CN105672083A - Airplane snowfield takeoff and landing blanket - Google Patents

Airplane snowfield takeoff and landing blanket Download PDF

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Publication number
CN105672083A
CN105672083A CN201610056224.3A CN201610056224A CN105672083A CN 105672083 A CN105672083 A CN 105672083A CN 201610056224 A CN201610056224 A CN 201610056224A CN 105672083 A CN105672083 A CN 105672083A
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CN
China
Prior art keywords
blanket
snowfield
landing
aircraft
cone
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201610056224.3A
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Chinese (zh)
Inventor
陈小燕
Original Assignee
陈小燕
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by 陈小燕 filed Critical 陈小燕
Priority to CN201610056224.3A priority Critical patent/CN105672083A/en
Publication of CN105672083A publication Critical patent/CN105672083A/en
Pending legal-status Critical Current

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Classifications

    • EFIXED CONSTRUCTIONS
    • E01CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
    • E01CCONSTRUCTION OF, OR SURFACES FOR, ROADS, SPORTS GROUNDS, OR THE LIKE; MACHINES OR AUXILIARY TOOLS FOR CONSTRUCTION OR REPAIR
    • E01C9/00Special pavings; Pavings for special parts of roads or airfields
    • EFIXED CONSTRUCTIONS
    • E01CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
    • E01CCONSTRUCTION OF, OR SURFACES FOR, ROADS, SPORTS GROUNDS, OR THE LIKE; MACHINES OR AUXILIARY TOOLS FOR CONSTRUCTION OR REPAIR
    • E01C9/00Special pavings; Pavings for special parts of roads or airfields
    • E01C9/008Paving take-off areas for vertically starting aircraft

Abstract

The invention discloses an airplane snowfield takeoff and landing blanket. The airplane snowfield takeoff and landing blanket comprises blank substrates and special-shaped conical nails. Each blanket substrate is provided with honeycomb concave pits, connecting sawteeth, countersunk blind holes and through holes. The two blanket substrates are seamlessly spliced through the connecting sawteeth. The special-shaped conical nails are in interference fit with the blanket substrates and fix the blanket substrates to the snowfield or ice field, so that the blanket substrates are prevented from displacing in the horizontal plane. The rapid, safe and efficient scheme is provided for airplane takeoff and landing on the snowfield and ice field, snow covers and ice on airplane runways do not need to be shoveled after snow, and the takeoff and landing blanket is directly laid on the runways and is used for takeoff and landing of airplanes.

