CN105507107A - Antiskid layer carpet for airplane to take off and land on snow land - Google Patents
Antiskid layer carpet for airplane to take off and land on snow land Download PDFInfo
- Publication number
- CN105507107A CN105507107A CN201610056266.7A CN201610056266A CN105507107A CN 105507107 A CN105507107 A CN 105507107A CN 201610056266 A CN201610056266 A CN 201610056266A CN 105507107 A CN105507107 A CN 105507107A
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- CN
- China
- Prior art keywords
- blanket
- carpet
- matrix
- land
- blanket body
- 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
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- 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
- E01C9/08—Temporary pavings
Abstract
The invention discloses an antiskid layer carpet for an airplane to take off and land on a snow land. The carpet comprises carpet base bodies and a special-shaped conical screw. Each carpet base body is provided with antiskid protections, connecting sawteeth, countersunk head blind holes, through holes, an upper layer carpet body and a lower layer carpet body. The two carpet base bodies are limited and spliced seamlessly through the upper layer carpet bodies, the lower layer carpet bodies and the connecting sawteeth. The special-shaped conical screw is in interference fit with the carpet base bodies and fixes the two adjacent carpet base bodies to the snow land or an ice land after penetrating through the upper layer carpet bodies and the lower layer carpet bodies so that the carpet base bodies can be prevented from being staggered in the horizontal plane. Meanwhile, by means of the antiskid protrusions of the carpet, certain friction force can be added, tires of an undercarriage are prevented from sliding, and the ground sliding process of the airplane is stable. A rapid, safe and effective scheme is provided for the airplane to take off and land on the snow land or the ice land; accumulated snow and ice on an airplane runway do not need to be removed after snow, and the carpet is directly laid on the runway so that the airplane can take off and land on the carpet.
Description
Technical field
The present invention relates to aircraft flight apparatus field, be specifically related to a kind of aircraft snowfield and rise and fall skid resistant course blanket.
Background technology
At present, changeable weather and the delayed flight that causes happens occasionally, particularly the heavy snow in winter is to taking off the inconvenience of landing and bringing, and often all needs to close airport, causes a large amount of passenger to be detained.On the one hand there is certain influence for cold weather to aircraft mechanical part, another aspect is frozen covering for runway by accumulated snow, and aircraft cannot normally take off landing; Conventional way is that the employing deicing vehicle that clears the snow cleans runway, but the method inefficiency, needs many and cleans simultaneously, length consuming time and also the deicing vehicle that clears the snow with high costs.
Summary of the invention
The object of the invention is to the above problem overcoming prior art existence, for aircraft snowfield ice landing of taking off a kind of quick, safe and effective scheme is provided, without the need to rooting out accumulated snow on runway and freezing after snow, direct laying takes off landing blanket on runway, for taking off landing.
For realizing above-mentioned technical purpose, reach above-mentioned technique effect, the present invention is achieved through the following technical solutions:
A kind of aircraft snowfield rises and falls skid resistant course blanket, comprises blanket matrix, abnormity cone nail, it is characterized in that: described blanket matrix is provided with anti-skidding projection, connects sawtooth, countersunk head blind hole, through hole, upper strata blanket body and lower floor's blanket body; With high-abrasive material in described anti-skidding projection, height of projection is less than 5mm, and shape is " people " font, and " people " font tip is oriented to be taken off or dropping motion direction, plays and prevents gear tyre skidding effect; Described upper strata blanket body and lower floor's blanket body lay respectively at the side, left and right of blanket matrix; Described upper strata blanket body is provided with countersunk head blind hole, through hole, and lower floor's blanket body is provided with through hole, and the height sum of upper strata blanket body and lower floor's blanket body equals blanket matrix thickness, and upper strata blanket body and lower floor's blanket body cooperatively interact, and limits relative position between two pieces of blanket matrixes; Described connection sawtooth lays respectively at on lower floor blanket body below the blanket body of upper strata, by seamless spliced for two pieces of blanket matrixes; Described abnormity cone nail comprises the head of a nail, nail bar, step surface and the conical surface; Described abnormity cone nail and blanket matrix interference fit, the head of a nail and countersunk head blind hole close contact, nail bar height value is greater than blanket matrix thickness value, step surface size is slightly larger than through-hole diameter, step surface, the conical surface are through blanket matrix or successively through upper strata blanket body and lower floor's blanket body, step surface, the conical surface hammer into snowfield or ice ground, blanket matrix are fixed on snowfield or ice ground, prevent the changing of the relative positions in horizontal plane of blanket matrix.
