EP0488880A1 - Vollschutzausrüstung - Google Patents
Vollschutzausrüstung Download PDFInfo
- Publication number
- EP0488880A1 EP0488880A1 EP91403195A EP91403195A EP0488880A1 EP 0488880 A1 EP0488880 A1 EP 0488880A1 EP 91403195 A EP91403195 A EP 91403195A EP 91403195 A EP91403195 A EP 91403195A EP 0488880 A1 EP0488880 A1 EP 0488880A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- circuit
- respiratory
- helmet
- garment
- gas
- 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.)
- Granted
Links
Images
Classifications
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62B—DEVICES, APPARATUS OR METHODS FOR LIFE-SAVING
- A62B17/00—Protective clothing affording protection against heat or harmful chemical agents or for use at high altitudes
- A62B17/005—Active or passive body temperature control
Definitions
- the present invention relates to personal protective equipment in a hostile atmosphere, in particular in an atmosphere containing toxic or corrosive products, comprising a diving suit provided with an autonomous supply of respiratory gas and means of ventilation of the diving suit.
- Equipment of this type is already known having a spacesuit consisting of a flexible and waterproof garment and a helmet with transparent visor, connectable to a gas reserve constituted by a supply cylinder of compressed respiratory gas.
- the protective equipment During interventions in such an atmosphere, the protective equipment must supply respiratory gas in quantity and appropriate quality and also ventilate the body to evacuate the heat and to avoid condensation.
- the gas coming from the bottle feeds an ejector intended to suck in air coming from the spacesuit and to put it in circulation for ventilation.
- the atmosphere breathed by the wearer of the suit is made up of a mixture of the supplied breathing gas and the suit's gas.
- the supply of gas from the bottle is compensated by an exhaust through valves fitted to the spacesuit.
- the ventilation circuit can be considered to be open, which results in wasted respiratory gas.
- Such equipment consequently has only a reduced autonomy, owing to the fact that the volume and the weight of the compressed gas cylinders used for respiration and ventilation must remain within acceptable limits.
- the invention aims to solve the problem of the protection of personnel having to intervene on the scene of accidents and for this to have equipment which allows physical activity, therefore a high metabolism, for a long period without dangerous increase in the content.
- CO2 inspired gases
- the invention proposes in particular individual protective equipment in which the reserve of respiratory gas consists of a tank of liquefied gas (liquid air, liquid oxygen or liquefied mixture containing helium and / or hydrogen in addition to oxygen and nitrogen) feeding a respiratory circuit opening into the helmet, generally through a regulating valve, which can be of conventional constitution;
- the equipment is characterized in that the respiratory circuit is supplied by the reservoir through the primary circuit of a heat exchanger and a pneumatic motor interposed between the heat exchanger and the respiratory circuit and is coupled to a circulation fan ventilation air of the garment in a closed circuit passing through the exchanger.
- the ventilation gas is cooled and dried before feeding the spacesuit.
- the return of the ventilation gas to the spacesuit can be carried out by distribution pipes opening out at the ends of the members, according to an already known arrangement, for example that described in document EP-A-0 317 415.
- the ventilation circuit can be closed or simply semi-closed, with evacuation of a gas flow, in the case of equipment intended to be used in the atmosphere.
- the face is separated from the atmosphere around the body by a seal (facial seal or more frequently neck seal) and the helmet is provided with an exhalation valve.
- a seal facial seal or more frequently neck seal
- the helmet is provided with an exhalation valve.
- only a fraction of the flow of respiratory gas coming from the primary circuit of the exchanger is sent to the pneumatic motor, the rest of the flow of gas supplying the helmet or a respiratory mask by the through an on-demand regulator.
- an economizer bag which may have a constitution and a function similar to that of the bags provided on the emergency oxygen masks intended for passengers on commercial aircraft, may be interposed between the outlet of the pneumatic engine and the intake into helmet.
- the invention makes it possible to use not only the breathable nature of the reserve gas but also its physical state, the liquefied gas constituting a source of frigories and the pressure of the vaporized gas. providing the energy needed for ventilation.
- the respiratory equipment shown diagrammatically in FIG. 1 comprises a suit having a garment 10 and a helmet 12 provided with a transparent visor 14.
- the helmet is provided with an exhalation valve 15 provided to maintain an overpressure of a few around the head. millibars compared to the ambient atmosphere.
- a neck seal 16 which is applied against the skin separates the space surrounding the head from the space surrounding the rest of the body. This neck seal 16 can be replaced by a facial seal or an oro-nasal mask.
