CN204554238U - A kind of aluminum foil composite heat shroud - Google Patents

A kind of aluminum foil composite heat shroud Download PDF

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Publication number
CN204554238U
CN204554238U CN201520126379.0U CN201520126379U CN204554238U CN 204554238 U CN204554238 U CN 204554238U CN 201520126379 U CN201520126379 U CN 201520126379U CN 204554238 U CN204554238 U CN 204554238U
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China
Prior art keywords
heat shroud
foil composite
coating layer
shroud
heat insulation
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Application number
CN201520126379.0U
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Chinese (zh)
Inventor
黄明国
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hunan Star Prosperous Space Flight New Material Ltd Co
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Hunan Star Prosperous Space Flight New Material Ltd Co
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Priority to CN201520126379.0U priority Critical patent/CN204554238U/en
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Publication of CN204554238U publication Critical patent/CN204554238U/en
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Abstract

The utility model relates to a kind of heat shroud of the equipment such as instrument, instrument when being in long on aerospace craft under heatproof or Low emissivity hot-fluid state of the art condition.Disclosed in the utility model, the bottom of heat shroud is made up by a kind of aluminum foil composite heat shroud of high-temperature heat insulation cloth, described high-temperature heat insulation cloth has overlap edge in the corner of instrument and apparatus, be coated with at the outer surface of high-temperature heat insulation cloth and be brushed with continuous print adiabatic coating layer, end face that is outer at adiabatic coating layer and heat shroud is coated with layer of varnish, has aluminium foil composite adiabatic film at this layer of varnish external pasting.This heat shroud conformability easy for installation, shaping is good, protection effect is stablized.

Description

A kind of aluminum foil composite heat shroud
Technical field
The utility model relates to a kind of heat shroud of the equipment such as instrument, instrument when being in long on aerospace craft under heatproof or Low emissivity hot-fluid state of the art condition.
Background technique
At present, the heat insulation material of space flight instrument, instrumentation adopts the wrapped method of multilayer to protect instrument, instrumentation mostly, and this technology exists the shortcomings such as frock inconvenience, shaping conformability is bad, protection effect is unstable.Wrapped fado adopts high-temperature heat insulation cloth to carry out 1/2 scrap (bridge) method and is wound around, and comparatively consuming time comparatively speaking, can produce fifth wheel during winding and gain in weight, in flight course, the heat insulation material of privileged sites exists loose risk under certain frequency.
Model utility content
The technical problems to be solved in the utility model is to provide a kind of aluminum foil composite heat shroud.
For solving the problems of the technologies described above, the utility model about the technological scheme of aluminum foil composite heat shroud is: it makes the bottom of heat shroud by high-temperature heat insulation cloth, described high-temperature heat insulation cloth has overlap edge in the corner of instrument and apparatus, be coated with at the outer surface of high-temperature heat insulation cloth and be brushed with continuous print adiabatic coating layer, end face that is outer at this adiabatic coating layer and heat shroud is coated with layer of varnish, has aluminium foil composite adiabatic film at this layer of varnish external pasting.
Further, described heat shroud is provided with stop hole and lacing hole, and running through in described lacing hole has stainless steel glass cord.
Preferably, described high-temperature heat insulation cloth thickness is 0.3mm, and the thickness of the adiabatic coating layer on described high-temperature heat insulation cloth is 2.0-3.0mm.
Preferably, described adiabatic coating layer is polyurethane adiabatic coating layer.
The utility model, about the making method of the heat shroud of heatproof Low emissivity time long, comprises following process step: 1. make mould; 2. make the bottom of heat shroud of high-temperature heat insulation cloth according to mould; 3. at the outside brushing adiabatic coating of high-temperature heat insulation cloth and baking-curing; 4. rush stop hole and lacing hole according to drawing in heat shroud predetermined portion, crack; 5. the end face lacquer varnish of and heat shroud outer at adiabatic coating layer baking-curing; 6. on layer of varnish, paste aluminium foil composite adiabatic film; 7. lacing hole is run through with stainless steel glass cord.
3. described step is brush brush polyurethane adiabatic coating at the outer surface palm fiber of high-temperature heat insulation cloth, each brushing paint about thickens 0.03-0.06mm, after brushing, product is placed in temperature 25 ± 5 DEG C, relative moisture dries naturally lower than in the room of 65%, time is 10-15 minute, again the product naturally dried is placed in 120 DEG C of electric heating casees and toasts 40-60 minute, coating is solidified completely, then carry out brushing next time and solidification, so repeatedly make whole coating thickness reach 2.0-3.0mm.
The varnish that described step is 5. sprayed is chlorosulfonated polyethylene varnish, toasts 30-40 minute under the protecting cover of lacquer varnish being placed on 100-120 DEG C of temperature environment, ensures that chlorosulfonated polyethylene is varnish curing.
Adopt the utility model making method to produce long time heatproof Low emissivity heat shroud, easy for installation, shaping conformability is good, protection effect is stablized, can 152KW/m 2keep 73 seconds under heat-flux conditions, in heat shroud, instrument, instrument surface temperature are lower than 35 DEG C.
Accompanying drawing explanation
Fig. 1 is the structural representation of the utility model aluminum foil composite heat shroud.
Embodiment
As shown in Figure 1, the utility model about the preferred embodiment of aluminum foil composite heat shroud is: the bottom being made up heat shroud of the high-temperature heat insulation cloth 2 that 0.3mm is thick is wrapped on mould 1, described high-temperature heat insulation cloth 2 has overlap edge in the corner of instrument and apparatus, be coated with at the outer surface of high-temperature heat insulation cloth 2 and be brushed with continuous print, thickness is the polyurethane adiabatic coating layer 3 of 2.4mm, end face that is outer at polyurethane adiabatic coating layer 3 and heat shroud is coated with layer of varnish 4, aluminium foil composite adiabatic film 5 is had at this layer of varnish 4 external pasting, described heat shroud is provided with stop hole and lacing hole, run through in described lacing hole and have stainless steel glass cord.
The utility model comprises following process step about the making method of the heat shroud of heatproof Low emissivity time long:
(1) mould is made
By Customer design department provide need protect instrument, instrument, equipment size drawing, according to drawing processing mold;
(2) high-strength high-temperature adiabatic cloth presses the cutting of mould unfolded drawing
By mould unfolded drawing cutting high-strength high-temperature adiabatic cloth, choose the best alternatives, control the generation of fifth wheel;
(3) lap-joint's brushing adhesive glue
With 504 mighty bonds by A:B=2:1 mix in 25 DEG C of temperature environments, keep 10-15 minute after brush lap-joint at high-strength high-temperature adiabatic cloth, lap-joint is apart from back gauge 15mm;
(4) Overmolded on mould
By high-strength high-temperature adiabatic cloth on mould coated good after, fix with transparent adhesive tape and drawing pin;
(5) brush coating
With palm fiber brush brushing polyurethane adiabatic coating on high-strength high-temperature adiabatic cloth, guarantee without current mark, about thicken 0.03-0.06mm according to each brushing paint;
(6) dry
After brushing, product is placed in temperature is 25 ± 5 DEG C, relative moisture is dried naturally lower than in the room of 65%, the time is 15 minutes;
(7) baking-curing
Naturally the product dried is placed in 120 DEG C of electric heating casees and toasts 40-60 minute, product is solidified completely, avoid because the time limit produces the phenomenon that is clamminess; Step (5)-(7) repeatedly, make the total thickness of polyurethane adiabatic coating layer reach 2.4mm;
(8) repair, clean
Surface treatment is carried out to product inner and outer surface, rejects fifth wheel;
(9) according to drawing requirement setting-out, be cut to given size, rush stop hole and lacing hole according to drawing in predetermined portion, crack;
(10) spray chlorosulfonated polyethylene varnish, utilize its good resistance, stop steam to the corrosion of product, ensure that product is not clamminess under 5 years particular surroundingss; (11) at 100-120 DEG C of temperature, baking 30-40min ensures that chlorosulfonated polyethylene is varnish curing;
(12) on layer of varnish, paste aluminium foil composite adiabatic film;
(13) run through lacing hole with stainless steel glass cord by drawing, long position binding is agglomerating, unties during installation.

