CN107190608A - A kind of forced landing buffering rescue runway - Google Patents
A kind of forced landing buffering rescue runway Download PDFInfo
- Publication number
- CN107190608A CN107190608A CN201710600718.8A CN201710600718A CN107190608A CN 107190608 A CN107190608 A CN 107190608A CN 201710600718 A CN201710600718 A CN 201710600718A CN 107190608 A CN107190608 A CN 107190608A
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- runway
- rescue
- wall
- layer
- forced landing
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- 230000003139 buffering effect Effects 0.000 title claims abstract description 22
- 239000010410 layer Substances 0.000 claims description 76
- 239000011229 interlayer Substances 0.000 claims description 13
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 10
- 239000006260 foam Substances 0.000 claims description 7
- 239000000835 fiber Substances 0.000 claims description 6
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 5
- 239000000203 mixture Substances 0.000 description 9
- 230000000694 effects Effects 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- 239000000498 cooling water Substances 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 238000013517 stratification Methods 0.000 description 2
- 206010000369 Accident Diseases 0.000 description 1
- 241000628997 Flos Species 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000034994 death Effects 0.000 description 1
- 231100000517 death Toxicity 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Classifications
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C3/00—Fire prevention, containment or extinguishing specially adapted for particular objects or places
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C37/00—Control of fire-fighting equipment
- A62C37/04—Control of fire-fighting equipment with electrically-controlled release
-
- 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
-
- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01C—CONSTRUCTION OF, OR SURFACES FOR, ROADS, SPORTS GROUNDS, OR THE LIKE; MACHINES OR AUXILIARY TOOLS FOR CONSTRUCTION OR REPAIR
- E01C9/00—Special pavings; Pavings for special parts of roads or airfields
-
- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01F—ADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE
- E01F15/00—Safety arrangements for slowing, redirecting or stopping errant vehicles, e.g. guard posts or bollards; Arrangements for reducing damage to roadside structures due to vehicular impact
Landscapes
- Engineering & Computer Science (AREA)
- Health & Medical Sciences (AREA)
- Public Health (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Road Paving Structures (AREA)
Abstract
A kind of forced landing buffering rescue runway, is related to a kind of aircraft safety and road facility.The present invention solves existing aircraft hardness during forced landing and landed, the problem of easily occurring fatal crass.It includes rescue runway, stop wall and fire extinguishing system, the rescue runway is software runway, the rescue runway includes horizontally disposed primary runway, the angle of attack runway for being inclined at primary runway front end and the slope section runway for being inclined at primary runway rear end, the slope section one end of runway away from primary runway is set less than primary runway, the obstruction wall is that software stops wall, the wall that stops stops wall including the side for being arranged on the preceding obstruction wall of rescue runway front end with being arranged on rescue runway both sides, high-order angle of attack runway bottom is provided with command and control center, fire extinguishing system is arranged on the both sides of rescue runway, sensor is provided with rescue runway, fire extinguishing system passes through sensor control action.The present invention is used for forced landing rescue.
Description
Technical field
Road facility the present invention relates to a kind of aircraft safety, and in particular to a kind of forced landing buffering rescue runway.
Background technology
Nowadays aircraft trip is as a kind of main trip instrument, and annual global commerce flight frequency is up to ten million
Secondary, flight safety reliability is very high, but when aircraft because the reason such as machinery, hydraulic pressure or electric equipment failure cause undercarriage without
In the case that method is opened, or other reasons cause the dangerous property of aircraft regular descent, at this moment there is aircraft accident, machine ruins people
Situation about dying still can not be avoided, and probability of the forced landing without injures and deaths is very low, in aviation history and in modern Aviation practice, usually be gone out
Now because undercarriage fail cause aircraft can not regular descent the problem of, be forced landing when, can aircraft landing moment aircraft
Bottom enclosure and ground hard contact, cause the accident of fatal crass to occur.In order to avoid the generation of such accident, China and foreign countries' aviation
The engineers and technicians in field have carried out substantial amounts of technological improvement, but these technological improvements are to be conceived to undercarriage with aircraft to pacify
Above full performance.For example, installing electronic additional, surge, manually etc. in the mechanism of rise and fall rack control device and other handling failures.So
Although doing reduces the probability of accident generation, problems can not be fundamentally solved.
