CN1966351A - Aerostat cold-proof dust-proof clothes - Google Patents
Aerostat cold-proof dust-proof clothes Download PDFInfo
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- CN1966351A CN1966351A CNA200610145469XA CN200610145469A CN1966351A CN 1966351 A CN1966351 A CN 1966351A CN A200610145469X A CNA200610145469X A CN A200610145469XA CN 200610145469 A CN200610145469 A CN 200610145469A CN 1966351 A CN1966351 A CN 1966351A
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Abstract
The invention relates to an anti-cold dustproof clothes of aircraft, wherein its production comprises that: (1), producing large wing anti-cold dustproof clothes that sizing the material based on the size of large wing, movably connecting each sections at edges; arranging fixing line at the connected part; at two longitudinal sides and outer edge, passing lead line through; arranging connecting line at the inner edge and connecting line transversely; (2), producing horizontal wing anti-cold dustproof clothes that sizing material based on horizontal wing, connecting sections at edges, arranging fixing line longitudinally at connected part, passing lead lines at two longitudinal side edges and connecting lines transversely; (3), producing engine anti-cold dustproof clothes that sizing material based on engine size, connecting each part, the edge of open contains closing line. The invention has simple production and low cost, without pollution.
Description
[technical field]
The present invention relates to a kind of aerocraft cold-proof dust-proof device, particularly relate to a kind of aerostat cold-proof dust-proof clothes.
[background technology]
For aircraft industry, the safety of flight is important to seeing, and must put in the first place.How to reach real safety, at first should consider from the angle of protection.Here said protection is promptly to the big wing of aerocraft, the exterior protection of horizontal tail and driving engine.Because these positions are exposed in the open, often have dust, through regular meeting because of ponding frost, freeze.These all can jeopardize flight safety.
At present, the de-icing method that aircraft industry adopted is to use the deicing special vehicle, with a type deicing liquid, sprays each position of aircraft.Waste of manpower like this, material resources and consuming time.With a Boeing-737 is example, purchases a special use and removes 1,800,000 yuan in ice machine behaviour people coin, and the personal services calculated by man-hour, needed with a large amount of water in ice detachment simultaneously, and deicing liquid has also caused pollution to environment.And, under the low situation of temperature, can freeze once more immediately.
[summary of the invention]
Task of the present invention provides a kind of aerostat cold-proof dust-proof clothes, has solved the dustproof of aerocraft and because of preventing ponding frost, icing problem.And processing is simple, and cost is low, and is easy to use.
Technical scheme of the present invention is for to cut out material therefor according to the size of big wing, horizontal tail and driving engine, each several part is flexibly connected, vertically be provided with reinforcing cord in the junction, the big vertical both sides of the edge of wing cold-proof dust-proof clothes reach in the outer section edge runs through plumbous rope, reaches in inner segment edge and laterally is provided with connection cord; Run through plumbous rope in the vertical both sides of the edge of horizontal tail cold-proof dust-proof clothes, laterally be provided with connection cord simultaneously; For the driving engine cold-proof dust-proof clothes, the rope that closes up is housed in its opening part edge.
The invention has the beneficial effects as follows and make simply, uses very conveniently that after processing according to this job operation, put and get final product, cost is extremely low.Actv. has solved aerocraft because of ponding frost, icing and dust protection problem, and environment is not polluted, and has saved great amount of manpower and material resources and time, and actv. has guaranteed flight safety simultaneously.
[description of drawings]
Fig. 1 is the right big wing cold-proof dust-proof clothes dimension figure of Boeing-737.
Fig. 2 is the big wing cold-proof dust-proof clothes dimension figure in a Boeing-737 left side.
Fig. 3 is the right horizontal tail cold-proof dust-proof clothes of a Boeing-737 dimension figure.
Fig. 4 is a Boeing-737 left side horizontal tail cold-proof dust-proof clothes dimension figure.
Fig. 5 is the double buckle connection diagram.
Fig. 6 is a double buckle junction reinforcing cord connection diagram.
Fig. 7 is left horizontal tail cold-proof dust-proof clothes connection cord and reinforcing cord scheme drawing.
Fig. 8 is right horizontal tail cold-proof dust-proof clothes connection cord and reinforcing cord scheme drawing.
