WO2013118145A2 - Appareil repliable portable destiné au transport mains libres d'une pluralité de charges utiles, y compris d'êtres humains, et escamotable sur le corps du sauveteur, système et procédés associés - Google Patents

Appareil repliable portable destiné au transport mains libres d'une pluralité de charges utiles, y compris d'êtres humains, et escamotable sur le corps du sauveteur, système et procédés associés Download PDF

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Publication number
WO2013118145A2
WO2013118145A2 PCT/IN2013/000055 IN2013000055W WO2013118145A2 WO 2013118145 A2 WO2013118145 A2 WO 2013118145A2 IN 2013000055 W IN2013000055 W IN 2013000055W WO 2013118145 A2 WO2013118145 A2 WO 2013118145A2
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WO
WIPO (PCT)
Prior art keywords
payload
unit
rescuer
arms
fastening
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PCT/IN2013/000055
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English (en)
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WO2013118145A3 (fr
Inventor
Aslam Sharief MUHAMMED
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Muhammed Aslam Sharief
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Application filed by Muhammed Aslam Sharief filed Critical Muhammed Aslam Sharief
Publication of WO2013118145A2 publication Critical patent/WO2013118145A2/fr
Publication of WO2013118145A3 publication Critical patent/WO2013118145A3/fr

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Classifications

    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61GTRANSPORT, PERSONAL CONVEYANCES, OR ACCOMMODATION SPECIALLY ADAPTED FOR PATIENTS OR DISABLED PERSONS; OPERATING TABLES OR CHAIRS; CHAIRS FOR DENTISTRY; FUNERAL DEVICES
    • A61G1/00Stretchers
    • A61G1/013Stretchers foldable or collapsible
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62BHAND-PROPELLED VEHICLES, e.g. HAND CARTS OR PERAMBULATORS; SLEDGES
    • B62B1/00Hand carts having only one axis carrying one or more transport wheels; Equipment therefor
    • B62B1/18Hand carts having only one axis carrying one or more transport wheels; Equipment therefor in which the load is disposed between the wheel axis and the handles, e.g. wheelbarrows
    • B62B1/20Hand carts having only one axis carrying one or more transport wheels; Equipment therefor in which the load is disposed between the wheel axis and the handles, e.g. wheelbarrows involving parts being collapsible, attachable, detachable or convertible
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62BHAND-PROPELLED VEHICLES, e.g. HAND CARTS OR PERAMBULATORS; SLEDGES
    • B62B5/00Accessories or details specially adapted for hand carts
    • B62B5/06Hand moving equipment, e.g. handle bars
    • B62B5/068Connections to the body for moving the cart, e.g. harnesses
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B62LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
    • B62BHAND-PROPELLED VEHICLES, e.g. HAND CARTS OR PERAMBULATORS; SLEDGES
    • B62B2202/00Indexing codes relating to type or characteristics of transported articles
    • B62B2202/42Persons or animals, dead or alive

Definitions

  • This invention relates to the field of transporting and transferring payloads in a quick and efficient manner; more particularly to manual transport and transfer of humans especially in emergencies entailing constraints of time, safety, additional manpower and specialised equipment, among others.
  • the commonly used transport/transfer systems and apparatus employed in non-combat environments include at least two or more hands (manpower), a stretcher or such other device that more often than not, occupies considerable space besides being unwieldy, to secure, transport and transfer the injured/sick.
  • Professional rescuers such as fire-fighters, military personnel etc., undergo specialised and intensive training and discipline to handle emergency rescue operations with ad hoc kits and accoutrements to bundle- and-drag/package-and-move or lift the injured or deceased from one place to another.
  • quality training and discipline is lacking in staff of civilian hospitals, due to economic, operational, among other reasons.
  • the bundle- and-drag/package-and-move methods used by fire- fighters or military personnel serve mainly the purpose of moving/transporting the injured/deceased over a very short distance only, since it is neither feasible nor safe to drag a human over long distances especially over uneven, wet or untrodden terrain, in which case the only alternative is to physically carry the injured/deceased to the destination - which is a tiresome and tedious proposition and which entails the total engagement of at least one arm of the rescuer, besides engaging his focus to keep his balance and pace etc., which compromise the rescuers safety as well, in the incendiary/combat arena.
