US3000010A - Pressure suit - Google Patents
Pressure suit Download PDFInfo
- Publication number
- US3000010A US3000010A US507405A US50740555A US3000010A US 3000010 A US3000010 A US 3000010A US 507405 A US507405 A US 507405A US 50740555 A US50740555 A US 50740555A US 3000010 A US3000010 A US 3000010A
- Authority
- US
- United States
- Prior art keywords
- panels
- pressure
- suit
- electrical
- wearer
- 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.)
- Expired - Lifetime
Links
- 239000004744 fabric Substances 0.000 description 11
- 239000002184 metal Substances 0.000 description 7
- 229910052751 metal Inorganic materials 0.000 description 7
- 239000000463 material Substances 0.000 description 4
- 239000004020 conductor Substances 0.000 description 3
- 230000003014 reinforcing effect Effects 0.000 description 2
- 239000004753 textile Substances 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229920000742 Cotton Polymers 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 230000001595 contractor effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 239000010985 leather Substances 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- FESBVLZDDCQLFY-UHFFFAOYSA-N sete Chemical compound [Te]=[Se] FESBVLZDDCQLFY-UHFFFAOYSA-N 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D10/00—Flight suits
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D10/00—Flight suits
- B64D2010/005—High altitude suits or garments, e.g. partial or total pressure
Definitions
- This invention relates to a pressure suit for aircraft pilots.
- FIGURE l is a view of a pressure suit of the invention as worn by a pilot;
- FIGURE 2 is a diagrammatic plan section of the suit of FIGURE 1 in the chest region illustrating the contracting action thereof in increasing pressure upon the wearer;
- FIGURE 3 is a sectional view of the air permeable materials from which the suit of FIGURE l is formed.
- the pressure suit of the invention preferably comprises a contractible body covering 10, a helmet 11, gloves 12, and boots 13.
- the covering is formed of an air permeable mate rial 14 shown in section in FIGURE 3 having an outer layer preferably formed of closely knitted relatively ne enamel-insulated copper wire cloth 15 separated from an inner cotton or other suitable textile cloth 16 by an inisulating material 17 such as batting formed of line glass bers.
- Sleeves 1-8 are fastened relatively tightly about the wearers arms by the slide fasteners v19 and are laced as at 20 to a shoulder fitting 21 on each side suitably reinforced with leather sheeting 22 or the like.
- the covering 10 is separable on substantially vertical spaced apart lines 24 and 25 extending from shoulder to toe down the front of the body and is suitably reinforced by reinforcing strips 25 and 26 to support lacings 27 and 28 whereby in the upper regions of the suit so formed a front panel portion 29 is fastened to a back panel portion 30 as shown in FIGURE 2.
- Tensioning electrical solenoid devices 31 having a conventional solenoid or coil part 32 adapted to draw thereinto the rod or core 33 anchored to anchorage fitting 34, are mounted on the reinforcing strips 25 and 26.
- the solenoid devices 31 are connected electrically in parallel through junction box 31a and cable 31b to a suitable source of electrical power including a rheostat (not shown) whereby the energization of the solenoids can be controlled to apply predetermined tensioning represented by arrows Y and effect control of pressure or tensioning upon the body of the wearer.
- the solenoid devices may be covered by a pliable pouch 35 to protect the mechanism thereof.
- the helmet 11 may embody earphones 36 and a microphone 37 connectable by cable 38 to a communication system (not shown). Note that the boots 13 terminating at 39 are also tensionable and are separable upon removal of lacings 27 and 28.
- a metal fabric formed of knitted wire wherein each wire carries an insulating coating forms a part of this invention. It is intended that a plurality of individual wires of such fabric may be connected electrically in parallel to serve as an electrical conductor having resistance to current iiow whereby the fabric may be heated. Also the metal fabric herein as compared with a textile fabric may present a greater mass for absorption of nuclear radiation.
