CN102582852A - Astronautic anti-G suit - Google Patents
Astronautic anti-G suit Download PDFInfo
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- CN102582852A CN102582852A CN2012100602859A CN201210060285A CN102582852A CN 102582852 A CN102582852 A CN 102582852A CN 2012100602859 A CN2012100602859 A CN 2012100602859A CN 201210060285 A CN201210060285 A CN 201210060285A CN 102582852 A CN102582852 A CN 102582852A
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Abstract
The invention belongs to the technical field of manned spaceflight, and particularly relates to gravity physiological protective equipment, in particular to an astronautic anti-G suit, which comprises a suit surface component and an anti-G capsule component. The suit surface component comprises a waist component (1) enclosing a waist and a belly of an astronaut and trouser leg components (12) enclosing two legs of the astronaut respectively, the anti-G capsule component comprises a belly capsule (8), leg capsules (9) and a one-way inflating valve (10), the belly capsule (8) and the leg capsules (9) are made of double-faced rubbered cloth and integrally connected, and the anti-G capsule component is fixed to the inner surface of the suit surface component through a capsule sleeve. After the astronautic anti-G suit is inflated, the anti-G capsule component expands to generate mechanical pressure on the astronaut body surface, so that necessary anti-G physiological protection is provided. The astronautic anti-G suit is convenient to take on or take off, suitable for astronauts of different figures and capable of finely adjusting body surface pressure.
Description
Technical field
The invention belongs to the manned space technology field, particularly a kind of gravity physical protection equipment.
Background technology
+ Gx effect has extensive and complicated pathologic, physiologic influence to human body, therefore, in manned space flight, must it be protected, to ensure astronaut's operation work efficiency, healthy and life security.Research shows that astronaut's overweight endurance can be significantly lowered in medium-term and long-term flight.In order to solve the overweight problem that the astronaut is faced in the return course after medium-term and long-term space travel, the Russia and the U.S. have all developed antigravity suit.The U.S. spaceflight antigravity suit is similar with the aviation antigravity suit.Russia's antigravity suit is divided into space flight antigravity suit and flight back protective clothing, and flight back protective clothing has been compared some different (variations) with intumescent aviation clothes, and the clothes internal pressure is produced by manual blood-pressure gage.The space flight antigravity suit is processed with elastic fabric, and elasticity is very strong, and is made up of a pair of length trousers and a pair of spat.On the limit of pants and gaiter belt is arranged, be used to adjust clothes and exert pressure to lower body.The length of waistband is regulated with two belts.Through using the such material of nylon to alleviate the weight of clothes.Antigravity suit also comprises short underwear.Before each flight, each astronaut need adjust the distance of belt on garment dimension and thigh and the shank according to individuality.Before landing 2～3 days, the astronaut then will adjust antigravity suit according to the variation of the caused body sizes of microgravity.Also want the correctness of final inspection adjustment when wearing clothes before the landing.
At present, China does not still have space flight and uses anti-G equipment, needs development to be fit to the space flight antigravity suit that China astronaut uses.
Summary of the invention
The objective of the invention is: provide a kind of, and be convenient to the space flight antigravity suit wearing and adjust for the astronaut provides necessary physical protection.
Technical scheme of the present invention is: a kind of space flight antigravity suit, and it comprises: clothing face assembly and anti-lotus capsule component;
Said clothing face assembly is made up of waist feature that surrounds astronaut's waist and belly and the trouser legs assembly that surrounds astronaut's two legs respectively; Waist zipper is equipped with at position, the corresponding astronaut waist right side of said waist feature dual-side, and the corresponding astronaut's waist left-hand portion in said waist feature middle part is equipped with the waist accommodation zone of being made up of the protecting cloth of regulating rope and band velcro; The corresponding astronaut of said trouser legs assembly dual-side is equipped with big slide fastener in two inboard leg positions; Huckle accommodation zone and the calf accommodation zone of being made up of the protecting cloth of regulating rope and band velcro is equipped with at the rear side position in corresponding astronaut's two legs of said trouser legs assembly;
Belly capsule and shank capsule that said anti-lotus capsule component is made, is connected as a single entity by double spread cloth, and unidirectional charging connector is formed; Said anti-lotus capsule component is fixed on said clothing face module inner by capsule set.
