| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 41 | Full-body stress transfer suit | US19015 | 1993-02-18 | US5659895A | 1997-08-26 | Thomas J. Ford, Jr. |
| A stress transfer garment for an individual in a low gravity environment to minimize bone deconditioning and the migration of fluids to the torso. The garment includes members made of elastic or resilient material which cover the torso and multiple limbs. The members extend down the long axis of the body, with each member interlaced with the member on each side at least once to form a mesh-like structure. The garment is fitted for an individual in a first position, preferably the fetal position. Any movement by a part of the body covered by the members from the fetal position, stretches those members. The stretched members deliver a physical strain along the long axis of the body to the underlying bone structure. The garment may also be designed to deliver a physical strain across the short axis of the body which is greater across the torso than the limbs and is sufficient to prevent body fluids from the limbs from migrating to the torso. The garment may be formed as a one-piece or two-piece garment. | ||||||
| 42 | Spacesuit sizing system | US553980 | 1990-07-17 | US5068919A | 1991-12-03 | Robert R. MacKendrick; Mario Gonsalves |
| A system for adjusting the size of a spacesuit is provided in which threaded rings of varying sizes are screwed into annular collars which are affixed to the section of the spacesuit whose size is to be adjusted. The rings and the collars include redundant interlocks designed to prevent inadvertent uncoupling of the components. In certain preferred embodiments, multi-start, centralizing, acme screw threads are used. | ||||||
| 43 | Pressure sealing bearing assembly for use in environmental control suits and environmental suits containing such bearing assemblies | US627455 | 1984-07-03 | US4596054A | 1986-06-24 | Robert R. MacKendrick; Dennis L. Finch |
| A bearing assembly for sealing the relatively rotatable adjoining portions of a pressurized environmental control suit for human use utilizes a pair of rotatable bearing members with an annular sealing member having a body portion and a lip portion extending from the body portion at an angle thereto. The lip portion includes an outer end portion of relatively thin cross section and a thicker portion disposed adjacent the body portion. The relatively thin outer end portion deflects in contact with the opposed surface and extends therealong to provide a seal therewith with relatively little friction. Upon conditions for extreme pressure differential, the thicker portion of the lip will be deflected to increase the amount of lip length bearing upon the surface of the opposed member to increase the sealing action. | ||||||
| 44 | Torso sizing ring construction for hard space suit | US684193 | 1984-12-20 | US4593415A | 1986-06-10 | Hubert C. Vykukal |
| A hard suit for use in space or diving applications having an adjustable length torso covering that will fit a large variety of wearers. The torso covering comprises an upper section and a lower section which interconnect so that the covering will fit wearers with short torsos. One or more sizing rings may be inserted between the upper and lower sections to accommodate larger torso sizes as required. Since access of the astronaut to the torso covering is preferably through an opening in the back of the upper section (which is closed off by the backpack), the rings slant upward-forward from the lower edge of the opening. The lower edge of the upper covering section has a coupler which slants upward-forward from the lower edge of the back opening. The lower torso section has a similarly slanted coupler which may interfit with the upper section coupler to accommodate the smallest torso size. One or more sizing rings may be inserted between the coupler sections of the upper and lower torso sections to accommodate larger torsos. Each ring has an upper coupler which may interfit with the upper section coupler and a lower coupler which may interfit with the lower section coupler. | ||||||
| 45 | Sequentially pressurized flight suit | US528567 | 1983-09-01 | US4583522A | 1986-04-22 | Armand Aronne |
| A valving system and modified anti-G flight suit are disclosed which operate in either of two modes. In an anti-blackout mode, pneumatic bladders in the flight suit are simultaneously inflated. In an anti-fatigue mode, the bladders are sequentially inflated in a repeated cycle so as to prevent pooling of blood and other body fluids in the leg and lower seat area. | ||||||
| 46 | Spacesuit torso closure | US780569 | 1977-03-23 | US4091465A | 1978-05-30 | Bruce W. Webbon; Hubert C. Vykukal |
| A separable entry closure assembly for joining axially separable tubular segments of a pressure suit along an angulated zone of separation having a first portion projected transversely beneath the axilla zone of the suit and a second portion projected behind the shoulder zone thereof and characterized by a first endless member of a rigid configuration affixed to one segment of the suit, a second endless member of a rigid configuration affixed to the other segment and mated in hermetically sealed relation with the first endless member, and a releasable "C" section clamp releasably securing the first endless member to the second endless member. | ||||||
| 47 | Porous polyethylene sheet | US29803572 | 1972-10-16 | US3865674A | 1975-02-11 | DULING IRL N; MERGES JR JOHN C |
| Disclosed is an opaque, porous polyethylene sheet. Molecular weight of the polyethylene is in excess of 500,000. The porous sheet is capable of receiving a permanent impression and the area receiving the impression becomes translucent. Method for preparing the sheet is described.