Further, described blanket matrix is nonmetals, non-rigid material, rollable one-tenth web-like.
Further, the left and right distribution mode of described connection sawtooth is staggered arrangement, and countersunk head blind hole and through hole are coaxially positioned at and are connected on the axis of symmetry of sawtooth, avoids stressed concentrating on the same line.
Further, described conical surface material is hard metal, and shape is circular cone or rectangular pyramid or hexagonal pyramid; The described conical surface is provided with bocca, and the quantity of bocca is two or two or more, is evenly distributed on the conical surface top of the conical surface, increases the contact area of nail.
Further, described blanket matrix width is greater than 1m, is greater than undercarriage tyre width.
The invention has the beneficial effects as follows: landing of taking off that the present invention is aircraft snowfield ice provides a kind of quick, safe and effective scheme, without the need to rooting out accumulated snow on runway and freezing after snow, direct laying takes off landing blanket on runway, utilize abnormity cone nail and blanket matrix interference fit, blanket matrix is fixed on snowfield or ice ground, prevents the changing of the relative positions in horizontal plane of blanket matrix; And utilize connection sawtooth, upper strata blanket body and lower floor's blanket body by spacing for blanket matrix seamless link, the anti-skidding projection of simultaneously originally taking off on landing blanket can increase certain frictional force, prevent gear tyre from skidding, make the sliding race process of aircraft steady, thus for aircraft in the landing of taking off of snowfield ice ground.
Above-mentioned explanation is only the general introduction of technical solution of the present invention, in order to better understand technological means of the present invention, and can be implemented according to the content of manual, coordinates accompanying drawing to be described in detail as follows below with preferred embodiment of the present invention.The specific embodiment of the present invention is provided in detail by following examples and accompanying drawing thereof.
Accompanying drawing explanation
Accompanying drawing described herein is used to provide a further understanding of the present invention, and form a application's part, schematic description and description of the present invention, for explaining the present invention, does not form inappropriate limitation of the present invention.In the accompanying drawings:
Fig. 1 is that aircraft snowfield of the present invention rises and falls the seamless spliced schematic diagram of skid resistant course blanket;
Fig. 2 is that aircraft snowfield of the present invention rises and falls skid resistant course blanket top schematic diagram;
Fig. 3 is that aircraft snowfield of the present invention rises and falls skid resistant course blanket bottom schematic view;
Fig. 4 is that aircraft snowfield of the present invention rises and falls skid resistant course blanket direction of motion schematic diagram;
Fig. 5 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, anti-skidding protruding 3, connect sawtooth 4, countersunk head blind hole 5, through hole 6, upper strata blanket body 7, lower floor's blanket body 8, the head of a nail 21, nail bar 22, step surface 23, the conical surface 24, bocca 25.
Detailed description of the invention
Below with reference to the accompanying drawings and in conjunction with the embodiments, describe the present invention in detail.
With reference to shown in Fig. 1-5, a kind of aircraft snowfield rises and falls skid resistant course blanket, comprises blanket matrix 1, abnormity cone nail 2, it is characterized in that: described blanket matrix 1 be provided with anti-skidding protruding 3, connect sawtooth 4, countersunk head blind hole 5, through hole 6, upper strata blanket body 7 and lower floor's blanket body 8; With high-abrasive material on described anti-skidding protruding 3, height of projection is less than 5mm, and shape is " people " font, and " people " font tip is oriented to be taken off or dropping motion direction, plays and prevents gear tyre skidding effect; Described upper strata blanket body 7 and lower floor's blanket body 8 lay respectively at the side, left and right of blanket matrix 1; Described upper strata blanket body 7 is provided with countersunk head blind hole 5, through hole 6, lower floor's blanket body 8 is provided with through hole 6, upper strata blanket body 7 equals blanket matrix 1 thickness with the height sum of lower floor's blanket body 8, and upper strata blanket body 7 and lower floor's blanket body 8 cooperatively interact, and limit relative position between two pieces of blanket matrixes 1; Described connection sawtooth 4 lays respectively at on lower floor blanket body 8 below upper strata blanket body 7, by seamless spliced for two pieces of blanket matrixes 1; Described abnormity cone nail 2 comprises the head of a nail 21, nail bar 22, step surface 23 and the conical surface 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 bar 22 height value is greater than blanket matrix 1 one-tenth-value thickness 1/10, step surface 23 size is slightly larger than through hole 6 diameter, step surface 23, the conical surface 24 are through blanket matrix 1 or successively through upper strata blanket body 7 and lower floor's blanket body 8, step surface 23, the conical surface 24 hammer into snowfield or ice ground, blanket matrix 1 are fixed on snowfield or ice ground, prevent blanket matrix 1 changing of the relative positions in horizontal plane.The straight and even dry ground of anti-skidding protruding 3 simulation, for providing a stable frictional force in the sliding race process of aircraft, guarantees to take off undercarriage smooth ride in descent.