Fig. 9 is right big wing cold-proof dust-proof clothes connection cord and reinforcing cord scheme drawing
Figure 10 is big wing cold-proof dust-proof clothes connection cord in a left side and reinforcing cord scheme drawing
Figure 11 is a connection diagram at the bottom of the connection cord abdomen.
Figure 12 is the plumbous rope of a driving engine running-on scheme drawing.
Figure 13 is for using aerocraft of the present invention position scheme drawing.
Figure 14 is a Boeing-737 type engine section cold-proof dust-proof clothes dimension figure.
Figure 15 runs through scheme drawing for plumbous rope.
[specific embodiment]
Fig. 1 is the right big wing cold-proof dust-proof clothes dimension figure of Boeing-737, and wherein 1 is the outer section of wing, and 2 is the wing stage casing, and 3 is the wing inner segment; Fig. 2 is the big wing cold-proof dust-proof clothes dimension figure in a Boeing-737 left side, and wherein 4 is the outer section of wing, and 5 is the wing stage casing, and 6 is the wing inner segment; Fig. 3 is the right horizontal tail cold-proof dust-proof clothes of a Boeing-737 dimension figure, and wherein 7 is the outer section of wing, and 8 is the wing inner segment; Fig. 4 is a Boeing-737 left side horizontal tail cold-proof dust-proof clothes dimension figure, and wherein 9 is the outer section of wing, and 10 is the wing inner segment; Fig. 5 is the double buckle connection diagram, and wherein 11 is the outer section of wing, and 12 is the wing inner segment, and 13 are button, and 14 is the son button; Fig. 6 is a double buckle junction reinforcing cord connection diagram, and wherein 15 is reinforcing cord; Fig. 7 is left horizontal tail cold-proof dust-proof clothes connection cord and reinforcing cord scheme drawing, and wherein 16 is connection cord, and 17 is reinforcing cord; Fig. 8 is right horizontal tail cold-proof dust-proof clothes connection cord and reinforcing cord scheme drawing, and wherein 18 is connection cord, and 19 is reinforcing cord; Fig. 9 is right big wing cold-proof dust-proof clothes connection cord and reinforcing cord scheme drawing, and wherein 20 is connection cord, and 21 is reinforcing cord; Figure 10 is big wing cold-proof dust-proof clothes connection cord in a left side and reinforcing cord scheme drawing, and wherein 22 is connection cord, and 23 is reinforcing cord; Fig. 1 is a connection diagram at the bottom of the connection cord abdomen, and wherein 24 is connection cord; Figure 12 is the plumbous rope of a driving engine running-on scheme drawing, and wherein 25 is plumbous rope; Figure 13 is for using aerocraft of the present invention position scheme drawing, and wherein 26 be right big wing section, and 27 is 6 to be left side wing section greatly, and 28 is right horizontal tail, and 29 is left horizontal tail, and 30 is engine section; Figure 14 is a Boeing-737 type cold-proof dust-proof clothes dimension figure, and Figure 15 runs through scheme drawing for plumbous rope, and wherein 31 is plumbous rope.
Big wing section cold-proof dust-proof clothes: with material therefor according to big wing interior, in, an outer section size cuts out, and each section in edge's flexible connection, vertically is provided with reinforcing cord in the junction; Outside reaching, vertical both sides of the edge of described big wing section cold-proof dust-proof clothes run through plumbous rope in the section edge, edge is provided with connection cord at inner segment, simultaneously laterally be provided with connection cord, the connection cord that laterally is provided with is no less than 50cm in the length with the overlapping part of wing section.
Horizontal tail part cold-proof dust-proof clothes: material therefor is cut out according to inside and outside section size of horizontal tail, each section flexibly connected in edge, vertically be provided with reinforcing cord in the junction; Run through plumbous rope in vertical both sides of the edge of described horizontal tail part cold-proof dust-proof clothes, laterally be provided with connection cord simultaneously, the connection cord that laterally is provided with is no less than 50cm in the length with the overlapping part of wing section.
Engine section cold-proof dust-proof clothes: material therefor is cut out according to the size of driving engine, each several part is sewed up, the rope that closes up is housed in its opening part edge.