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| 48 | Flexible joint for pressurizable garment | US68945567 | 1967-12-11 | US3832735A | 1974-09-03 | ELKINS W; CONNELL E; ALESNA R |
| A flexible joint for a pressurizable garment has two fabric layers bonded together. The lay of one layer is straight cut and the other of bias cut. A ring-like tension member covered with Teflon disposed at the minor diameter of each joint convolution, is unrestrained other than being retained thereat in the flexure plane. A compression ring is secured at the major diameter, at certain of the convolutions, preferably alternate ones. A pair of axially disposed cable joint restraints at the convolution periphery are disposed in a plane normal to the flexure plane.
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| 49 | Spacesuit thigh restraint assembly | US3699589D | 1968-08-05 | US3699589A | 1972-10-24 | DURNEY GEORGE P |
| A thigh restraint assembly for a pressurized spacesuit which provides improved mobility for the wearer in the area of the thigh an crotch. It comprises thigh convolutes restrained by fabric covers and vertical thigh cables and reinforcement in combination with a plurality of crotch cables and cords passing through the crotch between the front and rear of the suit. The assembly cooperates with the torso and upper legs of the suit to maintain suit stability and to provide stress relief in the area of the joints. It cooperates with a torso block and tackle assembly to provide 90* of forward bending movement.
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| 50 | Temperature control system for space suit | US3648765D | 1970-11-24 | US3648765A | 1972-03-14 | STARR JAMES B |
| A temperature control system for a space suit having a warm fluid loop and a cold fluid loop with a mixing valve for adding fluid in the cold loop with fluid in the warm loop. A sensor is provided to control a throttle in the cold fluid loop for regulating the amount of fluid being added from the cold loop to the warm loop.
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| 51 | Underwater space suit pressure control regulator | US3636966D | 1969-10-24 | US3636966A | 1972-01-25 | ALDRICH BILLY R; COOPER CHARLES R; RASQUIN JOHN R |
| A device for regulating the pneumatic pressure in a ventilated space suit relative to the pressure imposed on the suit when being worn by a person underwater to simulate space environment for testing and experimentation. A box unit located on the chest area of the suit comprises connections for suit air supply and return lines and carries a regulator valve that stabilizes the air pressure differential between the inside and outside of the suit. The valve and thus suit pressure is controlled by the suit occupant and the valve includes a mechanism for quickly dumping the suit pressure in case of emergency. Pressure monitoring and relief devices are also included in the box unit.
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| 52 | Pressure suit load-relieved size-adjustment joints | US3628189D | 1970-06-22 | US3628189A | 1971-12-21 | MARRONI MICHAEL A JR; GETCHELL DOUGLAS E |
| Plug loads in a pressurized suit are transmitted across sizeadjusting joints in order to relieve convolute distortion which increases the torque required for flexing the various portions of the pressurized suit. In a first arm embodiment, the plug load restraint terminates in a rigid arm ring; in a second arm embodiment, the plug load restraint terminates in an eyelet which is laced in a fanned out fashion to the opposite side of the adjustment joint, thereby to spread the load to a substantially rigid wrist ring. In a leg embodiment, the plug load restraint of the knee section is joined to a plug load restraint of an ankle section directly, by an adjustable strap, the ankle section terminating in a load-distributing member near the sole of the boot.
