US1991601A - Stratosphere flying suit - Google Patents

Stratosphere flying suit Download PDF

Info

Publication number
US1991601A
US1991601A US644580A US64458032A US1991601A US 1991601 A US1991601 A US 1991601A US 644580 A US644580 A US 644580A US 64458032 A US64458032 A US 64458032A US 1991601 A US1991601 A US 1991601A
Authority
US
United States
Prior art keywords
suit
air
pressure
stratosphere
flying
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
Application number
US644580A
Inventor
Lasaux Cecil F De
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.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US644580A priority Critical patent/US1991601A/en
Application granted granted Critical
Publication of US1991601A publication Critical patent/US1991601A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • AHUMAN NECESSITIES
    • A62LIFE-SAVING; FIRE-FIGHTING
    • A62BDEVICES, APPARATUS OR METHODS FOR LIFE-SAVING
    • A62B17/00Protective clothing affording protection against heat or harmful chemical agents or for use at high altitudes
    • A62B17/008High-altitude pressure suits
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D10/00Flight suits
    • B64D2010/005High altitude suits or garments, e.g. partial or total pressure

Definitions

  • the invention relates to flying clothes tor use at great altitudes, as in the stratosphere, and has, for an object the provision of a suit within which a supply of iresh air can be maintainedat-a uniform pressure substantially that of the atmosphere at sea level, thereby furnishing an airman using the suit with the air necessary for comiortable breathing and avoiding the great discomfort experienced under rapid changes of pressure incident to steep climbs and fast dives.
  • the invention further consists in the several features hereinaiter described and claimed.
  • Fig. 2 is a detail transverse sectional view of iastening means for the suit
  • Fig. 3 is a detail sectional view of a detachable mask connection
  • Fig. 4 is a schematic diagram of the air supplying means tor the suit.
  • the numeral 10 designates .a one-piece suit which is formed of a flexible reinforced composition of rubber and fabric and which may be stayed if desired.
  • The'suit is made in step-in style and the trout has double walls 11 and 12 each closed by a slide-fastener 13, there being an interlocking connection 14 between the walls adapted to be sealed by pressure within the suit.
  • Elastic sealing bands 15 may be used around the arms and similar bands may, if desired, be used around the legs.
  • a hood or helmet 16 is formed on the suit and has a maskreceiving opening at its front provided with a surrounding bead 1'7 enclosing a wire 18.
  • a mask 19 is mounted in the hood in register with the hood opening and has a marginal bead 2d enclosing a wire 21.
  • the mask 19 is detachably secured to the hood by spring-urged locking levers 22, and the beads 17 and 20 are retained in sealing engagement by air pressure 'within the suit.
  • the mask carries goggles 23, preferably of the frost-proof type, a speaking unit 24 such as a microphonaand an emergency air outlet 25.
  • the suit is provided with a fresh air inlet 26 which is connected by an internal conduit 2'1 terminating near the mouth oi! the person using the suit.
  • Air cells 28 are formed in the suit to Fig. 1 is an elevation of a flying suit embodyfortable pressures may be used.
  • the pressure 15 front opening, and a vvision-aflording mask deform a life preserver and are adapted to be inflated by the-user through one or more tubes 29.
  • An air outlet 30 is carried on the top of the hood 15 and ear telephones 31 are carried at the sides of the hood.
  • the Iresh air for the suit is supplied by a suitable air compressor 32, here indicated to be driven by an air screw 33.
  • the air is delivered through a pressure regulator 34 and an airrfllter. 35 and thence through a flexible conduit ⁇ 36 to the suit. 10
  • the outgoing foul air passes through a pressure regulator 37 maintaining the air within the suit at a predetermined pressure, preferably that 01' the atmosphere at sea level, although other comregulator 37 may be embodied in the air outlet 30 on the helmet.
  • the air entering the compressor is quite cold at great altitudes, but is heated by compression and agitation in the compressor and may be further heated it desired. 20
  • the proportion of oxygen in the, atmosphere is substantially the same up to an altitude of about 120,000 ieet so that when the rarefied air is compressed-to sea level pressure, the normal proportion or oxygen will be present.
  • the 25 suit may be electrically heated in any well-known manner.
  • a flying'sult for great altitudes comprisin 30 an envelope adapted to iit about a wearer and adapted to hold air at a pressure substantially greater than the ambient rarefle'd air, said suit having a head-receiving hood provided with a 35 tachably covering said opening and,bearing at its edges against the inner surface oi. the hood to resist air pressure within the hood.
  • a flying suit for great altitudes comprising an envelope to flt about a wearer and to hold air 40 ata pressure greater than the surrounding air pressure, said envelope having inner and outer walls with a separable interlocking connection multiple-operated envelope.

