CN110217404A - A kind of safe stake of forced landing interception - Google Patents
A kind of safe stake of forced landing interception Download PDFInfo
- Publication number
- CN110217404A CN110217404A CN201910556216.9A CN201910556216A CN110217404A CN 110217404 A CN110217404 A CN 110217404A CN 201910556216 A CN201910556216 A CN 201910556216A CN 110217404 A CN110217404 A CN 110217404A
- Authority
- CN
- China
- Prior art keywords
- pile body
- layer
- forced landing
- intercepts
- flexible glue
- 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.)
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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—Arresting gear; Liquid barriers
- B64F1/025—Arresting gear; Liquid barriers using decelerating or arresting beds
-
- 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
- B64F1/18—Visual or acoustic landing aids
- B64F1/20—Arrangement of optical beacons
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Piles And Underground Anchors (AREA)
Abstract
The invention discloses a kind of forced landings to intercept safe stake, including preceding pile body, pile body afterwards, pile body gap band, flexible glue layer, concrete fixing layer and pile body frame, the preceding pile body is identical with the rear pile body structure, fixed by pile body frame support, the bottom of the pile body frame is embedded in inside the concrete fixing layer, the flexible glue layer is equipped with above the concrete fixing layer, the pile body lower portion above the flexible glue layer is alternately filled with compression fire proofing firbre cotton layer and shock resistance cellucotton layer, there are gaps to form the pile body gap band between the preceding pile body and the rear pile body, the both sides of the edge part of the compression fire proofing firbre cotton layer and the shock resistance cellucotton layer is embedded with fire plant.Beneficial effect is: scientific, economical and effective can intercept by accident aircraft and safety is force-landed, it is ensured that space flight and the personal safety and safety of property trained.
Description
Technical field
The present invention relates to aviations and military training ground safeguard field, intercept safety more particularly to a kind of forced landing
Stake.
Background technique
Aircraft refers to that the power device with a tool or more tool engines generates the thrust advanced or pulling force, by consolidating for fuselage
Determine wing and generate lift, in the aircraft for overweighting air of endoatmosphere flight, three kinds of sea-freight at present, land transportation and air transportion traffic fortune
Defeated mode greatly facilitates people's lives, and aircraft undoubtedly in all vehicles belong to it is safest, but such as
Fruit once goes wrong, and will will cause extremely serious property, personal damage again, and the survival rate of persons on board is almost nil, special
Be not a certain airspace aircraft break down or it is on fire etc. need ground level emergency to force-land when be difficult success mostly, this be also always with
Come, one of unsolved significant problem in the whole world, it is therefore desirable to which a kind of scientific and effective method solves the problems, such as this.
Summary of the invention
The object of the invention is that it is urgent to provide a kind of aircraft in order to ensure the trained safety forced landing of space flight, military flight
Drop intercepts safe stake.
The present invention through the following technical solutions to achieve the above objectives:
A kind of forced landing intercepts safe stake, including preceding pile body, rear pile body, pile body gap band, flexible glue layer, concrete fixing layer and
Pile body frame, the preceding pile body is identical with the rear pile body structure, is fixed by pile body frame support, the pile body frame
The bottom of frame is embedded in inside the concrete fixing layer, and the flexible glue layer, institute are equipped with above the concrete fixing layer
It states the pile body lower portion above flexible glue layer and is alternately filled with compression fire proofing firbre cotton layer and shock resistance cellucotton layer, it is described
There are gaps to form the pile body gap band between preceding pile body and the rear pile body, and the compression fire proofing firbre cotton layer resists with described
The both sides of the edge part of impact cellucotton layer is embedded with fire plant, is also embedded with and blocks inside the preceding pile body and the rear pile body
Net is cut, the both ends of the intercept net are stretched through steel wire tow line to be fixed.
In order to further increase the performance that forced landing intercepts safe stake, the flexible glue layer with a thickness of 1 meter, the coagulation
Native fixing layer with a thickness of 2 meters, the gap width of the pile body gap band is 8 meters.
In order to further increase the performance that forced landing intercepts safe stake, the interception rope that the intercept net is two centimeters is worked out
It forms.
In order to further increase the performance that forced landing intercepts safe stake, the fire plant is connected with high pressure hose,
The high pressure hose is connected with water source.
In order to further increase the performance that forced landing intercepts safe stake, the intercept net is arranged one every 6 meters, uniformly
It is distributed in the inside of the pile body frame.
In order to further increase the performance that forced landing intercepts safe stake, the side of preceding pile body is provided with impact instruction point,
Being covered with reflective indicateing arm on impact instruction point can be impacted convenient for vector aircraft night and daytime, the top peace of preceding pile body
Safe forced landing is carried out equipped with satellite status device convenient for the big greasy weather.
In above structure, the length of preceding pile body and rear pile body is 200 meters, and width is 80 meters, when aircraft be down to it is liftoff
Start to rush ahead when 50 meters or so of face the impact instruction point of pile body, and when aircraft is stuck in inside pile body, fire plant explosion is opened,
To aircraft and pile body fast cooling, such as because misoperation causes head to rush at ground, flexible glue layer can to difficultly carrying out buffering adjusting,
Avoid casualties caused by impacting compared with great dynamics.