  • an average human adult can at best carry one injured/deceased adult at a time and run/walk, which would at least double his time to cover the same distance, as without the load.
  • the structure, shape, size and weight of an adult human renders him all the more unwieldy especially when his body is limp due to injury/death. This could mean each injured person requires one ad hoc, robust and willing rescuer, in an emergency - which (ratio of 1 : 1) is highly improbable in most emergency circumstances where damage to life and limb is rapid and severe.
  • the aspect of being a four-wheeled stretcher greatly reduces its manoeuvrability and navigability as also the comfort accorded to the injured during transport on uneven terrain due to the rigid chassis that bears the payload.
  • the relatively long time it would take to secure the injured with straps on to the stretcher is another disadvantage especially in view of the shortage of time and hands (manpower) during emergencies such as in the battle field or fire accidents.
  • a further drawback is its relative infeasibility when the payload is to be airlifted.
  • Another main object of this invention is to design, construct and develop a cost It is therefore the main object of this invention to provide for an efficient, cost-effective, portable, collapsible apparatus, system and method/s for simple and quick, single- handed, hands-free, manual simultaneous transport and transfer of multiple payloads including humans, with minimal effort, that is light and stow-able on the person of the rescuer.
  • PLCE Personal Load Carrying Equipment
  • payload e.g., injured humans
  • a relatively rigid component being a highly collapsible system of at least two arms that supports a relatively flexible component; each arm comprising a plurality of elements that can be stretched out, or collapsed to occupy minimal space; each said element is provided with means to be fastened to the said relatively flexible component; the said arms converge toward their distal ends where they meet and get attached to means to reduce friction by such joint that allows for the necessary play/movement along the X and Y axes for the said two arms to be spliced/jointed at their proximal ends and to be separated, to facilitate transfer, loading and unloading of the payload.;
  • a relatively flexile component being means to bear, support and cushion the payload, wherein the said flexible component is attached/secured to the said elements such that it does not hinder, hamper or tangle when the said elements rotate, collapse or stretch out, but stretches out and collapses in conjunction with the said elements; and further such that when the proximal ends of the said arms of the said rigid component are joined together or spliced and suspended vertically, the payload if any contained therein is not only snugly cocooned and secured from falling out, but is also not squeezed or crushed, while its overall posture/shape is preserved intact;
  • the said relatively flexile component is optionally further provided with a Substructure to support the payload in order to prevent it from buckling
  • the said substructure comprises a plurality of members which are collapsibly fastned one to another such that the maximum swing/pivotal/rotation about a given joint is about 180 degrees and suspended from the said arms by either flexible or rigid means whereby, when stretched out under the weight of the payload, the said members of the substructure form a plain surface; and wherein the said flexile component is attached/secured to the said members such that they do not hinder, hamper or tangle when the said elements rotate, collapse or stretch out, but stretch out and collapses in conjunction with the said elements;
  • Anchoring means provided at one (proximal) end of the said relatively rigid component, that aid in anchorage of the said unit (in)to a Fastening means of a Fastening-apparatus, comprising; (i)(c)(a) a vertical arm - being a cylinder or polyhedron that fits into the said fastening means; (i)(c)(b) a flexible or resilient means that connects the upper end of the said vertical arm to the said first/proximal element of a given arm and allows for vertical, horizontal play/movement of the said arm, and being made up of such flexible resilient material that can withstand and absorb the shock caused due to the walking/running/movement of the rescuer while the payload is pulled/pushed; the said flexible or resilient means makes an acute angle with the said vertical arm of the Anchoring means so as to form a hook-like structure to facilitate simple engagement of airlifting or other gear; the said anchoring means is further provided with suitable mechanism to be locked to and unlocked from the said fastening means;
  • the said Apparatus when stretched out, with the proximal end fastened/clung to the body of the rescuer through the Fastening means, transports a human or other payload in a reclining, recumbent or vertical posture/position, being light, highly collapsible, so as to be stowed on the person of a rescuer, by forming part of his personal gear/outfit and wherein a system of more than one such units can be effectively engaged by a single rescuer simultaneously.