Description

A kind of aircraft snowfield takes off landing blanket
Technical field
The present invention relates to aircraft flight apparatus field, be specifically related to a kind of aircraft snowfield and take off landing blanket.
Background technology
At present, changeable weather and the delayed flight that causes happens occasionally, particularly the heavy snow in winter is given and is taken off the inconvenience that landing brings, and often all needs airport is closed, causes a large amount of passenger to be detained. Be on the one hand that aircraft mechanical part is existed certain impact by cold weather, another aspect is frozen covering for runway by accumulated snow, and aircraft cannot normally take off landing; Conventional way is that runway is cleaned by the employing deicing vehicle that clears the snow, but the method inefficiency, needs many and cleans simultaneously, length consuming time and also the deicing vehicle that clears the snow is with high costs.
Summary of the invention
It is an object of the invention to the problem above overcoming prior art to exist, for aircraft snowfield ice landing of taking off a kind of scheme quick, safe and effective is provided, without rooting out accumulated snow on runway and freezing after snow, directly lay and take off landing blanket on runway, for taking off landing.
For realizing above-mentioned technical purpose, reaching above-mentioned technique effect, the present invention is achieved through the following technical solutions:
A kind of aircraft snowfield takes off landing blanket, including blanket matrix, abnormity cone nail, it is characterised in that: described blanket matrix is provided with honeycomb pit, connects sawtooth, countersunk head blind hole and through hole; Described connection sawtooth is by seamless spliced for two pieces of blanket matrixes; Described abnormity cone nail includes the head of a nail, nail rod, step surface and cone; Described abnormity cone nail and blanket matrix interference fit, the head of a nail and the close contact of countersunk head blind hole, nail rod height value is more than blanket matrix thickness value, step surface is slightly larger in dimension than through-hole diameter, step surface, cone traverse through hole, step surface, cone hammer into snowfield or ice ground, blanket matrix are fixed on snowfield or ice ground, it is prevented that the changing of the relative positions in horizontal plane of blanket matrix.
Further, described blanket matrix is nonmetallic materials, non-rigid material, rollable one-tenth web-like.
Further, with high-abrasive material on described honeycomb pit, pit depth, less than 5mm, is shaped as triangle or square or rhombus or regular hexagon.
Further, the described left and right distribution mode connecting sawtooth is staggered arrangement, and countersunk head blind hole is coaxially located at through hole on the axis of symmetry being connected sawtooth, it is to avoid stress is concentrated on the same line.
Further, described cone material is hard metal, is shaped as circular cone or rectangular pyramid or hexagonal pyramid.
Further, described blanket matrix width is more than 1m, more than undercarriage tyre width.
Further, the paving mode of described blanket matrix is that vertical aircraft is sliding to be run direction or lays in the same direction with aircraft sliding race direction.
The invention has the beneficial effects as follows: the present invention is aircraft snowfield ice, and landing of taking off provides a kind of scheme quick, safe and effective, without rooting out accumulated snow on runway and freezing after snow, directly lay and take off landing blanket on runway, utilize abnormity cone nail and blanket matrix interference fit, blanket matrix is fixed on snowfield or ice ground, prevent the changing of the relative positions in horizontal plane of blanket matrix, the honeycomb pit simultaneously originally taken off on landing blanket can increase certain frictional force, make the sliding race process of aircraft steady, thus for aircraft in the landing of taking off of snowfield ice ground.
Described above is only the general introduction of technical solution of the present invention, in order to better understand the technological means of the present invention, and can be practiced according to the content of description, below with presently preferred embodiments of the present invention and coordinate accompanying drawing describe in detail as after. The specific embodiment of the present invention is shown in detail in by following example and accompanying drawing thereof.
Accompanying drawing explanation
Accompanying drawing described herein is used for providing a further understanding of the present invention, constitutes the part of the application, and the schematic description and description of the present invention is used for explaining the present invention, is not intended that inappropriate limitation of the present invention. In the accompanying drawings:
Fig. 1 be aircraft snowfield of the present invention take off landing the seamless spliced schematic diagram of blanket;
Fig. 2 be aircraft snowfield of the present invention take off landing blanket partial schematic diagram;
Fig. 3 is a kind of abnormity cone nail schematic diagram of the present invention;
Number in the figure illustrates: blanket matrix 1, abnormity cone nail 2, honeycomb pit 3, connection sawtooth 4, countersunk head blind hole 5, through hole 6, the head of a nail 21, nail rod 22, step surface 23, cone 24.
Detailed description of the invention
Below with reference to the accompanying drawings and in conjunction with the embodiments, the present invention is described in detail.
With reference to shown in Fig. 1-3, a kind of aircraft snowfield takes off landing blanket, including blanket matrix 1, abnormity cone nail 2, it is characterised in that: described blanket matrix 1 is provided with honeycomb pit 3, connects sawtooth 4, countersunk head blind hole 5 and through hole 6; Described connection sawtooth 4 is by seamless spliced for two pieces of blanket matrixes 1; Described abnormity cone nail 2 includes the head of a nail 21, nail rod 22, step surface 23 and cone 24; Described abnormity cone nail 2 and blanket matrix 1 interference fit, the head of a nail 21 and countersunk head blind hole 5 are in close contact, nail rod 22 height value is more than blanket matrix 1 one-tenth-value thickness 1/10, step surface 23 is slightly larger in dimension than through hole 6 diameter, step surface 23, cone 24 traverse through hole 6, step surface 23, cone 24 hammer into snowfield or ice ground, blanket matrix 1 are fixed on snowfield or ice ground, it is prevented that blanket matrix 1 changing of the relative positions in horizontal plane.
Further, described blanket matrix 1 is nonmetallic materials, non-rigid material, rollable one-tenth web-like. Blanket matrix is divided into 20m, 50m or 100m mono-volume, can manually lay or adopt special laying apparatus car to lay.
Further, with high-abrasive material on described honeycomb pit 3, pit depth, less than 5mm, is shaped as triangle or square or rhombus or regular hexagon. Honeycomb pit 3 simulates straight and even dry ground, for providing a stable frictional force in the sliding race process of aircraft, it is ensured that take off undercarriage smooth ride in descent.
Further, the described left and right distribution mode connecting sawtooth 4 is staggered arrangement, and countersunk head blind hole 5 is coaxially located on the axis of symmetry being connected sawtooth 4 with through hole 6, it is to avoid stress is concentrated on the same line.
Further, described cone 24 material is hard metal, is shaped as circular cone or rectangular pyramid or hexagonal pyramid.Cone 24 penetrates in snowfield ice ground, and after compacting, abnormity cone is connected as a single entity with following closely 2 and snowfield ice.
Further, described blanket matrix 1 width is more than 1m, more than undercarriage tyre width.
Further, the paving mode of described blanket matrix 1 is that vertical aircraft is sliding to be run direction or lays in the same direction with aircraft sliding race direction.
The present invention is aircraft snowfield ice, and landing of taking off provides a kind of scheme quick, safe and effective, without rooting out accumulated snow on runway and freezing after snow, directly lay and take off landing blanket on runway, utilize abnormity cone nail and blanket matrix interference fit, blanket matrix is fixed on snowfield or ice ground, prevent the changing of the relative positions in horizontal plane of blanket matrix, the honeycomb pit simultaneously originally taken off on landing blanket can increase certain frictional force, make the sliding race process of aircraft steady, thus for aircraft in the landing of taking off of snowfield ice ground.
The above, be only presently preferred embodiments of the present invention, and the present invention not does any pro forma restriction; The those of ordinary skill of all industry all can shown in by specification accompanying drawing and the above and implement the present invention swimmingly; But, all those skilled in the art without departing within the scope of technical solution of the present invention, utilize disclosed above technology contents and make a little change, modify and the equivalent variations of differentiation, be the Equivalent embodiments of the present invention; Meanwhile, all change of any equivalent variations, modification and differentiation etc. above example made according to the substantial technological of the present invention, all still fall within the protection domain of technical scheme.