- the gloves 12 may be formed of the metal fabric of the invention without additional insulatlefed Sete., Patent' 0 V'ing layers of material. Because the fabric is "ice" knitted and is of metal it embodies a limited characteristic of stretchability adapted to confine the ilesh at low atmospheric pressures. Accordingly, special tensioning devices need not necessarily be employed in regions of the arms and hands of the wearer.
- a pressure suit adapted to compensate for changes in atmospheric pressure upon the body of a wearer and comprising in combination: gas permeable pliable panels of limited interstitial stretchability formed to envelope the torso arms and legs of the human body; a plurality of electrical solenoid devices each having a core part attached to an edge of one of said panels and a coil part attached to an edge of an adjacent panel, said devices being adapted for tensioning said panels; and electrical conducting means for providing electrical energization of said devices whereby said panels are tensioned about the body of the wearer while enabling the skin of the body to breathe through said panels at substantially atmospheric pressure.
Landscapes
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Pulmonology (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toxicology (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Gloves (AREA)
Description
Sept. 19, 1961 c. RICH PRESSURE SUIT Filed may 1o, 1955 Inventor CARL R/cH by" QLQQMNQ Filed May 10, 1955, Ser. No. 507,405 4 Claims. (Cl. 2-2.1)
'This invention relates to a pressure suit for aircraft pilots.
It is the main object of the invention to provide a pressure suit which is air or gas permeable.
Other objects of the invention will be appreciated by a study of the following specification taken in conjunction with the accompanying drawings.
In the drawings:
FIGURE l is a view of a pressure suit of the invention as worn by a pilot;
FIGURE 2 is a diagrammatic plan section of the suit of FIGURE 1 in the chest region illustrating the contracting action thereof in increasing pressure upon the wearer;
FIGURE 3 is a sectional view of the air permeable materials from which the suit of FIGURE l is formed.
Referring to the drawings, the pressure suit of the invention preferably comprises a contractible body covering 10, a helmet 11, gloves 12, and boots 13.
The covering is formed of an air permeable mate rial 14 shown in section in FIGURE 3 having an outer layer preferably formed of closely knitted relatively ne enamel-insulated copper wire cloth 15 separated from an inner cotton or other suitable textile cloth 16 by an inisulating material 17 such as batting formed of line glass bers.
Sleeves 1-8 are fastened relatively tightly about the wearers arms by the slide fasteners v19 and are laced as at 20 to a shoulder fitting 21 on each side suitably reinforced with leather sheeting 22 or the like. The covering 10 is separable on substantially vertical spaced apart lines 24 and 25 extending from shoulder to toe down the front of the body and is suitably reinforced by reinforcing strips 25 and 26 to support lacings 27 and 28 whereby in the upper regions of the suit so formed a front panel portion 29 is fastened to a back panel portion 30 as shown in FIGURE 2.
Tensioning electrical solenoid devices 31 having a conventional solenoid or coil part 32 adapted to draw thereinto the rod or core 33 anchored to anchorage fitting 34, are mounted on the reinforcing strips 25 and 26. The solenoid devices 31 are connected electrically in parallel through junction box 31a and cable 31b to a suitable source of electrical power including a rheostat (not shown) whereby the energization of the solenoids can be controlled to apply predetermined tensioning represented by arrows Y and effect control of pressure or tensioning upon the body of the wearer. As shown in FIGURE l, the solenoid devices may be covered by a pliable pouch 35 to protect the mechanism thereof.
The helmet 11 may embody earphones 36 and a microphone 37 connectable by cable 38 to a communication system (not shown). Note that the boots 13 terminating at 39 are also tensionable and are separable upon removal of lacings 27 and 28.
A metal fabric formed of knitted wire wherein each wire carries an insulating coating forms a part of this invention. It is intended that a plurality of individual wires of such fabric may be connected electrically in parallel to serve as an electrical conductor having resistance to current iiow whereby the fabric may be heated. Also the metal fabric herein as compared with a textile fabric may present a greater mass for absorption of nuclear radiation. The gloves 12 may be formed of the metal fabric of the invention without additional insulatlefed Sete., Patent' 0 V'ing layers of material. Because the fabric is "ice" knitted and is of metal it embodies a limited characteristic of stretchability adapted to confine the ilesh at low atmospheric pressures. Accordingly, special tensioning devices need not necessarily be employed in regions of the arms and hands of the wearer.