  • FIGURE 1 describes the apparatus and system comprising four units, collapsed and stowed on the person of a rescuer as part of his outfit/gear.
  • FIGURE 2 describes one stretched out unit, fastened to the Fastening apparatus on the shoulder of a rescuer who is transporting the human payload, hands-free.
  • FIGURE 3 describes four personnel engaging one stretched-out unit each, viz., (i) front-shoulder; (ii) front-waist; (iii) rear-shoulder; and (iv) rear-waist.
  • FIGURE 4 describes a single individual engaging four different stretched-out units viz., (i) front-shoulder; (ii) front-waist; (iii) rear-shoulder; and (iv) rear-waist.
  • FIGURE 5 describes a close-up of the proximal end of a single element of an arm, being a hollow cylindrical tube with a transverse constriction around which is the Ring bearing a loop (being the means for fastening the netting to the rigid arm)
  • FIGURE 6 describes a longitudinal view of an arm showing a plurality of elements, each bearing a Ring and a Loop.
  • FIGURE 7 describes the Anchoring means comprising the vertical arm and the resilient means making an acute angle; connected to the l st /proximal element of the rigid component (or arm).
  • FIGURE 8 describes the close-up of the resilient means of the Anchoring means, bearing the swivelling means, connected to the rotary means being (i) a motor and (ii) a spindle with two draw-strings.
  • FIGURE 9 describes two rescuers, facing opposite directions, engaging a single unit each to transport human payloads, down the stairs.
  • FIGURE 10 describes a rescuer engaging a single unit to transport a human payload up the stairs, by turning the unit up-side down such that the caster/wheel is not in contact with the terrain.
  • FIGURE 1 1 describes a long shot of a human payload being airlifted vertically with the rigid arms of the unit spliced together.
  • FIGURE 12 describes a close-up of the airlifting gear (rope) from an aircraft, fastened to the hook-like structure formed by the acute angle made by the resilient means with the vertical arm of the Anchoring means of a unit.
  • FIGURE 13 describes a plurality of disassembled 'members' or Slats that form the 'Substructure' which is an optional accessory to the Unit.
  • FIGURE 14 describes the assembled Substructure comprising a plurality of 'members' or Slats that are hinged together to form a flat surface when stretched out.
  • FIGURE 15 describes the collapsed Substructure wherein the elastic/resilience means tend to collapse the Slats.
  • FIGURE 16 describes the apparatus and system comprising four units, bearing the optional Substructure, collapsed and stowed on the person of a rescuer as part of his outfit/gear.
  • FIGURE 17 describes a stretched out unit, showing the Substructure, along with optional Unloading gear, being Broad Strap(s) with tapering ends velcroed to a given member/Slat of the Substructure
  • FIGURE 18 describes the Spliced arms of a unit, carrying a human payload, anchored into the fastening means of the Fastening apparatus which forms part of the rescuer's outfit.
  • FIGURE 19 describes Step I to lift the Unit (with spliced arms) bearing a human payload, so as to carry it in a horizontal position, wherein, the region of the substructure corresponding to the midsection of the human payload is placed on the shoulder by rolling the distal end of the unit closer to the rescuers body while lifting its proximal end.
  • FIGURE 20 describes a Human payload being carried in horizontal position, (Step II), being the suitable method of transfer and transport especially while wading water or across such other forest or rugged terrain.
  • Air-lifting gear (Rope)
  • a Slat being one of the members of the Substructure
  • This invention anticipates material/s (including metals such as steel, aluminium, and various other metals and metallic alloys and other combinations, reinforced plastic, fiber-plastic, leather, rubber, PVC, their various forms, adaptations and versions and other materials) commonly used in the art for manufacture of medical or other transport equipment, and its parts, including fastening means etc., Also anticipated are materials used in the art for the manufacture of durable, heavy duty strings Or cords that can bear heavy loads and that are resilient to the required or suitable degree, while possessing anti-slip texture/properties. Obvious and rather trivial details that do not warrant specific mention and which are known and obvious to a person skilled in the art are not mentioned and/or explained and/or drawn, while they are very much a part of this invention. The description herein therefore shall not be construed to unduly limit the intended scope and extent of the invention. Meanings of important terms used:
  • 'Unit' comprises 1(a), 1(b), 1(c), 1(d), 1(e), 1(f) described herebelow.
