CN202396486U - Active heating type anti-immersion cold-proof flying wear - Google Patents
Active heating type anti-immersion cold-proof flying wear Download PDFInfo
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- CN202396486U CN202396486U CN2011205573641U CN201120557364U CN202396486U CN 202396486 U CN202396486 U CN 202396486U CN 2011205573641 U CN2011205573641 U CN 2011205573641U CN 201120557364 U CN201120557364 U CN 201120557364U CN 202396486 U CN202396486 U CN 202396486U
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Abstract
The utility model provides a thinner anti-immersion cold-proof flying wear structure capable of actively heating and carrying out temperature regulation, which replaces an original heavy structure which is purely and passively used for keeping warm. The thinner anti-immersion cold-proof flying wear structure comprises an anti-immersion layer and a warmth retention layer. The warmth retention layer is on the inner layer and the anti-immersion layer is on the outer layer, wherein a plurality of electric heating sheets, heating sheet wires, a power supply assembly and a power supply storage bag are also arranged on the warmth retention layer; and the electric heating sheets are connected with the power supply assembly by the heating sheet wires; and the power supply assembly is arranged in the power supply storage bag. According to the utility model, an active heating mode is adopted; the thickness of the flying wear is reduced; the heat load generated when a user wears the flying wear at ordinary times is greatly reduced and the wearing comfort is effectively improved.
Description
Technical field
The utility model relates to the anti-winter protection flying suit that soaks of active heating formula that a kind of pilot uses.
Background technology
Pilot's oversea flight in winter, emergency ejection or parachute jumping are disembarked, and will receive cold water low temperature after falling into water and threaten, and this needs the pilot to wear anti-ly to soak the winter protection flying suit, in case cold water soak prolongs the tolerance time of pilot in cold water that fall into water.
The anti-winter protection flying suit that soaks of pilot's dress has both at home and abroad at present all adopted passive resisting to soak warming frame mode, and primary structure is two-layer clothes, and skin soaks layer for anti-, and internal layer is a warming layer.Anti-full pressure suit assembling structure form of soaking the coating of layer employing whole body; The internal layer warming layer is cotton clothes.The groundwork principle is soaked into the warming clothing of internal layer for the anti-layer mode cold water that soaks in the back of falling into water, and leans on the heat exchange of the isolated human body of pilot's insulation cotton layer and extraneous (cold water and cold air), prevents that body temperature is too fast to scatter and disappear, reach prolong the time-to-live, purpose to be rescued.
Passive warm keeping structure anti-soaks the problem that insulated cold wear mainly exists: 1. cotton bed thickness is heavy, and weight loading is big with regard to the pilot who wears various special protecting clothings for original, and comfortableness is poor; 2. dress at ordinary times, temperature is higher in the aircraft cockpit, wears thick and heavy cotton clothes, has certain thermic load; 3. owing to wear thick and heavy cotton clothes, can only soak the outside that insulated cold wear is worn in high-performance apparels such as antigravity suit with resisting, make that whole clothing system structure is too fat to move, pilot's mobility reduces after the dressing, the back swimming of falling into water is difficult.
Summary of the invention
The utility model technical problem to be solved is the technical deficiency to above-mentioned existence, and the anti-winter protection flying suit structure of soaking that provides a kind of thiner can initiatively heating to go forward side by side the trip temperature adjusting replaces simple passive warming thick and heavy structure.
The utility model solves the technical scheme that its technical problem adopted:
The anti-winter protection flying suit that soaks of a kind of active heating formula; Include anti-layer and the warming layer of soaking, warming layer is at nexine, and the anti-layer that soaks is at skin; It is characterized in that: the polylith electric heating sheets also is housed on the described warming layer; Heating plate lead, power supply module and power supply storage bag, electric heating sheets is connected with power supply module through the heating plate lead, and power supply module is installed in the power supply storage bag.
In such scheme, an end of described heating plate lead connects electric heating sheets, and the other end passes to resist through lead switching seal nipple and soaks a layer waist, is connected with power supply module.
In such scheme, described lead switching seal nipple comprises rubber base and ramie rope; Rubber base is the sucker shape structure that has the hole; The rubber base bottom is bonded in the inner surface of flying suit, and the heating plate lead passes the hole on the said rubber base, and tightens with the ramie rope at connecting portion.