What I claim as my invention is:
1. A pressure suit adapted to compensate for changes in atmospheric pressure upon the body of a wearer and comprising in combination: metal wire fabric gas perm@ able pliable panels of limited interstitial stretchability formed to enclose the human body; electrical tensioning means attached to portions of adjacent panels; and electrical conducting means for providing electrical energization of said tensioning means whereby said panels are tensioned to apply a predetermined pressure to the body of the wearer while enabling the skin of the body to breathe through said panels at substantially atmospheric pressure.
2. A pressure suit adapted to compensate for changes in atmospheric pressure upon the body of a wearer and comprising in combination: knitted insulated metal wire fabric gas permeable pliable panels of limited interstitial stretchability formed to enclose the human body, said insulated Wire constituting an electrical conductor; an electrical circuit for supplying electrical energy to said conductor whereby heat may be generated; electrical solenoid tensioning means having core parts attached to an edge of one of said panels and coil parts attached to an edge of an adjacent panel; and electrical conducting means for providing electrical energization of said tensioning means whereby said panels are tensioned to apply a pre determined pressure to the body of the wearer while enabling the skin of the body to breathe through said panels at substantially atmospheric pressure.
3. A pressure suit adapted to compensate for changes in atmospheric pressure upon the body of a wearer and comprising in combination: gas permeable pliable panels of limited interstitial stretchability formed to envelope the torso arms and legs of the human body; a plurality of electrical solenoid devices each having a core part attached to an edge of one of said panels and a coil part attached to an edge of an adjacent panel, said devices being adapted for tensioning said panels; and electrical conducting means for providing electrical energization of said devices whereby said panels are tensioned about the body of the wearer while enabling the skin of the body to breathe through said panels at substantially atmospheric pressure.
4. A suit adapted to confine the esh of the body of the wearer under a condition of low atmospheric pressure and comprising in combination: a plurality of flexible gas permeable panels formed of knitted metal wire of limited interstitial stretchability and adapted to enclose the human body; means connecting certain of said panels to denne an enclosing suit for a wearers body enabling the skin of the body to breathe at atmospheric pressure through said panels; electrical solenoid tensioning means having a core part thereof attached to an edge of one of said panels and the coil part thereof attached to an adjacent panel; and electrical conducting means for providing electrical energization of said tensioning means whereby said panels are tensioned to restrict the esh of the body to substantially maintain the internal pressures therein under a condition of lesser external atmospheric pressure providing normal body evaporation function under abnormally low pressure conditions.
References Cited in the tile of this patent UNITED STATES PATENTS 506,282 Timmis Oct. l0, 1893 (Other references on following page)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US507405A US3000010A (en) | 1955-05-10 | 1955-05-10 | Pressure suit |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US507405A US3000010A (en) | 1955-05-10 | 1955-05-10 | Pressure suit |
Publications (1)
Publication Number | Publication Date |
---|---|
US3000010A true US3000010A (en) | 1961-09-19 |
Family
ID=24018519
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US507405A Expired - Lifetime US3000010A (en) | 1955-05-10 | 1955-05-10 | Pressure suit |
Country Status (1)
Country | Link |
---|---|