  • 'Apparatus' comprises one unit, and the fastening-apparatus, which forms part of the rescuers outfit/gear, and which bears the fastening means.
  • 'System' comprises the plurality of Apparatus that one rescuer can don and engage simultaneously or otherwise, with or without a payload.
  • 'Rescuer' means preferably a human, but includes a machine, robot and an animal engaged in a rescue operation.
  • each unit of the system comprising;
  • a relatively rigid component being a highly collapsible system of at least two arms [1] that supports a relatively flexible component - being the netting [14] described hereinbelow; each arm [1] comprises a plurality of (about 10 - 11) elements [2] that can be stretched out, or collapsed to occupy minimal space;
  • Each said element [2] of the arm [1] being a hollow cylindrical pipe about 8 inches in (total) length, and wherein one (distal) end is flanged into a Collar about 0.5 inches in length and with an outer diameter (of about 0.05 inches) greater than the diameter of the rest of the respective element [2].
  • the arrangement of the said elements [2] is telescoping such that the last element [4] (at the distal end of a given arm) has the smallest diameter and snugly fits into the lumen of the preceding element [2] which has a marginally greater diameter, and the first (or proximal) element [3] of an arm [1] has the largest diameter (without limitation) of about 1.25 inches.
  • the said collar bears a transverse constriction [5] of about 0.25 inches in length and 0.05 inches in depth) on its outer surface to accommodate a Ring [6] that rotates freely around but is restricted within the said transverse constriction [5].
  • the said Ring [6] bears on its outer edge, a Loop [7] of about 0.2 inch diameter.
  • Each said element [2] or hollow cylindrical pipe bears screw threads (not shown in drawings), both on its outer surface and its inner surface along its length excepting the said collar.
  • the 'lead' of the said threads is preferably wide (about 4 inches, without limitation) so as to enable greater degree of telescopic extension and collapse per rotation.
  • Each said element [2] or hollow cylindrical pipe has a transverse circular ridge (not shown in drawings) around the outer surface at its proximal end and another transverse circular ridge in its inner surface at its distal end just before the flange/collar such that each element [2] (except the 1 st or proximal element [3]) is permanently locked to the preceding element [2] of next higher diameter (by the said transverse circular ridges) thereby restricting its movement from coming free of the preceding element [2] of next higher diameter but allowing for its slide- able/telescopic/rotary movement within.
  • the proximal ends of the said arms [1] are attached to Anchoring means [8].
  • the said arms [1] converge toward their distal end where they meet and get attached to the means to reduce friction - being preferably a swivel-able caster or wheel [22], thereby forming a triangular stretcher.
  • the joint where the distal ends of the said arms [1] meet with each other and with the said caster [22], is such that it allows for the necessary play/movement along the X and Y axes for the said two arms to be spliced/jointed at their proximal ends.
  • Such joint is without limitation at least one pivot joint or a hinge joint or ball and socket joint or any combination of thereof, so as to facilitate the transfer, loading and unloading of the payload.
  • the material that the said elements [2] are made of is, without limitation - metal (steel) or alloys or plastic or P VC, Fibre-plastic or reinforced plastic or combinations of such other material known in the art that is light and capable of withstanding the weight of the payload and makes a smooth surface that offers minimal friction during extension or collapse of the said elements [2].
  • a relatively flexile component being means to bear, support and further cushion the payload, which is preferably (without limitation) a netting [14] made of light weight, and preferably all-weather durable material with the desired degree of elasticity such as but not limited to nylon, spliced with rubber or such other suitable material/s or combination/s thereof known in the art, wherein each end of every main/transverse strand of the net [14] is tied/secured to the said loop [7] attached to the said Ring [6] referred above, such that every main transverse strand connects one element [2] of a given arm [1] to the corresponding element [2] of another.
  • a netting [14] made of light weight, and preferably all-weather durable material with the desired degree of elasticity such as but not limited to nylon, spliced with rubber or such other suitable material/s or combination/s thereof known in the art, wherein each end of every main/transverse strand of the net [14] is tied/secured to the said loop [7
  • Each said main/transverse strand is further connected to adjacent strands by means of longitudinal strands so as to form a net [14] to effectively bear the weight of the payload.