Beneficial effect is: forced landing provided by the present invention intercepts safe stake can be scientific, economical and effective by thing
Therefore aircraft carries out interception and safety forced landing, by being trained on the ground vacant lot in corresponding course line that safety stake is still living and in good health with military flight
In region, it is ensured that the personal safety and safety of property of space flight and training.
Detailed description of the invention
Fig. 1 is the structural schematic diagram that a kind of forced landing of the present invention intercepts safe stake；
Fig. 2 is the intercept net schematic diagram that a kind of forced landing of the present invention intercepts safe stake；
Fig. 3 is the aircraft interception schematic diagram that a kind of forced landing of the present invention intercepts safe stake.
The reference numerals are as follows:
1, preceding pile body；2, rear pile body；3, pile body gap band；4, flexible glue layer；5, concrete fixing layer；6, pile body frame；7, it compresses
Fire proofing firbre cotton layer；8, shock resistance cellucotton layer；9, fire plant；10, impact instruction point；11, steel wire tow line；12, intercept net.
Specific embodiment
In the description of the present invention, it is to be understood that, term " center ", " longitudinal direction ", " transverse direction ", "upper", "lower",
The orientation or positional relationship of the instructions such as "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outside" is
It is based on the orientation or positional relationship shown in the drawings, is merely for convenience of description of the present invention and simplification of the description, rather than instruction or dark
Show that signified device or element must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as pair
Limitation of the invention.In addition, term " first ", " second " etc. are used for description purposes only, it is not understood to indicate or imply phase
To importance or implicitly indicate the quantity of indicated technical characteristic.The feature for defining " first ", " second " etc. as a result, can
To explicitly or implicitly include one or more of the features.In the description of the present invention, unless otherwise indicated, " multiple "
It is meant that two or more.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can
To be mechanical connection, it is also possible to be electrically connected；It can be directly connected, can also can be indirectly connected through an intermediary
Connection inside two elements.For the ordinary skill in the art, above-mentioned term can be understood by concrete condition
Concrete meaning in the present invention.
The present invention will be further explained below with reference to the attached drawings:
As shown in Figure 1-Figure 3, a kind of forced landing intercepts safe stake, including preceding pile body 1, rear pile body 2, pile body gap band 3, flexible glue
Layer 4, concrete fixing layer 5 and pile body frame 6, preceding pile body 1 is identical with rear 2 structure of pile body, solid by the support of pile body frame 6
Fixed, the bottom of pile body frame 6 is embedded in inside concrete fixing layer 5, and the top of concrete fixing layer 5 is equipped with flexible glue layer 4, soft
Alternately filled with compression fire proofing firbre cotton layer 7 and shock resistance cellucotton layer 8, preceding pile body 1 inside the pile body frame 6 of 4 top of glue-line
There are slit-shaped pile body space bands 3 between rear pile body 2, compress the two sides of fire proofing firbre cotton layer 7 and shock resistance cellucotton layer 8
Marginal portion is embedded with fire plant 9, and intercept net 12 is also embedded with inside preceding pile body 1 and rear pile body 2, and the both ends of intercept net 12 are logical
It crosses steel wire tow line 11 and stretches fixation.
In order to further increase the performance that forced landing intercepts safe stake, flexible glue layer 4 with a thickness of 1 meter, concrete is fixed
Layer 5 with a thickness of 2 meters, the gap width of pile body gap band 3 is 8 meters, and intercept net 12 is that two centimeters of interception rope is worked out, and is disappeared
Anti- device 9 is connected with high pressure hose, and the high pressure hose is connected with water source, and intercept net 12 is arranged one every 6 meters, uniformly
It is distributed in the inside of pile body frame 6, the side of preceding pile body 1 is provided with impact instruction point 10, is covered on impact instruction point 10 anti-
Light indicateing arm can be impacted convenient for vector aircraft night and daytime, and the top of preceding pile body 1 is equipped with satellite status device just
Safe forced landing is carried out in the big greasy weather.
In above structure, the length of preceding pile body 1 and rear pile body 2 is 200 meters, and width is 80 meters, when aircraft be down to from
Start to rush ahead when 50 meters or so of ground the impact instruction point 10 of pile body 1, when aircraft is stuck in inside pile body, fire plant explosion
It opens, gives aircraft and pile body fast cooling, such as because misoperation causes head to rush at ground, flexible glue layer 4 can be to difficultly delaying
Section is reconstituted, casualties caused by impacting compared with great dynamics is avoided.
In the present embodiment, the lower of concrete fixing layer 5 can build market place builet below the ground, underground factory, bulk storage plant, country
The Large Undergrounds place such as grain reserves storehouse, entrance are opened up from side.