Further, described blanket matrix 1 is nonmetals, 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, the left and right distribution mode of described connection sawtooth 4 is staggered arrangement, countersunk head blind hole 5 and through hole 6 be coaxially positioned at be connected sawtooth 4 the axis of symmetry on, avoid stressed concentrate on the same line.
Further, the described conical surface 24 material is hard metal, and shape is circular cone or rectangular pyramid or hexagonal pyramid; The described conical surface 24 is provided with bocca 25, and the quantity of bocca 25 is two or two or more, is evenly distributed on the conical surface top of the conical surface 24, increases the contact area of nail.The conical surface 24 penetrates in snowfield ice ground, and after compacting, abnormity is connected as a single entity with boring nail 2 and snowfield ice.
Further, described blanket matrix 1 width is greater than 1m, is greater than undercarriage tyre width.
Landing of taking off that the present invention is aircraft snowfield ice provides a kind of quick, safe and effective scheme, without the need to rooting out accumulated snow on runway and freezing after snow, direct laying takes off landing blanket on runway, utilize abnormity cone nail and blanket matrix interference fit, blanket matrix is fixed on snowfield or ice ground, prevents the changing of the relative positions in horizontal plane of blanket matrix; And utilize connection sawtooth, upper strata blanket body and lower floor's blanket body by spacing for blanket matrix seamless link, the anti-skidding projection of simultaneously originally taking off on landing blanket can increase certain frictional force, prevent gear tyre from skidding, 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 preferred embodiment of the present invention, not does any pro forma restriction to the present invention; 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 are not departing within the scope of technical solution of the present invention, utilize disclosed above technology contents and make a little change, modify with differentiation equivalent variations, be Equivalent embodiments of the present invention; Meanwhile, all according to substantial technological of the present invention to the change of any equivalent variations that above embodiment is done, modify and differentiation etc., within the protection domain all still belonging to technical scheme of the present invention.
Claims (5)
1. an aircraft snowfield rises and falls skid resistant course blanket, comprise blanket matrix (1), abnormity cone nail (2), it is characterized in that: described blanket matrix (1) is provided with anti-skidding projection (3), connects sawtooth (4), countersunk head blind hole (5), through hole (6), upper strata blanket body (7) and lower floor's blanket body (8); Described anti-skidding projection (3) is upper with high-abrasive material, and height of projection is less than 5mm, and shape is " people " font, and " people " font tip is oriented to be taken off or dropping motion direction, plays and prevents gear tyre skidding effect; Described upper strata blanket body (7) and lower floor's blanket body (8) lay respectively at the side, left and right of blanket matrix (1); Described upper strata blanket body (7) is provided with countersunk head blind hole (5), through hole (6), lower floor's blanket body (8) is provided with through hole (6), upper strata blanket body (7) equals blanket matrix (1) thickness with the height sum of lower floor's blanket body (8), upper strata blanket body (7) and lower floor's blanket body (8) cooperatively interact, and limit relative position between two pieces of blanket matrixes (1); Described connection sawtooth (4) lays respectively at below, upper strata blanket body (7) with in lower floor's blanket body (8), by seamless spliced for two pieces of blanket matrixes (1); Described abnormity cone nail (2) comprises the head of a nail (21), nail bar (22), step surface (23) and the conical surface (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 bar (22) height value is greater than blanket matrix (1) one-tenth-value thickness 1/10, step surface (23) size is slightly larger than through hole (6) diameter, step surface (23), the conical surface (24) are through blanket matrix (1) or successively through upper strata blanket body (7) and lower floor's blanket body (8), step surface (23), the conical surface (24) hammer into snowfield or ice ground, blanket matrix (1) is fixed on snowfield or ice ground, prevents blanket matrix (1) changing of the relative positions in horizontal plane.