  • the said netting [14] so formed is in the form of a triangular narrowing hammock characterised by a structure that provides for the centre of gravity of the payload to rest rather toward the distal end of the said rigid arms [1], and further such that when the proximal ends of the said arms [1] (of the rigid component described above) are joined together or spliced and suspended (vertically) from the said proximal end, the payload (especially but not limited to human [23]) contained in the said netting [14] is not only snugly cocooned and secured from falling out, but is also not squeezed or crushed, while its overall posture is preserved intact,
  • the said unit is further provided with a mechanism to automatically stretch out and automatically collapse by actuating the required mechanism
  • the 1 st (proximal element [3]) of each arm [1] is connected directly or indirectly to a rotary device such as a motor [15] and/or a draw string/s [19] wound on a spindle [17] such that the rotating motion in a given direction of (at least) the second last element [2] causes the said second last element [2] to unscrew or unwind itself from the last (distal) element [4] and once the said second last element [2] unscrews itself from its succeeding/last element [4] and ceases to rotate, the third last element [2] unscrews itself from the said second last element [2] and so on until the first (proximal element [3]) of each arm unscrews itself from its succeeding element [2] thereby causing the collapsed arms [1] of the unit to stretch out.
  • a rotary device such as a motor [15]
  • the said unscrewing and screwing of elements [2] is effectively brought about due to the fact that on the one hand, the 1 st element [2] is freely swivel-able about its longitudinal axis at its proximal end wherein it is connected to the anchoring means [8] by a swivelling joint [12], which in turn is connected to the rotary device, and on the other hand the last or distal element [4] of each arm is nonrotary since it is fixed to the last or distal element [4] of the other arm and also to the head of a swivelling castor or wheel [22], and the stretching out and collapse is further brought about by the screw threads on the inner and outer ' surfaces of each element [2].
  • two draw-strings [19] are also wound around a spindle [17] connected to the said swivelling means [12] which in turn is connected to the proximal end of each 1 st proximal element [3] such that when one of the said draw-string [19] is manually pulled, it unwinds to rotate the spindle [17] and in turn rotates the said 1 st proximal element/s [3] in a given direction; and like wise when the other draw-string [19] is pulled it causes rotation of the spindle [17], the said swivelling means [12] and the said 1 st proximal elements [3] in the opposite direction, thereby bringing about the stretching out and collapse of the arms [1] of the unit.
  • the said spindle [17] is coaxially placed just behind the swivelling means [12] and is connected to it through a hollow cylindrical tube [18] which can disengage and engage the said swivelling means [12] when a draw-string [19] is to be pulled.
  • One end of each of the said draw strings [19] (wound in opposite directions) is permanently fixed to the said spindle [17] while the other end of each drawstring [19] is free to be pulled/drawn.
  • the shaft [16] of the motor [15] that connects the swivelling means [12] runs through the said hollow cylindrical tube [18] such that the motor [15] engages the said swivelling means [12], without engaging the said spindle [17].
  • Anchoring means [8] provided at one (upper/proximal) end of the said relatively rigid component, that aid in anchorage of the said unit (in)to the Fastening means [21] of the Fastening-apparatus [20]; - comprising (a) a vertical arm [9] - being a cylinder or cylindrical polygon or polyhedron made of light and strong material - that fits into a fastening means [21] or hole or mortise; (b) a flexible or resilient means [10] that connects the upper end of the said vertical arm [9] to the said first/proximal element [3] of a given arm [1] (rigid component) and allows for vertical, horizontal play/movement of the said arm [1] - being made up of either a cylindrical piece of (without limitation) rubber or such other flexible resilient material optionally reinforced/supported with metal wire, or a metal spring or such other material or structure that can withstand the stress caused when the payload is pulled/pushed and that can absorb the shock caused due to the walking
  • the said flexible or resilient means [10] makes an preferably acute ( ⁇ 90 degrees) angle with the said Vertical arm [9] of the Anchoring means [8] so as to form a hook-like structure [1 1] to facilitate simple engagement of airlifting gear [24] or other gear or rope or knot, when the unit along with its payload is to be transported/transferred.