The content of the invention
The present invention is landed to solve existing aircraft hardness during forced landing, the problem of easily occurring fatal crass,
And then there is provided a kind of forced landing buffering rescue runway.
The present invention is for the technical scheme that is used of solution above-mentioned technical problem：
A kind of forced landing buffering rescue runway, it includes rescue runway, stops wall and fire extinguishing system, the rescue runway
For software runway, the rescue runway include horizontally disposed primary runway, the angle of attack runway for being inclined at primary runway front end and
The slope section runway of primary runway rear end is inclined at, the slope section one end of runway away from primary runway is set less than primary runway, the resistance
Block wall and stop wall for software, the obstruction wall includes being arranged on the preceding obstruction wall of rescue runway front end and is arranged on rescue runway two
The side of side stops wall, high-order angle of attack runway bottom is provided with command and control center, fire extinguishing system is arranged on rescue runway
Both sides, rescue runway on be provided with sensor, fire extinguishing system passes through sensor control action.
Further, each side is stopped and is provided with some anti-collision barrels on the inside of wall, and some anti-collision barrels are stopped along side
Wall length direction side by side and is vertically arranged, and the bottom of anti-collision barrel is positioned by they sup-port, and anti-collision barrel is rubber tube.
Further, the bottom surface that the bottom surface of rescue runway stops wall with side is generally aligned in the same plane, and each side stops wall with rescuing
Help and positioning interlayer is provided between runway, the bottom of anti-collision barrel is arranged on the top of positioning interlayer by support bar, wherein, prevent
Hit between cylinder and support bar, between support bar and positioning interlayer or between support bar and anti-collision barrel and positioning interlayer be to turn
Dynamic connection.
Further, twice buffer subsystem is arranged side by side on primary runway, the two ends of per pass buffer subsystem are respectively and fixedly connected to both sides
Side is stopped on wall.
Further, the rescue runway includes upper and lower two buffer layer, the hardness of the upper and lower two buffer layer according to
Wire netting is provided between secondary increase, upper and lower two buffer layer, the top surface of upper strata cushion is provided with two layers of tarpaulin；The resistance
Block and be provided with rubber slab between four layers of weight body sponge that wall includes being arranged side by side, adjacent heavy two layers body sponge；Forced landing is buffered
Rescuing runway also includes lash rope, and the heavy body sponge is stitched into one with rubber slab by lash rope.
Further, the upper strata cushion from top to bottom includes one layer of rubber slab, two layers weight body sponge, one layer of rubber
Plate, one layer of palm fibre pad, one layer of rubber slab, one layer of weight body sponge, two layers tarpaulin, one layer of weight body sponge, one layer of palm fibre pad, one layer of weight body sea
Continuous and one layer of rubber slab；It is hard that lower floor's cushion includes one layer of rubber slab, two layers of hard weight body sponge, one layer of palm fibre pad and one layer
Matter weight body sponge.
Further, open up fluted on ground, rescue runway and obstruction wall are respectively positioned in groove, positioned at rescue runway four
Groove is provided with the groove in week or in the groove of rescue runway both sides, the fire extinguishing system includes some groups of fire extinguishing components, if
Do described group of fire extinguishing component to be distributed in the side grooves of rescue runway, every group of fire extinguishing component includes the recirculated water being sequentially connected
Pump, foam water pot, high-pressure hydraulic pump and fire extinguishing sprayer.
Further, it is equal between the bottom of rescue runway and groove floor and between the bottom of obstruction wall and groove floor
Pedestal is provided with, angle of attack runway front upper is provided with two Observation telescopes, and two Observation telescopes stop wall respectively close to two sides
Set, the Observation telescope and command and control center UNICOM.
Further, it is 89m that two sides, which stop the distance between wall, and the thickness that each side stops wall is 5m, angle of attack runway
Range of tilt angles be 0 °~60 °.
The present invention has the following effects that compared with prior art：
The present invention can provide soft landing platform by rescuing runway and stopping wall in forced landing for aircraft, also,
In airplane soft landing, fire-fighting fire extinguishing measure can be taken in time, it is ensured that body and staff on board's safety, are that follow-up rescue is striven
Valuable time is taken, meanwhile, the action of fire extinguishing system can not only be controlled in command and control center, additionally it is possible to needed for storage rescue
Goods and materials, to ensure that first aid can be carried out to the personnel of body in time when aircraft breaks down and needs forced landing, and in rescue
Fire fighting truck or crane etc. is provided afterwards to clear up body.It is straight with aircraft by the forced landing buffering rescue runway of the present invention
Connect forced landing to compare on airfield runway, more timely to the personnel rescuing in body, rescue success rate improves 60 percent.