In such scheme, the described anti-layer that soaks is made for passing through the vapour impermeable material, and the back shoulder is provided with the watertight zip fastener structure of horizontal opening.
In such scheme, described electric heating sheets is a carbon fibre heating plate, is separately positioned on about the inboard anterior part of chest of warming layer about each a slice, preabdomen each a slice about each a slice, back part a slice, rear waist a slice, huckle.
In such scheme, described power supply module includes lithium battery, the automatic opener of entry, manually opened structure, gear governor motion, and wherein the automatic opener of entry has adopted and gone into the principle that seawater excites connection automatically.
The beneficial effect of the utility model is:
1. owing to adopted the initiatively mode of heating, the thickness of flying suit reduces, and greatly reduces the thermic load when wearing at ordinary times, has effectively improved snugness of fit.
2. because power supply module has adopted the entry pattern of unlatching automatically, after falling into water, warming layer heats automatically, can be implemented in heating warm-keeping under personnel's comatose state, prolongs survival time.
3. because power supply module has adopted the gear setting, cold season fall into water with landing conditions under, personnel can experience according to self, regulate the heating gear, reach the best human effect.
Description of drawings
Fig. 1 is the anti-front view that soaks layer of the utility model embodiment.
Fig. 2 is the perspective view of the utility model embodiment warming layer.
Fig. 3 is the cutaway view of the lead switching seal nipple of the utility model embodiment.
Fig. 4 is the battery component schematic diagram of the utility model embodiment
The anti-layer, 2-power supply storage bag, 3-warming layer, 4-electric heating sheets of soaking of 1-among the figure; 5-heating plate lead, 6-power supply module, 7-lead switching seal nipple, the automatic opener of 8-entry; The manually opened structure of 9-, 10-gear governor motion, 11-battery, 12-ramie line; The 13-watertight zip fastener, 14-crotch belly watertight zip fastener, the quick-release coupling of 15-waterproof.
The specific embodiment
Below in conjunction with the specific embodiment, the utility model is further described:
Like the anti-winter protection flying suit that soaks of Fig. 1 active heating formula shown in Figure 2; Include anti-layer 1 and the warming layer 3 of soaking; Warming layer 3 is at nexine, and the anti-layer 1 that soaks also is equipped with polylith electric heating sheets 4 at skin on the described warming layer 3; Electric heating sheets 4 is connected with power supply module 6 through heating plate lead 5, and power supply module 6 is installed in the power supply storage bag 2.
As shown in Figure 1, power supply storage bag 2 is arranged on the anti-left belly 1 that soaks layer 1, and watertight zip fastener 13 is arranged on anti-shoulder back of the body lateral attitude of soaking layer 1, is provided with crotch belly watertight zip fastener 14 at the crotch belly.
As shown in Figure 2, warming layer 3 heads straight for flap hatch frame for the shirtfront, totally 8 of electric heating sheets 4, be separately positioned on about the anterior part of chest of warming layer 3 each one, about preabdomen each one, about one of back part, one of rear waist, huckle each one.
8 electric heating sheets 4 adopt parallel waies to connect through heating plate lead 5, and in the left belly position of warming layer 3 boundling, and pass from the outlet of warming layer 3 left bellies.Add the heat demand according to human body, the area of 8 heating plates 5 differs.
As shown in Figure 3, the anti-left belly that soaks in the layer 1 is provided with seal member, and the sealing parts comprise lead switching seal nipple 7 and ramie rope 12.Lead switching seal nipple 7 is bonded in the anti-inner surface that soaks layer 1, and heating plate lead 5 passes lead switching seal nipple 7, and tightens with ramie rope 12 at connecting portion, is used for the sealing that heating plate lead 5 passes lead switching seal nipple 7.Waterproof quick-release coupling 15 is adopted at the two ends of heating plate lead 5 here, and the outside is used to connect battery component 6, and the inboard is used for the heating plate lead 5 of electric heating sheets 4 boundlings.
As shown in Figure 4, said battery component 6 is made up of the automatic opener of entry 8, manually opened structure 9, gear governor motion 10, battery 11.The automatic opener 8 of entry adopts the mode of parallel circuit to connect with manually opened structure 9, then preceding termination battery 11, and back termination gear governor motion 10, the other end of gear governor motion 10 is connected to through the quick-release mode and leads on the heating plate lead 5.Battery component 6 is placed in the power supply storage bag 2.