  • the said anchoring means [8] is further provided with suitable mechanism known in the art to be locked to and unlocked from the said fastening means [21] such as by (without limitation) a press lock, (or push lock or a carter pin).
  • the other end of the said flexible or resilient means [10] is further provided with a swivelling means [12] which in turn is permanently fixed to the upper end of the said first/proximal element [3] of each arm [1] such that when the said swivelling means [12] rotates, the said first/proximal element [3] also rotates.
  • the said vertical arm [9] is further provided with a power source such as a battery which can be seated preferably within its hollow space and which is connected to the said motor [15].
  • One or both of the said vertical arms [9] of the said anchoring means [8] is further provided with simple clamping or clipping means at the upper end such that the two arms [1] of the said rigid component can be spliced and clamped together by pushing one member of the said clipping/clamping means located on one of the said vertical arm [9] into/against another, wherein the said clipping/clamping means is without limitation a pipe clip or spring clamp, (e) A rotary means being, preferably but not limited to, (i) an electric motor [15] (preferably one for each arm) which is embedded in the said flexible or resilient means [10] and is connected to the said swivelling means [12], and (ii) Two draw-strings [19] wound (in opposite directions) around a spindle [17] which is coaxially connected to the said swivelling means [12], such that when one of the said draw-string [19] is pulled, the spindle [17] (and so the swivelling means [12
  • Both rotary means (i) and (ii) are embedded within the flexible/resilient means [10] as shown in the drawings.
  • the means to actuate the motor [15], being a switch (not shown in the drawings) is also located on the said flexible/resilient means [10].
  • the said Apparatus is triangular when stretched out, with the proximal end fastened/clung to the body of the rescuer through the Fastening means [21], transports a human [23] in a reclining posture/position while for instance being transported on ground, and can transfer the human [23] in a vertical position while for instance being air-lifted, being light, highly collapsible (when not in use), so as to be stowed on the person of a rescuer, by forming part of his personal gear/outfit and wherein more than one such units can be effectively engaged by a single rescuer simultaneously.
  • METHOD/S OF OPERATING THE PREFERRED EMBODIMENT METHOD/S OF OPERATING THE PREFERRED EMBODIMENT:
  • the rotary mechanism may be either a battery powered motor [15] or the manual draw-strings [19] wound around the spindle [17], embedded in the Flexible/resilient means [10] of the Anchoring means [8].
  • the Rescuer is now ready to comfortably transport at least (without limitation) up to 4 payloads (e.g., humans [23]) on (without limitation) at least 4 units on his person.
  • payloads e.g., humans [23]
  • a single rescuer donning the said (collapsed) System and Apparatus arrives at the spot and executes steps (a), (b), (c) and (d) above wherein he chooses to either push the payload by engaging the Unit/s in the from (ahead of him) or pull the payload by engaging the Unit/s behind him; In case of unfamiliar terrain he may choose to pull the payload by engaging the Unit/s behind him.
  • the rescuer executes the steps (a), (b), (c) and (d) above with the exception that the Unit is turned up-side down such that the caster [22] is not in touch with the ground and the distal elements [2] of the said Arms [1] are in contact with the ground/floor/stairs. This is to preclude a tangle of the caster [22] with the perpendicular phase of the stairs.
  • the rescuer may choose to preferably pull the Unit with the payload up the flight of stairs either fastened to the Fastening-Apparatus [20] or by holding the proximal ends of the Unit and climbing up as shown in the drawing.
  • the rescuer executes the steps (a), (b), (c) and (d) above, and may choose to preferably pull the Unit with the payload down the stairs either fastened to the Fastening- Apparatus [20] as shown in the drawings, or by holding the proximal ends of the Unit and climbing down.
  • the rescuer may adjust the length of the Arms [1] by actuating the rotary means to make the desired angle of the Unit with the ground, such that the payload does not touch the terrain while being transported.
  • the rescuer joins/splices the proximal ends of both arms [1] of the Unit by engaging the pipe clip or spring clamp such that the payload is secured and encapsulated by the netting [14] that enshrouds and cocoons it snugly and also by the said arms [1] that are joined together that provide rigidity and support to the capsule to keep the payload from buckling/deforming.