Description

' Feb. 19, 1935.
c. F. DE LASAUX STRATOSPHERE FLYING SUIT Filed Nov. 28, 1932 AIR COMPRESSOR PRESSURE REGULATOR AIR FILTER SUIT \ PRESSURE R EG U LATOR IgVENTOR TORNE;
Patented Feb. 19, 1935 UNITED STATES PATENT OFFICE 1,991,601 s'ras'rosrnnan FLYING sm'r Cecil F. De Iasaux, Milwaukee, Wis Application November 28, 1932, Serial No. 844,580
The invention relates to flying clothes tor use at great altitudes, as in the stratosphere, and has, for an object the provision of a suit within which a supply of iresh air can be maintainedat-a uniform pressure substantially that of the atmosphere at sea level, thereby furnishing an airman using the suit with the air necessary for comiortable breathing and avoiding the great discomfort experienced under rapid changes of pressure incident to steep climbs and fast dives. The invention further consists in the several features hereinaiter described and claimed.
In the accompanying drawing,
ing the invention;
Fig. 2 is a detail transverse sectional view of iastening means for the suit;
Fig. 3 is a detail sectional view of a detachable mask connection, and Fig. 4 is a schematic diagram of the air supplying means tor the suit.
In this drawing, the numeral 10 designates .a one-piece suit which is formed of a flexible reinforced composition of rubber and fabric and which may be stayed if desired. The'suit is made in step-in style and the trout has double walls 11 and 12 each closed by a slide-fastener 13, there being an interlocking connection 14 between the walls adapted to be sealed by pressure within the suit. Elastic sealing bands 15 may be used around the arms and similar bands may, if desired, be used around the legs. A hood or helmet 16 is formed on the suit and has a maskreceiving opening at its front provided with a surrounding bead 1'7 enclosing a wire 18.
' A mask 19 is mounted in the hood in register with the hood opening and has a marginal bead 2d enclosing a wire 21. The mask 19 is detachably secured to the hood by spring-urged locking levers 22, and the beads 17 and 20 are retained in sealing engagement by air pressure 'within the suit. The mask carries goggles 23, preferably of the frost-proof type, a speaking unit 24 such as a microphonaand an emergency air outlet 25.
The suit is provided with a fresh air inlet 26 which is connected by an internal conduit 2'1 terminating near the mouth oi! the person using the suit. Air cells 28 are formed in the suit to Fig. 1 is an elevation of a flying suit embodyfortable pressures may be used. The pressure 15 front opening, and a vvision-aflording mask deform a life preserver and are adapted to be inflated by the-user through one or more tubes 29.
An air outlet 30 is carried on the top of the hood 15 and ear telephones 31 are carried at the sides of the hood.
The Iresh air for the suit is supplied by a suitable air compressor 32, here indicated to be driven by an air screw 33. The air is delivered through a pressure regulator 34 and an airrfllter. 35 and thence through a flexible conduit {36 to the suit. 10
The outgoing foul air passes through a pressure regulator 37 maintaining the air within the suit at a predetermined pressure, preferably that 01' the atmosphere at sea level, although other comregulator 37 may be embodied in the air outlet 30 on the helmet. The air entering the compressor is quite cold at great altitudes, but is heated by compression and agitation in the compressor and may be further heated it desired. 20
The proportion of oxygen in the, atmosphere is substantially the same up to an altitude of about 120,000 ieet so that when the rarefied air is compressed-to sea level pressure, the normal proportion or oxygen will be present. If desired, the 25 suit may be electrically heated in any well-known manner. 1 I
what I claim as new and desire to secure by Letters Patent is:
1. A flying'sult for great altitudes comprisin 30 an envelope adapted to iit about a wearer and adapted to hold air at a pressure substantially greater than the ambient rarefle'd air, said suit having a head-receiving hood provided with a 35 tachably covering said opening and,bearing at its edges against the inner surface oi. the hood to resist air pressure within the hood.
2. A flying suit for great altitudes comprising an envelope to flt about a wearer and to hold air 40 ata pressure greater than the surrounding air pressure, said envelope having inner and outer walls with a separable interlocking connection multiple-operated envelope.
I CECE- F. DE LASAUX.
US644580A 1932-11-28 1932-11-28 Stratosphere flying suit Expired - Lifetime US1991601A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US644580A US1991601A (en) 1932-11-28 1932-11-28 Stratosphere flying suit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US644580A US1991601A (en) 1932-11-28 1932-11-28 Stratosphere flying suit

Publications (1)

Publication Number Publication Date
US1991601A true US1991601A (en) 1935-02-19

Family

ID=24585497

Family Applications (1)

Application Number Title Priority Date Filing Date
US644580A Expired - Lifetime US1991601A (en) 1932-11-28 1932-11-28 Stratosphere flying suit

Country Status (1)

Country Link
US (1) US1991601A (en)