During use, at first electric heating sheets 4, heating plate lead 5 are installed on the relevant position of warming layer 3, then battery component 6 is placed in the power supply storage bag 2, personnel have worn flying suit, and assist the close slide fastener 13 of drop-down Heshui the people.Through the opening of crotch belly watertight zip fastener 14, connect the lead switching inboard waterproof quick-release coupling 15 in seal nipple 7 places; In the anti-outside of soaking layer 1, also connect waterproof quick-release coupling 15, make the heating plate lead 5 between battery component 6 and the electric heating sheets 4 be in connection status.Drawing crotch belly watertight zip fastener 14.Behind the waterborne or land emergency escape of pilot, can start electric heating sheets work through the manually opened structure 9 of battery component 6, to human body heating, warming resisting cold.After falling into cold water, the anti-layer 1 that soaks has stoped cold water to soak the internal layer clothing, keeps warming effect, prolongs survival time; After pilot ejection is disembarked, lie in a comatose condition for some reason, perhaps forget the unlatching electrical heating, after falling into water, open heating automatically after the automatic opener 8 of the entry of battery component 6 is met water.The pilot can through the gear governor motion 10 of battery component 6, adjust heating power according to personal feeling.
The protection domain of the utility model is not limited to the above embodiments, and obviously, those skilled in the art can carry out various changes and distortion and not break away from the scope and the spirit of this utility model the utility model.If these changes and distortion belong in the scope of the utility model claim and equivalent technologies thereof, then the intention of the utility model also comprises these changes and is out of shape interior.
Claims (6)
1. anti-winter protection flying suit that soaks of heating formula initiatively; Include anti-layer and the warming layer of soaking, warming layer is at nexine, and the anti-layer that soaks is at skin; It is characterized in that: the polylith electric heating sheets also is housed on the described warming layer; Heating plate lead, power supply module and power supply storage bag, electric heating sheets is connected with power supply module through the heating plate lead, and power supply module is installed in the power supply storage bag.
2. active heating formula as claimed in claim 1 is anti-soaks the winter protection flying suit, and it is characterized in that: an end of described heating plate lead connects electric heating sheets, and the other end passes to resist through lead switching seal nipple and soaks a layer waist, is connected with power supply module.
3. according to claim 1 or claim 2 the anti-winter protection flying suit that soaks of active heating formula; It is characterized in that: described lead switching seal nipple; Comprise rubber base and ramie rope, rubber base is the sucker shape structure that has the hole, and the rubber base bottom is bonded in the inner surface of flying suit; The heating plate lead passes the hole on the said rubber base, and tightens with the ramie rope at connecting portion.
4. active heating formula as claimed in claim 1 is anti-soaks the winter protection flying suit, it is characterized in that: the described anti-layer that soaks is made for passing through the vapour impermeable material, and the back shoulder is provided with the watertight zip fastener structure of horizontal opening.
5. the anti-winter protection flying suit that soaks of active heating formula as claimed in claim 1; It is characterized in that: described electric heating sheets is a carbon fibre heating plate, is separately positioned on about the inboard anterior part of chest of warming layer about each a slice, preabdomen each a slice about each a slice, back part a slice, rear waist a slice, huckle.
6. active heating formula as claimed in claim 1 is anti-soaks the winter protection flying suit, and it is characterized in that: described power supply module includes lithium battery, the automatic opener of entry, manually opened structure, gear governor motion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205573641U CN202396486U (en) | 2011-12-28 | 2011-12-28 | Active heating type anti-immersion cold-proof flying wear |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205573641U CN202396486U (en) | 2011-12-28 | 2011-12-28 | Active heating type anti-immersion cold-proof flying wear |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202396486U true CN202396486U (en) | 2012-08-29 |
Family
ID=46694175
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011205573641U Expired - Fee Related CN202396486U (en) | 2011-12-28 | 2011-12-28 | Active heating type anti-immersion cold-proof flying wear |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202396486U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108685212A (en) * | 2018-05-31 | 2018-10-23 | 邦威防护科技股份有限公司 | Electrical heating vest |
-
2011
- 2011-12-28 CN CN2011205573641U patent/CN202396486U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108685212A (en) * | 2018-05-31 | 2018-10-23 | 邦威防护科技股份有限公司 | Electrical heating vest |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120829 Termination date: 20181228 |