Brief description of the drawings
Fig. 1 is dimensional structure diagram of the invention；
Fig. 2 is schematic top plan view of the invention；
Fig. 3 is left view schematic diagram of the invention；
Fig. 4 is enlarged drawing (section section view) at Fig. 1 B；
Fig. 5 is sectional perspective structural representation (section section view) of the invention.
Embodiment
Embodiment one：Illustrate present embodiment, a kind of forced landing buffering rescue runway, its bag with reference to Fig. 1~5
Include rescue runway 1, stop wall and fire extinguishing system 7, the rescue runway 1 is software runway, and the rescue runway 1 is set including level
The primary runway 2 put, the slope section runway for being inclined at the angle of attack runway 4 of the front end of primary runway 2 and being inclined at the rear end of primary runway 2
3, the slope one end of section runway 3 away from primary runway 2 is set less than primary runway 2, and the obstruction wall is that software stops wall, the obstruction wall
Side including being arranged on the preceding obstruction wall 24 of rescue runway 1 front end and be arranged on rescue runway 1 both sides stops wall 5, positioned at a high position
The bottom of angle of attack runway 4 be provided with command and control center 6, fire extinguishing system 7 is arranged on the both sides of rescue runway 1, rescue runway 1
Sensor is provided with, fire extinguishing system 7 passes through sensor control action.
Rescue runway 1 and obstruction wall can provide cushioning effect for the forced landing of body, and soft landing, runway two are provided for aircraft
The fire extinguishing system 7 that side is set plays a part of putting out a fire to body.
Sensor is distributed in the top of rescue runway 1.Slope angle runway is that body falls into the offer transition of primary runway 2.Side stops wall 5
Vertical range between top to the top end face for rescuing runway 1 is 5m.
Rear during forced landing from rescue runway 1 enters, and rescue runway 1 is arranged near the normal duty runway in airport,
Command and control center 6 keeps real time information communications and liaison with airport overall control center, when feedback of the information has aircraft to need forced landing, rescues
The startup of each work system of runway 1 is helped, various rescue personnels are with equipment (such as fire fighting truck, ambulance etc.) in command and control center 6
Under total allotment, prepare rescue work, stop the moment on angle of attack runway 4, fire extinguishing system in primary runway 2 or front end when forced landing
7 automatic starts, to the mixture for rescuing shower water and fire foam on runway 1, are flown after rescuing successfully by wreck crane to forced landing
Machine carries out traction and removes out airport forced landing rescue runway 1.Command centre and command car can also control the work of fire extinguishing system
Make start and stop.
The present invention can be realized carries out forced landing rescue work, including civil aircraft, army to the aircraft of existing any type
With aircraft and Special Aircraft.
Embodiment two：Illustrate present embodiment with reference to Fig. 1~5, if the inner side that each side stops wall 5 is provided with
Dry anti-collision barrel 11, some anti-collision barrels 11 stop the length direction of wall 5 side by side along side and are vertically arranged, and the bottom of anti-collision barrel 11 leads to
They sup-port positioning is crossed, anti-collision barrel 11 is rubber tube.It is so designed that, anti-collision barrel 11 can also be Anti-collision barrel or bumping post.Machine
Body is after forced landing falls into rescue runway 1, and body stops wall 5 with both sides and is not directly contacted with, by the effect of anti-collision barrel 11, reduces resistance
The impact that wall is subject to is blocked, the speed of body is reduced.Other compositions are identical with embodiment one with annexation.
Embodiment three：Illustrate present embodiment with reference to Fig. 1~5, the bottom surface for rescuing runway 1 stops the bottom of wall with side
Face is generally aligned in the same plane, and each side, which is stopped, is provided with positioning interlayer 26, the bottom of anti-collision barrel 11 between wall 5 and rescue runway 1
By support bar be arranged on positioning interlayer 26 top, wherein, between anti-collision barrel 11 and support bar, support bar with positioning interlayer 26
Between or support bar and anti-collision barrel 11 and positioning interlayer 26 between be to be rotatably connected.It is so designed that, positioning interlayer 26 is
Weight body spongy layer, positioning interlayer 26 and side are provided with rubber slab between stopping wall 5.Anti-collision barrel 11 is rotatable, bent, in body
After being contacted with anti-collision barrel 11, can reduce its own and stop wall suffered by impulsive force, the speed of body can be reduced again.Other groups
Into identical with embodiment two with annexation.