Claims (5)

1. an aluminum foil composite heat shroud, it makes the bottom of heat shroud by high-temperature heat insulation cloth, it is characterized in that: described high-temperature heat insulation cloth has overlap edge in the corner of instrument and apparatus, be coated with at the outer surface of high-temperature heat insulation cloth and be brushed with continuous print adiabatic coating layer, end face that is outer at this adiabatic coating layer and heat shroud is coated with layer of varnish, has aluminium foil composite adiabatic film at this layer of varnish external pasting.
2. aluminum foil composite heat shroud according to claim 1, is characterized in that: described heat shroud is provided with stop hole and lacing hole, running through in described lacing hole has stainless steel glass cord.
3. aluminum foil composite heat shroud according to claim 1 and 2, is characterized in that: described high-temperature heat insulation cloth thickness is 0.3mm, and the thickness of the adiabatic coating layer on described high-temperature heat insulation cloth is 2.0-3.0mm.
4. aluminum foil composite heat shroud according to claim 1 and 2, is characterized in that: described adiabatic coating layer is polyurethane adiabatic coating layer.
5. aluminum foil composite heat shroud according to claim 3, is characterized in that: described adiabatic coating layer is polyurethane adiabatic coating layer.
CN201520126379.0U 2015-03-05 2015-03-05 A kind of aluminum foil composite heat shroud Active CN204554238U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520126379.0U CN204554238U (en) 2015-03-05 2015-03-05 A kind of aluminum foil composite heat shroud

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520126379.0U CN204554238U (en) 2015-03-05 2015-03-05 A kind of aluminum foil composite heat shroud

Publications (1)

Publication Number Publication Date
CN204554238U true CN204554238U (en) 2015-08-12

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520126379.0U Active CN204554238U (en) 2015-03-05 2015-03-05 A kind of aluminum foil composite heat shroud

Country Status (1)

Country Link
CN (1) CN204554238U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104676194A (en) * 2015-03-05 2015-06-03 湖南星鑫航天新材料股份有限公司 Aluminum foil composite heat-proof sleeve and manufacturing method thereof

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104676194A (en) * 2015-03-05 2015-06-03 湖南星鑫航天新材料股份有限公司 Aluminum foil composite heat-proof sleeve and manufacturing method thereof
CN104676194B (en) * 2015-03-05 2017-11-24 湖南星鑫航天新材料股份有限公司 A kind of aluminum foil composite heat shroud and preparation method thereof

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