US (1) | US3000010A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3164840A (en) * | 1961-02-27 | 1965-01-12 | Filtron Company Inc | Radiation protective garment |
US3284805A (en) * | 1964-04-30 | 1966-11-15 | Henry W Seeler | Combined cabin uniform and mechanical partial pressure suit complete with helmet |
US5072727A (en) * | 1988-06-06 | 1991-12-17 | Grumman Aerospace Corporation | Multi-purpose jerkin |
US6159574A (en) * | 1994-06-03 | 2000-12-12 | Fagerdala World Foams Ab | Laminated visco-elastic support |
US20110074380A1 (en) * | 2008-05-28 | 2011-03-31 | Silveray Co., Ltd. | Electric conduction pad and manufacturing method thereof |
US20160298933A1 (en) * | 2015-04-13 | 2016-10-13 | Umm Al-Qura University | Armored suit |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US506282A (en) * | 1893-10-10 | Illitjs augustus timmis | ||
US1965542A (en) * | 1933-11-24 | 1934-07-03 | Jr William Colvin | Fabric |
US1991601A (en) * | 1932-11-28 | 1935-02-19 | Lasaux Cecil F De | Stratosphere flying suit |
US2335474A (en) * | 1940-09-18 | 1943-11-30 | Herbert W Beall | Pressure producing apparatus |
GB591852A (en) * | 1941-09-13 | 1947-09-01 | Spencer Banbury Ltd | Improvements in or relating to protective garments particularly for aviators |
US2495316A (en) * | 1946-09-14 | 1950-01-24 | Clark | Garment or attachment for controlling the distribution, pressure, and circulation of body fluids |
US2531500A (en) * | 1948-02-13 | 1950-11-28 | Gen Motors Corp | Solenoid unit |
US2591030A (en) * | 1945-10-09 | 1952-04-01 | Berger Brothers Co | Solenoid-operated valve structure |
US2605065A (en) * | 1949-05-13 | 1952-07-29 | Robert W Wilkins | Net-suit, or combined g-suit, parachute, safety and crash harness |
US2664566A (en) * | 1951-06-22 | 1954-01-05 | Avo R Mianulli | Flexible shell suit |
US2670620A (en) * | 1950-08-29 | 1954-03-02 | Goldstaub Henry Herbert | Flexible electric heating element |
-
1955
- 1955-05-10 US US507405A patent/US3000010A/en not_active Expired - Lifetime
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US506282A (en) * | 1893-10-10 | Illitjs augustus timmis | ||
US1991601A (en) * | 1932-11-28 | 1935-02-19 | Lasaux Cecil F De | Stratosphere flying suit |
US1965542A (en) * | 1933-11-24 | 1934-07-03 | Jr William Colvin | Fabric |
US2335474A (en) * | 1940-09-18 | 1943-11-30 | Herbert W Beall | Pressure producing apparatus |
GB591852A (en) * | 1941-09-13 | 1947-09-01 | Spencer Banbury Ltd | Improvements in or relating to protective garments particularly for aviators |
US2591030A (en) * | 1945-10-09 | 1952-04-01 | Berger Brothers Co | Solenoid-operated valve structure |
US2495316A (en) * | 1946-09-14 | 1950-01-24 | Clark | Garment or attachment for controlling the distribution, pressure, and circulation of body fluids |
US2531500A (en) * | 1948-02-13 | 1950-11-28 | Gen Motors Corp | Solenoid unit |
US2605065A (en) * | 1949-05-13 | 1952-07-29 | Robert W Wilkins | Net-suit, or combined g-suit, parachute, safety and crash harness |
US2670620A (en) * | 1950-08-29 | 1954-03-02 | Goldstaub Henry Herbert | Flexible electric heating element |
US2664566A (en) * | 1951-06-22 | 1954-01-05 | Avo R Mianulli | Flexible shell suit |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3164840A (en) * | 1961-02-27 | 1965-01-12 | Filtron Company Inc | Radiation protective garment |
US3284805A (en) * | 1964-04-30 | 1966-11-15 | Henry W Seeler | Combined cabin uniform and mechanical partial pressure suit complete with helmet |
US5072727A (en) * | 1988-06-06 | 1991-12-17 | Grumman Aerospace Corporation | Multi-purpose jerkin |
US6159574A (en) * | 1994-06-03 | 2000-12-12 | Fagerdala World Foams Ab | Laminated visco-elastic support |
US20110074380A1 (en) * | 2008-05-28 | 2011-03-31 | Silveray Co., Ltd. | Electric conduction pad and manufacturing method thereof |
US20160298933A1 (en) * | 2015-04-13 | 2016-10-13 | Umm Al-Qura University | Armored suit |
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