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| 53 | Pressurized suit fabric convolute manipulation through material distribution | US3621542D | 1968-12-20 | US3621542A | 1971-11-23 | GETCHELL DOUGLAS E |
| ROOT CORDS IN FABRIC CONVOLUTES ARE DISPLACED RELATIVE TO THE GENERAL CENTER LINE OF RESTRAINT FABRIC MATERIAL OF WHICH A GENERALLY TUBULAR SECTION OF CONVOLUTES IS COMPRISED IN ORDER TO STABILIZE OR DISPLACE GIVEN CONVOLUTES WITH RESPECT TO OTHER CONVOLUTES IN THE SECTION. FURTHER, THE AMOUNT OF FABRIC ADJACENT TO VARIOUS INCREMENTAL LENGTHS OF A ROOT CORD IS ADJUSTED DIFFERENTIALLY SO AS TO ALTER THE CHARACTERISTICS OF ONE OR MORE CONVOLUTES FORMED THEREBY. THE INVENTION IS ILLUSTRATED IN TERMS OF OVERCOMING ADVERSE EFFECTS OF REPETITIVE BENDING OF JOINTS, AND IN TERMS OF OVER COMING A TENDENCY TOWARD CUTTING IN AS A RESULT OF WEDGE-SHAPED CONVOLUTES.
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| 54 | Pressurized suit-hip waist | US3574236D | 1968-12-20 | US3574236A | 1971-04-13 | GETCHELL DOUGLAS E; VAIL EDWIN G; MARRONI MICHAEL A JR; SMITH HARVEY A |
| A torso in a pressurized suit is joined to substantially parallel convolutes in the thighs of each leg by a hip-waist, or lower trunk portion which includes parallel convolutes substantially across the area from the groin to the waist, and a small number of shaped convolutes together with a sheer panel to form a hip and crotch transition between the parallel convolutes of the lower trunk and the parallel convolutes of the thighs. The shear panel may comprise three panels with the warp of the center panel perpendicular to the warp of the outer panels. A pair of doubly-crossed cables, from the center of the lower trunk in front through the crotch to the center of the lower trunk in the back, provide plug-load restraint.
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| 55 | Glove for a pressurized suit | US3564614D | 1968-12-20 | US3564614A | 1971-02-23 | GETCHELL DOUGLAS E; HARDY JOHN C; SMART JEROME C; BASTILLE SIMONE R |
| A GLOVE FOR A PRESSURIZED SUIT INCLUDES A PLURALITY OF FINGER STALLS JOINED TO A MAIN GLOVE RESTRAINT ASSEMBLY ALONG THE KNUCKLES AT THE REAR AND ALONG THE BREAK LINE OF THE PALM, EACH FINGER STALL COMPRISING AN INNER, FLEXIBLE BLADDER, A ONE-WAY STRETCH CLOTH PANEL PROVIDING HOOP LOAD RESTRAINT ACROSS THE BACK OF EACH STALL, RESTRAINT CLOTH ACROSS THE FRONT OF EACH STALM AND A PLEATED RESTRAINT CLOTH PROTECTION COVER OVER THE ONE-WAY STRETCH CLOTH ON THE BACK OF EACH STALL, A DIAMOND SHAPED, FOLDED WEB JOINS THE ROOT OF ONE STALL TO THE ROOT OF AN ADJACENT STALL, AND THE POSITION OF THE WEB IS STABILIZED BY RESTRAINT CORDS LEADING FROM THE CROTCH THUS FORMED BETWEEN ADJACENT STALLS AT THE FRONT AND THE REAR TO A POINT NEAR THE KNUCKLES ON THE BACK TRANK AND TO A POINT NEAR THE PALM BREAK LINE ON THE FRONT TRAK. LATERAL RESTRAINTS ARE PROVIDED IN PIPING WITHIN THE LATERAL SEAMS OF EACH SIDE OF EACH FINGER STALL, THE PIPING RUNNING ALONG THE REAR SEAM OF THE WEB AND THE RESTRAINT CORD THEREIN PASSING THROUGH A SECTION OF PIPING WHICH HOLDS THE REAR WEB STABILIZING RESTRAINT CORD AND TERMINATING AT AN ADJACENT POINT. THE MAIN GLOVE BODY IS COMPRISED OF A REAR TRANK, A PALM HEEL PANEL OR TRANK, AND A THUMB TRANSITION PIECE. A THUMB STALL IS FASHIONED IN A MANNER SIMILAR TO THAT AN INDIVIDUAL