  • This obviates the need to additionally secure the payload with straps or other such securing gear, since the said netting [14] snugly grips the payload and the said Arms [1] act as the mainstay to lend support and preserve the posture/shape of the payload.
  • the rescuer then fastens the airlifting gear [24] such as a rope to the spliced Anchoring means [8] that form a hook-like structure [11] by making an acute angle with the arms [1], by means of a slipknot or other such knot.
  • the payload along with the unit is now suspended vertically and can be drawn up/down from the aircraft [13].
  • a simple method to unload a given payload would include without limitation, while the unit is not vertical in position, moving the proximal end of one of the said arms [1] of the said rigid component away from the other along the vertical axis/plane, such that the payload gently rolls over, out of the said unit.
  • This is made possible by either a double hinge joint/pivot joint (one perpendicular to the other) or a ball and socket joint or any combination thereof.
  • the said unit In case of an injured (e.g., human [23]/animal) payload, the said unit is placed on the surface on to which it is to be transferred, and then the netting [14] is gently pulled from underneath the payload along with the said rigid arms [1] along the direction of the longitudinal strands of the netting [14] toward the distal end, while gently lifting the corresponding sections of the payload.
  • an injured e.g., human [23]/animal
  • This invention anticipates further adaptations of the said system and apparatus to suit specific and varied needs of the soldier/rescuer such as but not limited to be used (a) as climbing/scaling/rappelling gear, (b) as towing gear, (c) for mounting and positing surveillance devices such as cameras/scanners or other communication systems etc.,
  • This embodiment is a stripped/bare cost-effective version similar to
  • Anchoring means [8] does not contain any automatic mechanism for stretching out or collapsing the said elements [2].
  • Embodiment-I This embodiment is similar to Embodiment-I hereabove, except the following distinguishing aspects wherein, the said relatively flexile component referred to in 1(b) of Embodiment I is further provided with;
  • the said substructure comprises a plurality of members [25] which are collapsibly fastned one to another such that the maximum swing/pivotal/rotation about a given joint is (about) 180 degrees and suspended from the said arms [1] either by means of the transverse strands of the said netting or by means of rods (of hard plastic, metal or PVC or other suitable material known in the art) or by a combination of the two, whereby, when stretched out under the weight of the payload [23, 35], the said members [25] of the substructure [26, 27] form a plain supporting surface; and wherein the said flexile component [14] is attached/secured to the said members [25] such that they do not hinder, hamper or tangle when the said elements [2] rotate, collapse or stretch out, but stretch out and collapses in conjunction with the said elements [2];
  • the said members are 'Slats' [25] or such other flat and preferably rectangular structures made of light weight material such as (but not limited to) Plastic, PVC, Aluminium or other metals or alloys or such combination of materials known in the art such as but not limited to leather Slats provided with metallic hinges, which provide the necessary rigidity and strength to bear a given class/weight/size of payload.
  • light weight material such as (but not limited to) Plastic, PVC, Aluminium or other metals or alloys or such combination of materials known in the art such as but not limited to leather Slats provided with metallic hinges, which provide the necessary rigidity and strength to bear a given class/weight/size of payload.
  • Each slat [25] has a rather flat rectangular surface wherein, one (anterior) side of which (called the Male-end) is provided with a hinge-knuckle, bearing Pins [28] on either side of the said knuckle, and the other (posterior) side of which (called the Female-end) is provided with knuckles bearing holes [29] to accommodate the said pins of the Male-end of another slat.
  • the thichness/hight of the slat [25] which equals the diameter of the said knuckles is (without limitation) about 2.5 - 5 mm.
  • Each slat [25] is further provided with an 'Abutment cum Stop structure' [32] which restricts the rotational/pivoting/swing angle of one slat with respect to the other, to a maximum of 180 degrees such that when the said slats [25] of the substructure [27] are hinged together and stretched out, they form a flat surface which does not buckle under the weight of the payload, wherein the said Abutment cum Stop structure [32] is an extension of the dorsal surface of the slat [25], in the form a strong plate or strip which extends (without limitation to) about 5mm - 15mm, beyond the said Knuckles [29] at its Female-end, so as to restrict and arrest the swing/rotation/pivotal of the Male-end of another slat which is hinged to it, to a maximum of 180 degrees.