2. a kind of aircraft snowfield according to claim 1 rises and falls skid resistant course blanket, it is characterized in that: described blanket matrix (1) is nonmetals, non-rigid material, rollable one-tenth web-like.
3. a kind of aircraft snowfield according to claim 2 rises and falls skid resistant course 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) and through hole (6) be coaxially positioned at be connected sawtooth (4) the axis of symmetry on, avoid stressed concentrate on the same line.
4. a kind of aircraft snowfield according to claim 3 rises and falls skid resistant course blanket, it is characterized in that: the described conical surface (24) material is hard metal, and shape is circular cone or rectangular pyramid or hexagonal pyramid; The described conical surface (24) is provided with bocca (25), and the quantity of bocca (25) is two or two or more, is evenly distributed on the conical surface top of the conical surface (24), increases the contact area of nail.
5. a kind of aircraft snowfield according to claim 4 rises and falls skid resistant course blanket, it is characterized in that: described blanket matrix (1) width is greater than 1m, is greater than undercarriage tyre width.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610056266.7A CN105507107A (en) | 2016-01-27 | 2016-01-27 | Antiskid layer carpet for airplane to take off and land on snow land |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610056266.7A CN105507107A (en) | 2016-01-27 | 2016-01-27 | Antiskid layer carpet for airplane to take off and land on snow land |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105507107A true CN105507107A (en) | 2016-04-20 |
Family
ID=55715386
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610056266.7A Pending CN105507107A (en) | 2016-01-27 | 2016-01-27 | Antiskid layer carpet for airplane to take off and land on snow land |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105507107A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106939708A (en) * | 2017-04-10 | 2017-07-11 | 刘阳 | A kind of compound airport with many airplane parking areas and shutdown boarding methods |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN87203910U (en) * | 1987-03-18 | 1987-12-26 | 鲁伟 | Antiskid device for walking ice-snow surface |
| CN2092623U (en) * | 1990-12-06 | 1992-01-08 | 张仁贵 | Self-lock steel nails |
| GB2433539A (en) * | 2005-12-23 | 2007-06-27 | Woodpath Ventures Ltd | Mat for use in temporary road, scaffolding and the like |
| CN201409779Y (en) * | 2009-06-04 | 2010-02-24 | 广西福园剑麻股份有限公司 | Splicing sisal carpet |
| CN202055141U (en) * | 2011-04-20 | 2011-11-30 | 俞威 | Electric heating snow removing plate |
| CN202323607U (en) * | 2011-11-14 | 2012-07-11 | 苏州市广卫特种水泥制品有限公司 | Paving plate |
| KR20130047094A (en) * | 2011-10-31 | 2013-05-08 | 임선우 | Overspeed protection road block |
| CN204023353U (en) * | 2014-06-03 | 2014-12-17 | 王义高 | Deicing or snow melting rubber electric blanket |
| CN204683268U (en) * | 2015-06-10 | 2015-10-07 | 安吉县欧义竹木制品有限公司 | A kind of seamed rug |
-
2016
- 2016-01-27 CN CN201610056266.7A patent/CN105507107A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN87203910U (en) * | 1987-03-18 | 1987-12-26 | 鲁伟 | Antiskid device for walking ice-snow surface |
| CN2092623U (en) * | 1990-12-06 | 1992-01-08 | 张仁贵 | Self-lock steel nails |
| GB2433539A (en) * | 2005-12-23 | 2007-06-27 | Woodpath Ventures Ltd | Mat for use in temporary road, scaffolding and the like |
| CN201409779Y (en) * | 2009-06-04 | 2010-02-24 | 广西福园剑麻股份有限公司 | Splicing sisal carpet |
| CN202055141U (en) * | 2011-04-20 | 2011-11-30 | 俞威 | Electric heating snow removing plate |
| KR20130047094A (en) * | 2011-10-31 | 2013-05-08 | 임선우 | Overspeed protection road block |
| CN202323607U (en) * | 2011-11-14 | 2012-07-11 | 苏州市广卫特种水泥制品有限公司 | Paving plate |
| CN204023353U (en) * | 2014-06-03 | 2014-12-17 | 王义高 | Deicing or snow melting rubber electric blanket |
| CN204683268U (en) * | 2015-06-10 | 2015-10-07 | 安吉县欧义竹木制品有限公司 | A kind of seamed rug |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106939708A (en) * | 2017-04-10 | 2017-07-11 | 刘阳 | A kind of compound airport with many airplane parking areas and shutdown boarding methods |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20160420 |