Use preferred cloth when making, light, wear-resisting, toughness, softness are not decreased aerocraft, the easily preservation that do not absorb water, but repeated use, and used life can reach more than 2 years; Used reinforcing cord, the connection cord and the rope that closes up are common rope; Used lead rope is more than the 80 gram/rice; Used flexible connection is the double buckle connection mode, does not damage the outside face of aerocraft like this, connect each section with double buckle after, the reinforcing cord that will be located at the vertical both sides of double buckle is again fastened.Reinforcing cord mainly plays the effect that prevents that double buckle is pullled by external force to come off.The lead rope of both sides mainly plays extra heavy effect, like this can be windproof.
During use if with each big wing interior, in, outer section is (as Fig. 1,2) and inside and outside section of each horizontal tail (as Fig. 3,4) connect (as Fig. 5) with double buckle, again each reinforcing cord is fastened, again cold-proof dust-proof clothes is enclosed within on big wing and the horizontal tail, the connection cord (as Fig. 7-10) of both sides is fastened at the bottom of the wing abdomen got final product again.
The overcoat of driving engine (as Figure 12) needs only from the head of driving engine and packs into, and mouth is tied to get final product then.
Concrete method for making is existing to be example with the Boeing-737 type, and the method for making of other type is identical, just the size difference.
(1) concrete grammar of the big wing section of making cold-proof dust-proof clothes:
(a) inner segment: cut out the cloth of specification shown in Fig. 1 inner segment well earlier, the limit of 2.5cm on the car of the position of 7.5m strong point, be used to run through connection cord, double buckle (is also referred to as sticking belt on getting on the bus on the long limit of 5.3m, the magic button) the child button in, detain longitudinally three road reinforcing cords on the cloth truck at son, be used to reinforce double buckle; Locate the limit of 2.5cm on the difference car in the both sides of cloth (4.4m is with 4.9m), be used to run through plumbous rope, plumbous rope plays windproof effect of scraping; Twice connection cord on getting on the bus in the position of both sides again, connection cord is no less than 50cm in the length with wing cloth lap partly;
(b) stage casing: cutting out a block specifications earlier is the cloth of 5.3m * 3m, (as stage casing among Fig. 1), box is respectively sewed at two at cloth, the position of box must be with interior, the child button correspondence of outer section, at vertical three road reinforcing cords on the car on the cloth of the position of box, the position of rope must be respectively with interior, and the reinforcing cord of outer section is corresponding; The limit of 2.5cm is used to run through plumbous rope on the difference car of the both sides of cloth, twice connection cord on each car of the both sides of lead rope position, and connection cord is no less than 50cm in the length with wing cloth lap partly;
(c) outer section: cut out the cloth of good outer section specification as shown in Figure 1 earlier, the limit of one 2.5cm is used to run through plumbous rope on minimum edge (position that 2.2m is long) car, and the limit of 2.5cm is used to run through plumbous rope on the car of the both sides (position that 9.8m and 10.8m are long) of cloth; Four road connection cords on the horizontal car in the position of cloth both sides again, connection cord is no less than 50cm in the length with the lap of wing cloth part; Son button on the wide position car of cloth 5.3m, the position of son button must be corresponding with the stage casing box; Three road reinforcing cords on the car again, the position of reinforcing cord must be corresponding with the stage casing reinforcing cord.
(2) make cold-proof dust-proof clothes horizontal tail concrete grammar partly
(a) inner segment: cut out the cloth that specification is 5.3m * 1m earlier, the limit of one 2.5cm on the sidecar that 5.3m is long is used to run through plumbous rope, and son is buckled three road reinforcing cords on vertical car of child button on another sidecar; The limit of one 2.5cm on each car of the both sides of cloth (position that 1m is wide) is used to run through plumbous rope;
(b) outer section: the cloth of cutting out good outer section specification as shown in Figure 3 earlier, locate the limit of one 2.5cm on the car in minimum position (1.5m) on one side, be used to run through plumbous rope, locate the limit of 2.5cm on the car at cloth both sides (7m is with 8m), be used to run through plumbous rope, three road connection cords on this two sidecar, connection cord is no less than 50cm in the length with wing cloth lap partly; Box on the car of the position of 5.3m, at vertical three road reinforcing cords on the car again, the position of reinforcing cord must be corresponding with the reinforcing cord of inner segment.