Embodiment four：Illustrate twice buffering is arranged side by side on present embodiment, primary runway 2 with reference to Fig. 1,2,4,5
Net 8, the two ends of per pass buffer subsystem 8 are respectively and fixedly connected to the side of both sides and stopped on wall 5.It is so designed that, buffer subsystem 8 is elastic network(s),
Body is rushed to stops body one step ahead before angle of attack runway 4, effectively prevent body from gunning off the runway.One layer of buffer subsystem 8 arrives rescue runway 1
The distance of rear end is 1100m, and another layer of buffer subsystem 8 to the distance of rescue runway 1 rear end is 1365m.Other compositions are with being connected pass
System is identical with embodiment one, two or three.
Embodiment five：Illustrate present embodiment with reference to Fig. 1~5, the rescue runway 1 includes upper and lower two layers and delayed
Layer is rushed, the hardness of the upper and lower two buffer layer increases successively, and wire netting 15, upper strata are provided between upper and lower two buffer layer
The top surface of cushion is provided with two layers of tarpaulin 16；It is described to stop four layers of weight body sponge 13 that wall includes being arranged side by side, adjacent two layers
Rubber slab 14 is provided between weight body sponge 13；Forced landing buffering rescue runway also includes lash rope 12, the heavy body sea
Silk floss 13 is stitched into one with rubber slab 14 by lash rope 12.Be so designed that, by it is soft to hard two buffer layer can be machine
Body provides suitable buffering during forced landing.Wire netting 15 is steel mesh.Because the tamper-proof intensity of tarpaulin 16 is high, therefore tarpaulin
16 are arranged on above rubber slab, because tarpaulin 16 is relatively thin, therefore set two layers of tarpaulin 16.Between each Rotating fields of obstruction wall, rescue and run
Between each Rotating fields in road, and between rescue runway and obstruction wall, connect solid in the way of suture using lash rope 12
It is fixed, it is ensured that the stability of its structure.Other compositions are identical with embodiment four with annexation.
Embodiment six：Illustrate present embodiment with reference to Fig. 4, the upper strata cushion from top to bottom includes one layer of rubber
Offset plate 14, two layers weight body sponge 13, one layer of rubber slab 14, one layer of brown pad 18, one layer of rubber slab 14, one layer of weight body sponge 13, two
Layer tarpaulin 16, one layer of weight body sponge 13, one layer of brown pad 18, one layer of weight body sponge 13 and one layer of rubber slab 14；Lower floor's buffering
Layer includes one layer of rubber slab 14, two layers of hard weight body sponge 17, one layer of brown pad 18 and one layer of hard weight body sponge 17.So set
Meter, the distribution mode of each layer can make body after rescue runway is fallen into, the enormous impact force of formation by each layer of rescue runway by
Layer is scattered to be absorbed.Each group stratification in every layer of cushion, such as rubber slab 14, weight body sponge 13, brown pad 18, if being each free
Dry plate block is spliced, and is stitched into one by lash rope, so as to form each group stratification of every layer of cushion.The hard
Weight body sponge 17 is continuous containing the sea of sand, and hardness heavier sponge 13 is big.Other compositions and annexation and the phase of embodiment five
Together.