Claims (7)

1. aircraft snowfield takes off a landing blanket, including blanket matrix (1), abnormity cone nail (2), it is characterised in that: described blanket matrix (1) is provided with honeycomb pit (3), connects sawtooth (4), countersunk head blind hole (5) and through hole (6); Described connection sawtooth (4) is by seamless spliced for two pieces of blanket matrixes (1); Described abnormity cone nail (2) includes the head of a nail (21), nail rod (22), step surface (23) and cone (24); Described abnormity cone nail (2) and blanket matrix (1) interference fit, the head of a nail (21) and countersunk head blind hole (5) close contact, nail rod (22) height value is more than blanket matrix (1) one-tenth-value thickness 1/10, step surface (23) is slightly larger in dimension than through hole (6) diameter, step surface (23), cone (24) traverse through hole (6), step surface (23), cone (24) hammer into snowfield or ice ground, blanket matrix (1) are fixed on snowfield or ice ground, it is prevented that blanket matrix (1) changing of the relative positions in horizontal plane.
2. a kind of aircraft snowfield according to claim 1 takes off landing blanket, it is characterised in that: described blanket matrix (1) is nonmetallic materials, non-rigid material, rollable one-tenth web-like.
3. a kind of aircraft snowfield according to claim 2 takes off landing blanket, it is characterised in that: described honeycomb pit (3) is upper with high-abrasive material, and pit depth, less than 5mm, is shaped as triangle or square or rhombus or regular hexagon.
4. a kind of aircraft snowfield according to claim 3 takes off landing blanket, it is characterized in that: the left and right distribution mode of described connection sawtooth (4) is staggered arrangement, countersunk head blind hole (5) is coaxially located on the axis of symmetry being connected sawtooth (4) with through hole (6), it is to avoid stress is concentrated on the same line.
5. a kind of aircraft snowfield according to claim 4 takes off landing blanket, it is characterised in that: described cone (24) material is hard metal, is shaped as circular cone or rectangular pyramid or hexagonal pyramid.
6. a kind of aircraft snowfield according to claim 5 takes off landing blanket, it is characterised in that: described blanket matrix (1) width is more than 1m, more than undercarriage tyre width.
7. a kind of aircraft snowfield according to claim 6 takes off landing blanket, it is characterised in that: the paving mode of described blanket matrix (1) is that vertical aircraft is sliding runs direction or run direction sliding with aircraft is laid in the same direction.
CN201610056224.3A 2016-01-27 2016-01-27 Airplane snowfield takeoff and landing blanket Pending CN105672083A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610056224.3A CN105672083A (en) 2016-01-27 2016-01-27 Airplane snowfield takeoff and landing blanket

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610056224.3A CN105672083A (en) 2016-01-27 2016-01-27 Airplane snowfield takeoff and landing blanket

Publications (1)

Publication Number Publication Date
CN105672083A true CN105672083A (en) 2016-06-15

Family

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Family Applications (1)

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CN201610056224.3A Pending CN105672083A (en) 2016-01-27 2016-01-27 Airplane snowfield takeoff and landing blanket

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Country Link
CN (1) CN105672083A (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2092623U (en) * 1990-12-06 1992-01-08 张仁贵 Self-lock steel nails
CA2312527A1 (en) * 2000-06-27 2001-12-27 Lloyd Knafelc Apparatus for roadways, and the like
CN200985482Y (en) * 2006-12-29 2007-12-05 王元立 Folding anti-skid and anti-trap bridge row
CN102979024A (en) * 2011-09-07 2013-03-20 东营市大生环保生产力促进中心有限公司 An aiding blanket for a wheeled vehicle slipping in a pit
JP2013159998A (en) * 2012-02-07 2013-08-19 Toshin Kogyo Co Ltd Simple covering plate
US20140270945A1 (en) * 2013-03-12 2014-09-18 Reynolds Presto Products Inc. Mat, portable porous construction mat system, tools, and methods
CN204300568U (en) * 2014-10-31 2015-04-29 福建和盛塑业有限公司 Waterproof anti-dropping type bellows joint member

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2092623U (en) * 1990-12-06 1992-01-08 张仁贵 Self-lock steel nails
CA2312527A1 (en) * 2000-06-27 2001-12-27 Lloyd Knafelc Apparatus for roadways, and the like
CN200985482Y (en) * 2006-12-29 2007-12-05 王元立 Folding anti-skid and anti-trap bridge row
CN102979024A (en) * 2011-09-07 2013-03-20 东营市大生环保生产力促进中心有限公司 An aiding blanket for a wheeled vehicle slipping in a pit
JP2013159998A (en) * 2012-02-07 2013-08-19 Toshin Kogyo Co Ltd Simple covering plate
US20140270945A1 (en) * 2013-03-12 2014-09-18 Reynolds Presto Products Inc. Mat, portable porous construction mat system, tools, and methods
CN204300568U (en) * 2014-10-31 2015-04-29 福建和盛塑业有限公司 Waterproof anti-dropping type bellows joint member

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Application publication date: 20160615

RJ01 Rejection of invention patent application after publication