(3) concrete grammar of production cold-proof dust-proof clothes engine section: cut out the circular cloth that diameter is 2.3m earlier, cut out the cloth of a 7.2m * 3.4m again, splice mutually the position that the girth of circular cloth and the 7.2m among 7.2m * 3.4m is long, again the 3.4m among 7.2m * 3.4m is sewed up mutually, with the limit that one 2.5cm sewed in the position on the mouth, the lead rope is run through wherein getting final product then.
Claims (5)
1. aerostat cold-proof dust-proof clothes is characterized in that:
(1) big wing section cold-proof dust-proof clothes: with material therefor according to big wing interior, in, an outer section size cuts out, and each section in edge's flexible connection, vertically is provided with reinforcing cord in the junction; Outside reaching, vertical both sides of the edge of described big wing section cold-proof dust-proof clothes run through plumbous rope in the section edge, edge is provided with connection cord at inner segment, simultaneously laterally be provided with connection cord, the connection cord that laterally is provided with is no less than 50cm in the length with the overlapping part of wing section;
(2) horizontal tail part cold-proof dust-proof clothes: material therefor is cut out according to inside and outside section size of horizontal tail, each section flexibly connected in edge, vertically be provided with reinforcing cord in the junction; Run through plumbous rope in vertical both sides of the edge of described horizontal tail part cold-proof dust-proof clothes, laterally be provided with connection cord simultaneously, the connection cord that laterally is provided with is no less than 50cm in the length with the overlapping part of wing section;
(3) engine section cold-proof dust-proof clothes: material therefor is cut out according to the size of driving engine, each several part is sewed up, the rope that closes up is housed in its opening part edge.
2. a kind of aerostat cold-proof dust-proof clothes as claimed in claim 1, described flexible connection are that double buckle connects.
3. a kind of aerostat cold-proof dust-proof clothes as claimed in claim 1, material therefor are waterproof cloth.
4. a kind of aerostat cold-proof dust-proof clothes as claimed in claim 1, described reinforcing cord, the connection cord and the rope that closes up are common rope.
5. a kind of aerostat cold-proof dust-proof clothes as claimed in claim 1, described plumbous rope is the above ropes of 80 gram/rice.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA200610145469XA CN1966351A (en) | 2006-11-17 | 2006-11-17 | Aerostat cold-proof dust-proof clothes |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA200610145469XA CN1966351A (en) | 2006-11-17 | 2006-11-17 | Aerostat cold-proof dust-proof clothes |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1966351A true CN1966351A (en) | 2007-05-23 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNA200610145469XA Pending CN1966351A (en) | 2006-11-17 | 2006-11-17 | Aerostat cold-proof dust-proof clothes |
Country Status (1)
| Country | Link |
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| CN (1) | CN1966351A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103991551A (en) * | 2014-05-30 | 2014-08-20 | 中国民航大学 | Ice and snow preventing method for flight airplane |
| CN104443418A (en) * | 2014-10-16 | 2015-03-25 | 李浩昌 | Cover or bag preventing wet fog rusting and corrosion of civil aviation berthed aircrafts or high-quality precision equipment |
| FR3057253A1 (en) * | 2016-10-11 | 2018-04-13 | Steven Tromeur | PROTECTIVE COVER FOR AIRCRAFT |
| WO2023175127A1 (en) | 2022-03-17 | 2023-09-21 | Youkana Diden Boris | Envelope, system and method for protecting a portion of an aircraft body |
-
2006
- 2006-11-17 CN CNA200610145469XA patent/CN1966351A/en active Pending
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103991551A (en) * | 2014-05-30 | 2014-08-20 | 中国民航大学 | Ice and snow preventing method for flight airplane |
| CN104443418A (en) * | 2014-10-16 | 2015-03-25 | 李浩昌 | Cover or bag preventing wet fog rusting and corrosion of civil aviation berthed aircrafts or high-quality precision equipment |
| FR3057253A1 (en) * | 2016-10-11 | 2018-04-13 | Steven Tromeur | PROTECTIVE COVER FOR AIRCRAFT |
| WO2023175127A1 (en) | 2022-03-17 | 2023-09-21 | Youkana Diden Boris | Envelope, system and method for protecting a portion of an aircraft body |
| FR3133599A1 (en) | 2022-03-17 | 2023-09-22 | Boris YOUKANA Diden | Envelope, system and method of protection for a portion of an aircraft body |
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