Embodiment seven：Illustrate to open up fluted 27 on present embodiment, ground with reference to Fig. 1~5, rescue runway 1
And obstruction wall is respectively positioned in groove 27, set in the groove 27 of the rescue surrounding of runway 1 or in the groove 27 of rescue runway 1 both sides
Groove 28 is equipped with, the fire extinguishing system 7 includes some groups of fire extinguishing components, and some described group of fire extinguishing components are distributed on rescue runway 1
Side grooves 28 in, every group of fire extinguishing component include be sequentially connected water circulating pump 20, foam water pot 21, high-pressure hydraulic pump 22 with
And fire extinguishing sprayer 23.It is so designed that, because the number of plies for rescuing runway 1 is more, thickness is larger, and its most of thickness is sunk into underground,
Only stay the thickness line above ground level of fraction to set, prevent when body from force-landing by the stop of the rear end of rescue runway 1, be easy to body to fall
Enter.Water circulating pump 20 can provide cooling water for the circulation of foam water pot 21, and cooling water enters in foam water pot 21 and foams mix
Afterwards, after being extracted by high-pressure hydraulic pump 22, by the pressurization of high-pressure hydraulic pump 22, sprayed by fire extinguishing sprayer 23, when aircraft landing
During, realized by fire extinguishing sprayer 23 and the spray of body is acted on.Other compositions and annexation and embodiment one,
2nd, three, five or six are identical.
Embodiment eight：With reference to the explanation present embodiment of Fig. 1~5, rescue runway 1 bottom and the bottom surface of groove 27 it
Between and stop wall bottom and the bottom surface of groove 27 between be provided with pedestal 19, the front upper of angle of attack runway 4 is provided with two
Observation telescope 9, and two Observation telescopes 9 stop walls 5 respectively close to two sides and set, the Observation telescope 9 and command and control center 6
It is logical.It is so designed that, pedestal 19 is steel construction, Observation telescope 9 can make staff can Real Time Observation in command and control center 6
Situation onto rescue runway 1, to ensure worker safety.Other compositions and annexation and the phase of embodiment seven
Together.
Embodiment nine：Illustrate present embodiment with reference to Fig. 1~5, it is 89m that two sides, which stop the distance between wall 5,
The thickness that each side stops wall 5 is 5m, and the range of tilt angles of angle of attack runway 4 is 0 °~60 °.It is so designed that, rescue runway 1
Overall length × beam overall is 1619m × 99m, and wherein the length of angle of attack runway 4 is 50m, and the length of slope angle runway is 50m.Other compositions
It is identical with embodiment one, two, three, five, six or eight with annexation.
Claims (9)
1. a kind of forced landing buffering rescue runway, it is characterised in that：It includes rescue runway (1), stops wall and fire extinguishing system
(7), the rescue runway (1) is software runway, and the rescue runway (1) includes horizontally disposed primary runway (2), is obliquely installed
Primary runway (2) front end angle of attack runway (4) and be inclined at primary runway (2) rear end slope section runway (3), slope section runway
(3) one end away from primary runway (2) is set less than primary runway (2), and the obstruction wall is that software stops wall, and the obstruction wall includes
The side for being arranged on the preceding obstruction wall (24) of rescue runway (1) front end and being arranged on rescue runway (1) both sides stops wall (5), is located at
High-order angle of attack runway (4) bottom is provided with command and control center (6), and fire extinguishing system (7) is arranged on the two of rescue runway (1)
Sensor is provided with side, rescue runway (1), fire extinguishing system (7) passes through sensor control action.
2. a kind of forced landing buffering rescue runway according to claim 1, it is characterised in that：Each side stops wall (5)
Inner side be provided with some anti-collision barrels (11), it is side by side and perpendicular that some anti-collision barrels (11) stop wall (5) length direction along side
Straight to set, the bottom of anti-collision barrel (11) is positioned by they sup-port, and anti-collision barrel (11) is rubber tube.
3. a kind of forced landing buffering rescue runway according to claim 2, it is characterised in that：Rescue the bottom of runway (1)
The bottom surface that face and side stop wall is generally aligned in the same plane, each side stop be provided between wall (5) and rescue runway (1) position every
Layer (26), the bottom of anti-collision barrel (11) is arranged on the top of positioning interlayer (26) by support bar, wherein, anti-collision barrel (11) and branch
Between strut, between support bar and positioning interlayer (26) or support bar and anti-collision barrel (11) and position between interlayer (26) and be
It is rotatably connected.
4. a kind of forced landing buffering rescue runway according to claim 1,2 or 3, it is characterised in that：On primary runway (2)
Twice buffer subsystem (8) is arranged side by side, the two ends of per pass buffer subsystem (8) are respectively and fixedly connected to the side of both sides and stopped on wall (5).