FINGER STALL, BUT WITHOUT ANY WEBBING. LATERAL RESTRAINTS ON THE THUMB STALL ARE JOINED TOGETHER IN A TURNAROUND THAT CIRCUMSCRIBES THE BASE OF THE THUMB STALL. |
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| 56 | Pre-shaped cloth convolutes for a pressurized suit | US3564610D | 1968-12-20 | US3564610A | 1971-02-23 | MARRONI MICHAEL A JR; GETCHELL DOUGLAS E; KORABOWSKI JOHN J |
| ONE OR MORE ARCUATE PIECES OF FLAT CLOTH ARE SEWN TOGETHER TO FORM A FRUSTO CONE, TWO FRUSTO CONES BEING SEWN TOGETHER AT THEIR LARGE ENDS FROM A PRE-SHAPED CONVOLUTE. A PLURALITY OF PRE-SHAPED CONVOLUTES ARE SEWN TOGETHER SO AS TO FORM A CONVOLUTE SECTION OF A PRESSURIZED SUIT.
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| 57 | Space suit protective assembly | US3559209D | 1967-03-17 | US3559209A | 1971-02-02 | VAIL EDWIN G |
| A SPACE SUIT COMPRISING A HELMET FORMED OF AN UPPER AND A LOWER SECTION WITH A FLUID-TIGHT DETACHABLE CONNECTION IN THE REGION OF THE NECK, AN UPPER TORSO SECTION PERMANENTLY JOINED TO THE LOWER HELMET SECTION AND PROVIDED WITH ARM COVERINGS, A LOWER TORSO SECTION JOINED TO THE UPPER TORSO SECTION BY A DETACHABLE FLUID-TIGHT ZIPPERLIKE JUNCTION EXTENDING HORIZONTALLY AROUND THE REAR OF THE BODY AND CONVERGING UPWARDLY IN FRONT, THE UPPER TORSO SECTION BEING FORMED OF A WOVEN FABRIC POSITIONED ON A BIAS, THE LOWER TORSO SECTION BEING FORMED OF AN UPPER PORTION OF WOVEN FABRIC AND A LOWER CORRUGATED PORTION COVERING THE WAIST AND HIP JOINT REGION, THE LOWER CORRUGATED PORTION CARRYING LEG COVERINGS, AN INTEGRATED SYSTEM OF TENSILE MEMBERS CONNECTING EACH ARM COVERING WITH THE LOWER EDGE OF THE LOWER HELMET SECTION AND ANOTHER INTEGRATED SYSTEM OF TENSILE MEMBERS CONNECTING EACH LEG COVERING WITH THE JUNCTION BETWEEN THE FABRIC PORTION AND THE CORRUGATED PORTION OF THE LOWER TORSO SECTION.
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| 58 | Multi-chamber controllable heat pipe | US3543839D | 1969-05-14 | US3543839A | 1970-12-01 | SHLOSINGER ARNOLD P |
| 1,222,310. Space suits. TRW Inc. 30 Dec., 1969 [14 May, 1969], No. 63371/69. Heading A3V. [Also in Division F4] A space suit having a shell 88 of rigid non-flexible construction incorporates a controllable heat pipe (see Division F4 for details) to regulate the transmission of heat from the body of an astronaut to the exterior radiating surface of the space suit according to thermal conditions in the space environment. A resilient undergarment 96 is provided to cushion the astronaut's body from the shell so as to permit body expansion resulting from breathing or muscular activity. | ||||||
| 59 | Biological isolation garment | US3516404D | 1969-09-09 | US3516404A | 1970-06-23 | SPROSS FRED R |
| 60 | Emergency space-suit helmet | US3514785D | 1966-02-24 | US3514785A | 1970-06-02 | SMITH HARVEY A |
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