- the garment is equipped with a network of pipes to organize the circulation of ventilation gas along the limbs and torso.
- this network of pipes includes a distributor 18 between pipes 20 for supplying gas to the ends of the members, the return being effected by circulation along the members towards the space surrounding the torso.
- the garment is equipped with a calibrated valve or more, 22 maintaining an overpressure in the spacesuit. This overpressure will often be around 2 millibars in the case of use of the spacesuit in an atmosphere under normal atmospheric pressure. It is sufficient to prevent the flooding of the suit with toxic or corrosive products from outside.
- a reserve of respiratory gas constituted by a reservoir 24 of liquefied breathable gas.
- This tank belongs to a converter whose general constitution is similar to that of the converters currently used in military aircraft to supply the crew with respiratory gas. It is fitted with a conventional pressure regulator, at 5 bars for example (not shown), and supplies the coil 26 constituting the primary circuit of a heat exchanger 28.
- the output of the coil 26 feeds a rotary pneumatic motor 30, the output of which is connected to a pipe 32 which opens into the helmet 12.
- An economizer bag 46 (in dashes in FIG. 1) can be connected to line 12.
- the respiratory gas which reaches the helmet cannot therefore in any case mix with the gas occupying the interior of the garment.
- the motor 30 is coupled to a fan 34 intended to take gas from the garment 10 and to circulate it in the exchanger 28, where this withdrawn gas cools and dries out.
- the heat exchanger 28 may comprise a casing 36 for guiding the gas, provided at its base with means for discharging the condensates, which can be reduced to a tube 38 of small section.
- the upper part of the envelope 36 can be simply opened widely above the fan 34, so as to collect gas in the garment 10.
- the lower part of the envelope 36 feeds a sheath 40 which opens into the distributor 18.
- the collected gas passes through the fan 34, scans the coil 26, passes through the distributor 18 and from there is sent to the ends of the members.
- FIG. 2 shows a motor 30 constituted by a turbine whose output shaft carries a fan propeller 34.
- the diameter of the turbine can be much smaller than that of the fan propeller, since the flow rate passing through the turbine is much lower than that which must pass through the secondary circuit of the exchanger. For example, for a flow of 8 to 15 l / min through the turbine, the flow of the fan will generally be between 150 and 200 l / min.
- the supply pressure of the motor can be several bars while a few millibars are enough to overcome the pressure losses of the ventilation circuit.
- the air supply to the fan can therefore take place through an annular space formed around the turbine.
- the supply of respiratory gas to the turbine and the departure of gas can be carried out by small diameter pipes.
- the motor 30 can have other constitutions: in particular, it can be constituted not by an expansion turbine, but by a volumetric machine, such as for example the pneumatic vane motor shown in FIG. 3.
- the rotor 42 which carries the pallets 44 is still coupled to the fan 34.
- the output of the coil of the exchanger 28 is connected to two circuits opening into the helmet.
- the first circuit is similar to that which is mounted in FIG. 1, but comprises a flexible economiser bag 46, contained in the garment and having a volume of the order of a liter when it is inflated.
- This bag 46 placed upstream of the outlet in the helmet 12 and downstream of the motor 30, adapts the continuous flow of the pneumatic motor 30 at the alternating flow of respiration, without increasing consumption.
- the second circuit includes a demand regulator 48 having a reference pressure tap in the helmet to control the flow. It feeds a diffuser 50 for demisting the visor 14, opening into the helmet.
- the variant embodiment shown in FIG. 5 differs from the previous one by selection means making it possible to supply the secondary circuit of the exchanger 28 either through the fan 34 (normal operation) or through a suction ejector 58 air in the garment.
- These selection means comprise a three-way valve 60, with manual control or with automatic control in the event of a malfunction of the motor-vacuum cleaner assembly.
- the valve 60 In a first position, the valve 60 sends a fraction of the gas leaving the primary circuit of the exchanger to the pneumatic motor 30. In its second position, it sends this fraction of the gas to the ejector 58.
- a non-return valve 62 is interposed on the air intake to the fan.
- Another valve 64 is interposed on the inlet to the ejector.