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2417177A (en) * 1947-03-11 High altitude flying suit
US2433768A (en) * 1942-05-29 1947-12-30 Goodrich Co B F Inflatable suit
US2449683A (en) * 1943-04-16 1948-09-21 John D Akerman Differential pressure valve
US2478765A (en) * 1947-10-06 1949-08-09 Chan J Kim Cocoon sun sweat suit
US2521767A (en) * 1944-07-17 1950-09-12 Dorothy Zecha Garment
US2647507A (en) * 1944-10-02 1953-08-04 Hubert K Shaw Buoyant, regulated-temperature weather-suit
US2761515A (en) * 1955-05-02 1956-09-04 Union Carbide & Carbon Corp Process and apparatus for fire protection
US2877966A (en) * 1955-03-30 1959-03-17 Garrett Corp Common oxygen supply for engine and cabin of high altitude aircraft
US3000010A (en) * 1955-05-10 1961-09-19 Kinghurst Ltd Pressure suit
DE1202141B (en) * 1957-12-09 1965-09-30 Siegfried Ruhnke Protective suit, which has parts designed as cavities for receiving breathing gas
US3777750A (en) * 1970-07-24 1973-12-11 Com A L En Atomique Protective clothing unit for conducting work in a deleterious atmosphere
FR2614538A1 (en) * 1987-04-28 1988-11-04 Grizard Jean Ventilated hood, in particular for civil, military or medical protection
US4800867A (en) * 1984-06-25 1989-01-31 Robert Owens Foot comforter
RU2776329C1 (en) * 2022-01-27 2022-07-18 Акционерное общество "Научно-производственное предприятие "Звезда" имени академика Г.И. Северина" System for pilot's personal protection in unpressurized cockpit when flying in stratosphere

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2417177A (en) * 1947-03-11 High altitude flying suit
US2433768A (en) * 1942-05-29 1947-12-30 Goodrich Co B F Inflatable suit
US2449683A (en) * 1943-04-16 1948-09-21 John D Akerman Differential pressure valve
US2521767A (en) * 1944-07-17 1950-09-12 Dorothy Zecha Garment
US2647507A (en) * 1944-10-02 1953-08-04 Hubert K Shaw Buoyant, regulated-temperature weather-suit
US2478765A (en) * 1947-10-06 1949-08-09 Chan J Kim Cocoon sun sweat suit
US2877966A (en) * 1955-03-30 1959-03-17 Garrett Corp Common oxygen supply for engine and cabin of high altitude aircraft
US2761515A (en) * 1955-05-02 1956-09-04 Union Carbide & Carbon Corp Process and apparatus for fire protection
US3000010A (en) * 1955-05-10 1961-09-19 Kinghurst Ltd Pressure suit
DE1202141B (en) * 1957-12-09 1965-09-30 Siegfried Ruhnke Protective suit, which has parts designed as cavities for receiving breathing gas
US3777750A (en) * 1970-07-24 1973-12-11 Com A L En Atomique Protective clothing unit for conducting work in a deleterious atmosphere
US4800867A (en) * 1984-06-25 1989-01-31 Robert Owens Foot comforter
FR2614538A1 (en) * 1987-04-28 1988-11-04 Grizard Jean Ventilated hood, in particular for civil, military or medical protection
RU2776329C1 (en) * 2022-01-27 2022-07-18 Акционерное общество "Научно-производственное предприятие "Звезда" имени академика Г.И. Северина" System for pilot's personal protection in unpressurized cockpit when flying in stratosphere

Similar Documents

Publication Publication Date Title
US1991601A (en) Stratosphere flying suit
US3680556A (en) Diving helmet
US3438060A (en) Airmen's helmets
US2861568A (en) Pressurized helmet for aviators
SE7908851L (en) DIVING EQUIPMENT
US2465973A (en) High elevation mask
US2303155A (en) Diving mask and apparatus
US1364104A (en) Gas-mask
US2568316A (en) Swim goggles
US3130415A (en) Helmet assembly with face seal and adjustment means therefor
US2001673A (en) Submarine lifesaving outfit
US1310825A (en) Respiratory apparatus
US1930399A (en) Helmet for divers, miners, firemen, and the like
US1742368A (en) Buoyant swimming suit
US1618347A (en) Life preserver
US3695262A (en) Lifesaving helmet
US2868195A (en) Oxygen mask
US2944544A (en) Respirators, particularly for submarine use
RU194375U1 (en) OXYGEN OXYGEN MASK WITH HYPOXIC HYPOXIA HAZARD SIGNALS
RU194655U1 (en) AVIATION OXYGEN MASK WITH A DIGITAL INDICATOR OF RESERVE CONSCIOUSNESS TIME
US3480967A (en) Pneumatic bathing cap
GB510491A (en) Improvements relating to gas masks
US2336979A (en) Aviation mask
US2861567A (en) Pressurized helmet for aviators
US2587958A (en) Hood for divers' suits