The basic principles, main features and advantages of the invention have been shown and described above.The technical staff of the industry should
Understand, the present invention is not limited to the above embodiments, and the above embodiments and description only describe originals of the invention
Reason, without departing from the spirit and scope of the present invention, various changes and improvements may be made to the invention, these changes and improvements
It all fall within the protetion scope of the claimed invention.The claimed scope of the invention is by appending claims and equivalents circle
It is fixed.
Claims (6)
1. a kind of forced landing intercepts safe stake, it is characterised in that: including preceding pile body, rear pile body, pile body gap band, flexible glue layer,
Concrete fixing layer and pile body frame, the preceding pile body is identical with the rear pile body structure, is supported by the pile body frame
Fixed, the bottom of the pile body frame is embedded in inside the concrete fixing layer, and the top of the concrete fixing layer is laid with
There is the flexible glue layer, the pile body lower portion above the flexible glue layer is alternately filled with compression fire proofing firbre cotton layer and anti-impact
Cellucotton layer is hit, there are gaps to form the pile body gap band, the compression fire prevention between the preceding pile body and the rear pile body
The both sides of the edge part of cellucotton layer and the shock resistance cellucotton layer is embedded with fire plant, the preceding pile body and the rear stake
Internal portion is also embedded with intercept net, and the both ends of the intercept net are stretched through steel wire tow line to be fixed.
2. a kind of forced landing according to claim 1 intercepts safe stake, it is characterised in that: the flexible glue layer with a thickness of
1 meter, the concrete fixing layer with a thickness of 2 meters, the gap width of the pile body gap band is 8 meters.
3. a kind of forced landing according to claim 1 intercepts safe stake, it is characterised in that: the intercept net is two centimeters
Interception rope work out.
4. a kind of forced landing according to claim 1 intercepts safe stake, it is characterised in that: the fire plant is connected with
High pressure hose, the high pressure hose are connected with water source.
5. a kind of forced landing according to claim 1 intercepts safe stake, it is characterised in that: the intercept net is every 6 meters
Setting one, is evenly distributed on the inside of the pile body frame.
6. a kind of forced landing according to claim 1 intercepts safe stake, it is characterised in that: the side of preceding pile body is provided with
Impact instruction point, impact indicates that reflective indicateing arm is covered on point can be impacted convenient for vector aircraft night and daytime, preceding
Satellite status device is installed at the top of pile body and carries out safe forced landing convenient for the big greasy weather.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910556216.9A CN110217404A (en) | 2019-06-25 | 2019-06-25 | A kind of safe stake of forced landing interception |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910556216.9A CN110217404A (en) | 2019-06-25 | 2019-06-25 | A kind of safe stake of forced landing interception |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110217404A true CN110217404A (en) | 2019-09-10 |
Family
ID=67814857
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910556216.9A Withdrawn CN110217404A (en) | 2019-06-25 | 2019-06-25 | A kind of safe stake of forced landing interception |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110217404A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20050129903A1 (en) * | 2003-11-12 | 2005-06-16 | Carr Patrick J. | Synthetic runway surface system |
| US20060018711A1 (en) * | 2004-07-21 | 2006-01-26 | Rogers Marvel Architects, Pllc | Vehicle barrier system |
| US20090189016A1 (en) * | 2008-01-25 | 2009-07-30 | Insitu, Inc. | Systems and methods for recovering and controlling post-recovery motion of unmanned aircraft |
| CN107190608A (en) * | 2017-07-21 | 2017-09-22 | 黄诚 | A kind of forced landing buffering rescue runway |
| CN107354835A (en) * | 2017-09-04 | 2017-11-17 | 黄诚 | A kind of forced landing buffering rescue runway |
| CN108560353A (en) * | 2018-04-25 | 2018-09-21 | 李金华 | A kind of airplane emergency forced landing runway and its method of construction |
| WO2018222551A1 (en) * | 2017-05-31 | 2018-12-06 | Insitu, Inc. | Systems and methods for capturing and recovering unmanned aircraft |
-
2019
- 2019-06-25 CN CN201910556216.9A patent/CN110217404A/en not_active Withdrawn
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20050129903A1 (en) * | 2003-11-12 | 2005-06-16 | Carr Patrick J. | Synthetic runway surface system |
| US20060018711A1 (en) * | 2004-07-21 | 2006-01-26 | Rogers Marvel Architects, Pllc | Vehicle barrier system |
| US20090189016A1 (en) * | 2008-01-25 | 2009-07-30 | Insitu, Inc. | Systems and methods for recovering and controlling post-recovery motion of unmanned aircraft |
| WO2018222551A1 (en) * | 2017-05-31 | 2018-12-06 | Insitu, Inc. | Systems and methods for capturing and recovering unmanned aircraft |
| CN107190608A (en) * | 2017-07-21 | 2017-09-22 | 黄诚 | A kind of forced landing buffering rescue runway |
| CN107354835A (en) * | 2017-09-04 | 2017-11-17 | 黄诚 | A kind of forced landing buffering rescue runway |
| CN108560353A (en) * | 2018-04-25 | 2018-09-21 | 李金华 | A kind of airplane emergency forced landing runway and its method of construction |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190910 |
|
| WW01 | Invention patent application withdrawn after publication |