Landscapes
- Health & Medical Sciences (AREA)
- Toxicology (AREA)
- General Health & Medical Sciences (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Respiratory Apparatuses And Protective Means (AREA)
- Professional, Industrial, Or Sporting Protective Garments (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9014811A FR2669541B1 (fr) | 1990-11-27 | 1990-11-27 | Equipement de protection a scaphandre. |
FR9014811 | 1990-11-27 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0488880A1 true EP0488880A1 (de) | 1992-06-03 |
EP0488880B1 EP0488880B1 (de) | 1995-10-11 |
Family
ID=9402639
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP91403195A Expired - Lifetime EP0488880B1 (de) | 1990-11-27 | 1991-11-26 | Vollschutzausrüstung |
Country Status (7)
Country | Link |
---|---|
US (1) | US5339806A (de) |
EP (1) | EP0488880B1 (de) |
JP (1) | JPH07554A (de) |
CA (1) | CA2056211C (de) |
DE (1) | DE69113757T2 (de) |
ES (1) | ES2079050T3 (de) |
FR (1) | FR2669541B1 (de) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1994028346A1 (en) * | 1993-06-01 | 1994-12-08 | Andonian Martin D | All position cryogenic liquefied-gas container |
GB2281103A (en) * | 1993-08-10 | 1995-02-22 | Luo A Fa | Fans driven by pneumatic motors |
US5499623A (en) * | 1992-02-22 | 1996-03-19 | Dragerwerk Ag | Gas mask and breathing equipment with liquefied respiration gas |
WO1996032988A1 (en) * | 1995-04-21 | 1996-10-24 | Figgie International Inc. | Apparatus for providing a conditioned airflow inside a microenvironment and method |
CN105066504A (zh) * | 2015-08-06 | 2015-11-18 | 浙江省江山市浙安消防设备有限公司 | 降温服制冷装置 |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2699414B1 (fr) * | 1992-12-22 | 1995-02-10 | Matisec Mat Ind Securite | Scaphandre de protection comportant un système respiratoire autonome intégré. |
US5632043A (en) * | 1995-04-13 | 1997-05-27 | Mitsubishi Semiconductor America Inc. | Hazardous material protection suit with carrying handles |
US5704073A (en) | 1995-08-01 | 1998-01-06 | Figgie International Inc. | Quick donning goggles for use with breathing mask |
US6681589B2 (en) * | 2002-02-01 | 2004-01-27 | Honeywell International Inc. | Space suit backpack using solid adsorbents for cryogenic oxygen storage, freezeout of carbon dioxide and moisture, and ice heat sink |
US6823867B2 (en) | 2002-04-12 | 2004-11-30 | 3M Innovative Properties Company | Pouch for the blower unit of a powered air purifying respirator |
US6948191B2 (en) * | 2002-04-12 | 2005-09-27 | 3M Innovative Properties Company | Personal protective suit with partial flow restriction |
US6796304B2 (en) | 2002-04-12 | 2004-09-28 | 3M Innovative Properties Company | Personal containment system with sealed passthrough |
US7124593B2 (en) * | 2003-09-02 | 2006-10-24 | Steve Feher | Temperature conditioning apparatus for the trunk of a human body |
EP1786523B1 (de) * | 2004-07-23 | 2009-10-07 | Interspiro, Inc. | Vorrichtung zur bereitstellung atembarer luft und körperlichen schutzes in einer kontaminierten umgebung |
US8011027B2 (en) * | 2004-11-17 | 2011-09-06 | Interspiro, Inc. | Protective seal mechanism |
US7937775B2 (en) | 2005-08-09 | 2011-05-10 | Microtek Medical, Inc. | Surgical protective head gear assembly including high volume air delivery system |
CA2677132A1 (en) * | 2007-04-11 | 2008-10-23 | John J. Davis | Atraumatic introducer for nasal endotracheal tubes and its method of use |
JP5198311B2 (ja) * | 2008-02-18 | 2013-05-15 | 株式会社イハラ | 防護装備、隔離設備およびフィルタ |
CN104841069B (zh) * | 2015-05-27 | 2018-04-06 | 苏州经贸职业技术学院 | 可降温防护服 |
JP7506390B2 (ja) * | 2019-11-19 | 2024-06-26 | 興研株式会社 | 空気呼吸器および空気呼吸器とともに着用される防火服 |
US20230330448A1 (en) * | 2020-10-19 | 2023-10-19 | Avox Systems Inc. | De-misting system for a mask and associated methods |
CN112999789A (zh) * | 2021-03-15 | 2021-06-22 | 恩平市超弦膜技术有限公司 | 应用于封闭式防护服正压呼吸***的分子膜气体净化方法 |
