail can be with support
Second risen blocks cable 14 and tangles, and second, which blocks cable 14, pulls the second hydraulic bjuffer 9 to provide decelerating drag for aircraft, promotes to fly
Machine, which slows down, to be stopped.
The present invention by first block cable 21 and second block cable 14 to aircraft carry out it is dual block, substantially increase this and block
The ability to work of device is hindered, if first blocks cable 21 and break, fails to stop in the aircraft of high speed slide, first to break blocks
Cable 21 can block that time that cable 21 breaks when first, the first electronic liter to high speed swinging around, for the safety of periphery personnel
Drop stake 2 can bounce rapidly, force break first to block cable 21 and act on above the first electric up-down stake 2, protect work around
Make the safety of personnel.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (5)
1. a kind of arresting gear to land for aircraft safety, including deck (1), it is characterised in that: the top of the deck (1)
From left to right it is successively arranged the first electric up-down stake (2), the first monitoring device (25), the second electric up-down stake (5), first electronic
Elevating lever (6), the second monitoring device (27), third electric up-down stake (7) and the second electric lifting rod (8), the second electric up-down
The top of stake (5) is rotatably connected to the first directive wheel (24) by the first rotating mechanism (28), first electric lifting rod (6)
Telescopic end be fixed with the first mounting base (18), the side of the first mounting base (18) is equipped with the first hydraulic bjuffer (19), institute
The movable end for stating the first hydraulic bjuffer (19) is fixed with first and blocks cable (21), and first, which blocks cable (21), is wrapped in first and leads
To on wheel (24), and the first junction for blocking cable (21) and the first hydraulic bjuffer (19) is equipped with tension sensor (20),
The third electric up-down stake (7) is rotatably connected to the second directive wheel (13) by the second rotating mechanism (26), the second electronic liter
The telescopic end of drop bar (8) is fixed with the second mounting base (15), and it is hydraulic slow that the side of second mounting base (15) is equipped with second
It rushes device (9), the movable end of the second hydraulic bjuffer (9) is connected with second and blocks cable (14), and second blocks cable (14) winding
On the second directive wheel (13), the output end of the input terminal electrical connection external power supply of open source single-chip microcontroller (10), monolithic of increasing income
The output end of machine (10) respectively with the first electric up-down stake (2), the second electric up-down stake (5), the first electric lifting rod (6),
The electrical connection of the input terminal of three electric up-down stakes (7) and the second electric lifting rod (8), the output end electricity of the tension sensor (20)
The input terminal of connection open source single-chip microcontroller (10).
2. a kind of arresting gear to land for aircraft safety according to claim 1, it is characterised in that: first prison
Surveying device (25) includes the first infrared remote receiver (3) and the first infrared transmitter (4), the first infrared remote receiver (3) and first red
External transmitter (4) is left and right symmetrically arranged in the top of deck (1), first infrared remote receiver (3) and the first infrared transmitter
(4) output end is electrically connected with the input terminal of open source single-chip microcontroller (10).
3. a kind of arresting gear to land for aircraft safety according to claim 1, it is characterised in that: first rotation
Rotation mechanism (28) includes first bearing (23), and first bearing (23) is mounted on the top of the second electric up-down stake (5), and described first
Bearing (23) is rotatablely connected by the first rotary shaft (22) and the first directive wheel (24).
4. a kind of arresting gear to land for aircraft safety according to claim 1, it is characterised in that: second prison
Surveying device (27) includes the second infrared transmitter (16) and the second infrared remote receiver (17), the second infrared transmitter (16) and second
Infrared remote receiver (17) is left and right symmetrically arranged at the top of deck (1), and second infrared transmitter (16) and second infrared connects
The output end for receiving device (17) is electrically connected with the input terminal of open source single-chip microcontroller (10).
5. a kind of arresting gear to land for aircraft safety according to claim 1, it is characterised in that: second rotation
Rotation mechanism (26) includes second bearing (11), and second bearing (11) is mounted on the retractable ends of third electric up-down stake (7), described
Second bearing (11) is rotatablely connected by the second rotary shaft (12) and the second directive wheel (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810803381.5A CN109050960A (en) | 2018-07-20 | 2018-07-20 | A kind of arresting gear to land for aircraft safety |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810803381.5A CN109050960A (en) | 2018-07-20 | 2018-07-20 | A kind of arresting gear to land for aircraft safety |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109050960A true CN109050960A (en) | 2018-12-21 |
Family
ID=64817703
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810803381.5A Pending CN109050960A (en) | 2018-07-20 | 2018-07-20 | A kind of arresting gear to land for aircraft safety |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109050960A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104002981A (en) * | 2013-02-22 | 2014-08-27 | 上海市南洋模范中学 | Carrier plane landing aid system for small aircraft carriers |
| CN104149987A (en) * | 2014-08-06 | 2014-11-19 | 福州立益电器机械有限公司 | Blocking device used for power transportation device |
| CN204823968U (en) * | 2015-06-23 | 2015-12-02 | 安阳鑫龙煤业（集团）红岭煤业有限责任公司 | Colliery double speed winch wire rope collapses disconnected protector |
| CN107310736A (en) * | 2017-08-24 | 2017-11-03 | 河南师范大学 | A kind of carrier-borne aircraft landing accessory system |
| CN209112461U (en) * | 2018-07-20 | 2019-07-16 | 朱建华 | A kind of arresting gear to land for aircraft safety |
-
2018
- 2018-07-20 CN CN201810803381.5A patent/CN109050960A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104002981A (en) * | 2013-02-22 | 2014-08-27 | 上海市南洋模范中学 | Carrier plane landing aid system for small aircraft carriers |
| CN104149987A (en) * | 2014-08-06 | 2014-11-19 | 福州立益电器机械有限公司 | Blocking device used for power transportation device |
| CN204823968U (en) * | 2015-06-23 | 2015-12-02 | 安阳鑫龙煤业（集团）红岭煤业有限责任公司 | Colliery double speed winch wire rope collapses disconnected protector |
| CN107310736A (en) * | 2017-08-24 | 2017-11-03 | 河南师范大学 | A kind of carrier-borne aircraft landing accessory system |
| CN209112461U (en) * | 2018-07-20 | 2019-07-16 | 朱建华 | A kind of arresting gear to land for aircraft safety |
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