5. a kind of forced landing buffering rescue runway according to claim 4, it is characterised in that：The rescue runway (1)
Including upper and lower two buffer layer, the hardness of the upper and lower two buffer layer increases successively, is set between upper and lower two buffer layer
There is wire netting (15), the top surface of upper strata cushion is provided with two layers of tarpaulin (16)；It is described to stop four layers that wall includes being arranged side by side
Rubber slab (14) is provided between weight body sponge (13), adjacent heavy two layers body sponge (13)；Forced landing buffering rescue runway is also
Including lash rope (12), the heavy body sponge (13) is stitched into one with rubber slab (14) by lash rope (12).
6. a kind of forced landing buffering rescue runway according to claim 5, it is characterised in that：The upper strata cushion by
It is up to lower to include one layer of rubber slab (14), heavy two layers body sponge (13), one layer of rubber slab (14), one layer of palm fibre pad (18), one layer of rubber
Offset plate (14), one layer of weight body sponge (13), two layers tarpaulin (16), one layer of weight body sponge (13), one layer of palm fibre pad (18), one layer of weight body
Sponge (13) and one layer of rubber slab (14)；Lower floor's cushion includes one layer of rubber slab (14), two layers of hard weight body sponge
(17), one layer of palm fibre pad (18) and one layer of hard weight body sponge (17).
7. a kind of forced landing buffering rescue runway according to claim 1,2,3,5 or 6, it is characterised in that：On ground
Open up fluted (27), rescue runway (1) and obstruction wall are respectively positioned in groove (27), positioned at the groove of rescue runway (1) surrounding
(27) groove (28) is provided with or in the groove (27) of rescue runway (1) both sides, the fire extinguishing system (7) is gone out including some groups
Fiery component, some described group of fire extinguishing components are distributed in the side grooves (28) of rescue runway (1), and every group of fire extinguishing component includes
Water circulating pump (20), foam water pot (21), high-pressure hydraulic pump (22) and the fire extinguishing sprayer (23) being sequentially connected.
8. a kind of forced landing buffering rescue runway according to claim 7, it is characterised in that：Rescue the bottom of runway (1)
Pedestal (19) is provided between portion and groove (27) bottom surface and between the bottom and groove (27) bottom surface of obstruction wall, the angle of attack is run
Road (4) front upper is provided with two Observation telescopes (9), and two Observation telescopes (9) are stopped wall (5) respectively close to two sides and set,
The Observation telescope (9) and command and control center (6) UNICOM.
9. a kind of forced landing buffering rescue runway according to claim 1,2,3,5,6 or 8, it is characterised in that：Two
It is 89m that side, which stops the distance between wall (5), and the thickness that each side stops wall (5) is 5m, the angle of inclination model of angle of attack runway (4)
Enclose for 0 °~60 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710600718.8A CN107190608A (en) | 2017-07-21 | 2017-07-21 | A kind of forced landing buffering rescue runway |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710600718.8A CN107190608A (en) | 2017-07-21 | 2017-07-21 | A kind of forced landing buffering rescue runway |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107190608A true CN107190608A (en) | 2017-09-22 |
Family
ID=59885120
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710600718.8A Withdrawn CN107190608A (en) | 2017-07-21 | 2017-07-21 | A kind of forced landing buffering rescue runway |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107190608A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110217404A (en) * | 2019-06-25 | 2019-09-10 | 纪衍雨 | A kind of safe stake of forced landing interception |
| CN114609962A (en) * | 2022-03-11 | 2022-06-10 | 芜湖市翔装机械设备制造有限公司 | Full-automatic control system and method for airport arresting equipment |
| CN118163955A (en) * | 2024-05-14 | 2024-06-11 | 中国人民解放军海军航空大学 | Runway interception device |
-
2017
- 2017-07-21 CN CN201710600718.8A patent/CN107190608A/en not_active Withdrawn
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110217404A (en) * | 2019-06-25 | 2019-09-10 | 纪衍雨 | A kind of safe stake of forced landing interception |
| CN114609962A (en) * | 2022-03-11 | 2022-06-10 | 芜湖市翔装机械设备制造有限公司 | Full-automatic control system and method for airport arresting equipment |
| CN114609962B (en) * | 2022-03-11 | 2023-12-12 | 芜湖市翔装机械设备制造有限公司 | Full-automatic control system and method for airport arresting equipment |
| CN118163955A (en) * | 2024-05-14 | 2024-06-11 | 中国人民解放军海军航空大学 | Runway interception device |
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Application publication date: 20170922 |