CN114084317A (zh) * | 2021-11-22 | 2022-02-25 | 东台市兴盾船舶设备有限公司 | 一种消防潜水浮力背心 |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1306894A (fr) * | 1961-11-23 | 1962-10-19 | Garrett Corp | Perfectionnements aux appareils de conditionnement |
FR2366028A1 (fr) * | 1976-10-01 | 1978-04-28 | Draegerwerk Ag | Vetement de protection contre la chaleur et les gaz |
US4181126A (en) * | 1978-01-23 | 1980-01-01 | Hendry Stephen M | Cryogenic, underwater-breathing apparatus |
GB2032255A (en) * | 1978-10-23 | 1980-05-08 | Draegerwerk Ag | A protective suit and method of cooling a wearer of the suit |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2423631A (en) * | 1942-01-26 | 1947-07-08 | Univ Minnesota | Conversion apparatus |
US2990695A (en) * | 1958-10-06 | 1961-07-04 | Bendix Corp | Thermodynamic transfer systems |
US3161192A (en) * | 1960-12-06 | 1964-12-15 | Mark E Mccormack | Air-conditioned protective garment and air-supply-and-conditioning apparatus for the same |
US3487765A (en) * | 1966-10-06 | 1970-01-06 | United Aircraft Corp | Protective garment ventilation system |
US3528414A (en) * | 1968-05-15 | 1970-09-15 | Us Air Force | Automatic analogue breathing system for multicell pressure suits |
US3730178A (en) * | 1970-03-24 | 1973-05-01 | F Moreland | Deep-sea dive suit and life support system |
SU698625A1 (ru) * | 1978-03-13 | 1979-11-25 | Одесский Технологический Институт Холодильной Промышленности | Автономна теплозащитна дыхательна система |
-
1990
- 1990-11-27 FR FR9014811A patent/FR2669541B1/fr not_active Expired - Fee Related
-
1991
- 1991-11-26 ES ES91403195T patent/ES2079050T3/es not_active Expired - Lifetime
- 1991-11-26 US US07/798,318 patent/US5339806A/en not_active Expired - Fee Related
- 1991-11-26 CA CA002056211A patent/CA2056211C/fr not_active Expired - Fee Related
- 1991-11-26 DE DE69113757T patent/DE69113757T2/de not_active Expired - Fee Related
- 1991-11-26 EP EP91403195A patent/EP0488880B1/de not_active Expired - Lifetime
- 1991-11-27 JP JP3312770A patent/JPH07554A/ja not_active Withdrawn
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1306894A (fr) * | 1961-11-23 | 1962-10-19 | Garrett Corp | Perfectionnements aux appareils de conditionnement |
FR2366028A1 (fr) * | 1976-10-01 | 1978-04-28 | Draegerwerk Ag | Vetement de protection contre la chaleur et les gaz |
US4181126A (en) * | 1978-01-23 | 1980-01-01 | Hendry Stephen M | Cryogenic, underwater-breathing apparatus |
GB2032255A (en) * | 1978-10-23 | 1980-05-08 | Draegerwerk Ag | A protective suit and method of cooling a wearer of the suit |
Non-Patent Citations (1)
Title |
---|
SOVIET INVENTIONS ILLUSTRATED Section PQ, Week C27, 13 Août 1980 Derwent Publications Ltd., London, GB; Class P35, AN F8905 & SU-A-698 625 (ODESSA REFRIG) * |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5499623A (en) * | 1992-02-22 | 1996-03-19 | Dragerwerk Ag | Gas mask and breathing equipment with liquefied respiration gas |
WO1994028346A1 (en) * | 1993-06-01 | 1994-12-08 | Andonian Martin D | All position cryogenic liquefied-gas container |
GB2281103A (en) * | 1993-08-10 | 1995-02-22 | Luo A Fa | Fans driven by pneumatic motors |
WO1996032988A1 (en) * | 1995-04-21 | 1996-10-24 | Figgie International Inc. | Apparatus for providing a conditioned airflow inside a microenvironment and method |
CN105066504A (zh) * | 2015-08-06 | 2015-11-18 | 浙江省江山市浙安消防设备有限公司 | 降温服制冷装置 |
Also Published As
Publication number | Publication date |
---|---|
DE69113757T2 (de) | 1996-03-14 |
JPH07554A (ja) | 1995-01-06 |
CA2056211A1 (fr) | 1992-05-28 |
DE69113757D1 (de) | 1995-11-16 |
FR2669541B1 (fr) | 1993-02-19 |
US5339806A (en) | 1994-08-23 |
FR2669541A1 (fr) | 1992-05-29 |
EP0488880B1 (de) | 1995-10-11 |
ES2079050T3 (es) | 1996-01-01 |
CA2056211C (fr) | 1998-09-29 |
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