After the present invention's inflation, anti-lotus capsule component expands astronaut's body surface is produced mechanical pressure, and necessary anti-lotus physical protection is provided.And be convenient to wear off, can satisfy astronaut's dress of different statures, can also the trimming body gauge pressure.
Description of drawings
Fig. 1 is a front view of the present invention;
Fig. 2 is anti-lotus capsule component structural representation among the present invention.
The specific embodiment
Embodiment 1: referring to accompanying drawing 1,2, and a kind of space flight antigravity suit, it comprises: clothing face assembly and anti-lotus capsule component;
Said clothing face assembly is made up of waist feature that surrounds astronaut's waist and belly 1 and 12 of trouser legs assemblies surrounding astronaut's two legs respectively; Waist zipper 3 is equipped with at position, the corresponding astronaut waist right side of said waist feature 1 dual-side, and said waist feature 1 middle part corresponding astronaut's waist left-hand portion is equipped with the waist accommodation zone of being made up of the protecting cloth of regulating rope and band velcro 7; The corresponding astronaut of said trouser legs assembly 12 dual-sides is equipped with big slide fastener 4 in two inboard leg positions; The huckle accommodation zone of being made up of the protecting cloth of regulating rope and band velcro 5 and calf accommodation zone 6 is equipped with at the rear side position in said trouser legs assembly 12 corresponding astronaut's two legs;
Belly capsule 8 and shank capsule 9 that said anti-lotus capsule component is made, is connected as a single entity by double spread cloth, and 10 compositions of unidirectional charging connector; Said anti-lotus capsule component is fixed on said clothing face module inner by capsule set.
Embodiment 2: referring to accompanying drawing 1,2, in embodiment 1 described space flight antigravity suit, said anti-lotus capsule component edge is provided with a plurality of fastened tabs pieces 11 that are used to connect said capsule set; Said unidirectional charging connector 10 is arranged on corresponding astronaut's waist left-hand portion.
Claims (2)
1. space flight antigravity suit, it is characterized in that: it comprises: clothing face assembly and anti-lotus capsule component;
Said clothing face assembly is made up of waist feature that surrounds astronaut's waist and belly (1) and the trouser legs assembly (12) that surrounds astronaut's two legs respectively; Waist zipper (3) is equipped with at position, the corresponding astronaut waist right side of said waist feature (1) dual-side, and the corresponding astronaut's waist left-hand portion in said waist feature (1) middle part is equipped with the waist accommodation zone of being made up of the protecting cloth of regulating rope and band velcro (7); The corresponding astronaut of said trouser legs assembly (12) dual-side is equipped with big slide fastener (4) in two inboard leg positions; Huckle accommodation zone (5) and the calf accommodation zone of being made up of the protecting cloth of regulating rope and band velcro (6) is equipped with at the rear side position in corresponding astronaut's two legs of said trouser legs assembly (12);
Belly capsule (8) and shank capsule (9) that said anti-lotus capsule component is made, is connected as a single entity by double spread cloth, and unidirectional charging connector (10) is formed; Said anti-lotus capsule component is fixed on said clothing face module inner by capsule set.
2. space flight antigravity suit according to claim 1 is characterized in that: said anti-lotus capsule component edge is provided with a plurality of fastened tabs pieces (11) that are used to connect said capsule set; Said unidirectional charging connector (10) is arranged on corresponding astronaut's waist left-hand portion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012100602859A CN102582852A (en) | 2012-03-09 | 2012-03-09 | Astronautic anti-G suit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012100602859A CN102582852A (en) | 2012-03-09 | 2012-03-09 | Astronautic anti-G suit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102582852A true CN102582852A (en) | 2012-07-18 |
Family
ID=46472244
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012100602859A Pending CN102582852A (en) | 2012-03-09 | 2012-03-09 | Astronautic anti-G suit |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102582852A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103407588A (en) * | 2013-08-23 | 2013-11-27 | 电子科技大学 | Assisting method and device for movements in space |
| CN109850158A (en) * | 2019-03-29 | 2019-06-07 | 中国人民解放军第四军医大学 | A kind of flyer's fatigue early warning seat |
| CN112849439A (en) * | 2021-02-07 | 2021-05-28 | 中国人民解放军63919部队 | Acceleration confrontation protective clothing |
| CN113879572A (en) * | 2021-09-30 | 2022-01-04 | 中国人民解放军空军军医大学 | Anti-load clothes device based on PVC gel driving |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0746496B1 (en) * | 1994-03-17 | 1999-11-03 | Celsius Aerotech AB | Device for exerting an external pressure on a human body |
| WO2002018206A1 (en) * | 2000-08-30 | 2002-03-07 | Mayo Foundation For Medical Research And Education | Chest garment with influence upon respiratory mechanics and pulmonary perfusion |
| US6695762B1 (en) * | 2002-12-05 | 2004-02-24 | Mustang Survival Corp | Fluid cooled pressure garment |
| RU2254272C2 (en) * | 2003-07-07 | 2005-06-20 | Государственный научный центр Российской Федерации Институт медико-биологических проблем Российской академии наук | Anti-g tubeless suit |
| CN101152907A (en) * | 2006-09-30 | 2008-04-02 | 上海市向明中学 | Space suit for preventing weightlessness |
| CN102009747A (en) * | 2010-11-19 | 2011-04-13 | 航宇救生装备有限公司 | Multicapsular retractable antigravity suit |
-
2012
- 2012-03-09 CN CN2012100602859A patent/CN102582852A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0746496B1 (en) * | 1994-03-17 | 1999-11-03 | Celsius Aerotech AB | Device for exerting an external pressure on a human body |
| WO2002018206A1 (en) * | 2000-08-30 | 2002-03-07 | Mayo Foundation For Medical Research And Education | Chest garment with influence upon respiratory mechanics and pulmonary perfusion |
| US6695762B1 (en) * | 2002-12-05 | 2004-02-24 | Mustang Survival Corp | Fluid cooled pressure garment |
| RU2254272C2 (en) * | 2003-07-07 | 2005-06-20 | Государственный научный центр Российской Федерации Институт медико-биологических проблем Российской академии наук | Anti-g tubeless suit |
| CN101152907A (en) * | 2006-09-30 | 2008-04-02 | 上海市向明中学 | Space suit for preventing weightlessness |
| CN102009747A (en) * | 2010-11-19 | 2011-04-13 | 航宇救生装备有限公司 | Multicapsular retractable antigravity suit |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103407588A (en) * | 2013-08-23 | 2013-11-27 | 电子科技大学 | Assisting method and device for movements in space |
| CN103407588B (en) * | 2013-08-23 | 2016-12-28 | 电子科技大学 | A kind of space sport auxiliary device |
| CN109850158A (en) * | 2019-03-29 | 2019-06-07 | 中国人民解放军第四军医大学 | A kind of flyer's fatigue early warning seat |
| CN112849439A (en) * | 2021-02-07 | 2021-05-28 | 中国人民解放军63919部队 | Acceleration confrontation protective clothing |
| CN112849439B (en) * | 2021-02-07 | 2024-09-03 | 中国人民解放军63919部队 | Acceleration countermeasure protective clothing |
| CN113879572A (en) * | 2021-09-30 | 2022-01-04 | 中国人民解放军空军军医大学 | Anti-load clothes device based on PVC gel driving |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20120718 |