  • Each slat is fastned/hinged to another, such that the Male-end of one slat [25] is fastened/hinged to the Female-end of another [25] and further such that the dorsal side of one slat is in phase with the ventral side of the other slat to which it is fastned/hinged.
  • Each slat is further provided with fastening means [31] so as(a) to be fastened to the said relatively flexible component (or the said netting [14]) or (b) to be directly suspended from the said arms [1] by means of rigid rods extending from the Loops [7] or Rings [6] therein, wherein, the said fastening means is a system of rings [31] through which the preferably transverse strands of the said net [14] or the said rods pass such that when the said arms [1] of a unit (and consequently the said netting [14]) stretch out, the said slats [25] are also forced to stretch out to form a flat substrutre [27].
  • the said Rings [31] are attached to the slats [25] such that one slat bearing the said rings on its dorsal side is fastned/hinged to another slat which bears the said rings on its ventral side whereby all the said rings[31] in a given substructure are on its ventral side.
  • each slat [25] is preferably (but not limited to) about 5 - 8 inches in width and either square or rectangular.
  • Each slat is further linked to its adjescent slat by a suitably mild resilience or elastic means [33] which tend to corrugate and collapse the said slats especially when no payload is laid on the said substructure whereby, when the unladen unit collapses, the said members/slats [25] of the substructure [26] also collapse, wherein "the said resilience/elastic means [33] are (without limitation) elastic bands [33] or springs fastned preferably at one end to the anterio-lateral side of one slat [25] and at the other end to the posterior-lateral side of the other slat [25] to which it is fastned/hinged.
  • the said resilience/elastic means [33] are (without limitation) elastic bands [33] or springs fastned preferably at one end to the anterio-lateral side of one slat [25] and at the other end to the posterior-lateral side of the other slat [25] to which it is fastned/
  • the last slat at the distal end is 'L' shaped (not shown in the drawings) in order to prevent the payload [23, 35] from slipping/sliding downward especially when the payload is transported in a reclining / recumbent or vertical position.
  • the said substructure [26, 27] is further provided with Detachable
  • Unloading gear [34] wherein, at least one broad strap with tapering ends [34], made of light weight flexible and durable material such as but not limited to Nylon, Polyester, leather, PVC or such other suitable material or fabric known in the art to be suitable to bear the weight of a given class/mass/size of payload, is velcroed to a slat/s of the said substructure [26, 27], wherin the central broad part of the said strap is preferably but not limited to about 6 inches in width and about 20 - 25 inches in length and the narrow/tapering part is about 2 inches in width and about 15 inches long on either side, provided with suitable fasteners such as but not limited to buckles or tucktite fasteners (not shown in the drawings), which facilitate quick and efficient unloading or offloading the payload from the unit whereby, at the time of unloading the two narrow ends of the said unloading gear [34] are fastned/buckled together and lifted to remove the payload out of the unit.
  • pneumatic or other buoying means may be incorporated with or fastened to the arms and/or netting so as to keep the payload afloat while traversing or fording water
  • the rotary mechanism may be either a battery powered motor [15] or the manual draw-strings [19] wound around the spindle [17], embedded in the Flexible/resilient means [10] of the Anchoring means [8].
  • a rescuer may carry the payload [35] on the said unit either on his shoulder or head or back or in his arms (or such part of the body on which to balance the laden unit) as convenient and may carry more than one units at a time for transportation on foot.
  • the unit optionally fitted with the Buoying means can be made to float on the surface of the water whereby the rescuer can drag the said laden unit along, while swimming across the water.
  • Substructure [27] in a unit is optionally provided with 'Unloading gear' [34], being Broad Strap(s) with tapering ends [34], such that a small area of about 1 to 2 square inches of the ventral side of each said broad strap/s is velcroed to a said member/Slat;
  • each unloading gear [34] When the payload (especially injured human) contained in the said unit described in embodiment 3, is to be unloaded with minimal effort and stress to the rescuer and the rescued, the said tapering ends of each unloading gear [34] are fastened together, encircling the payload' s girth, by fastening means such as but not limited to buckles or tucktite fasteners (not shown in the drawings), and gently lifted out of the unit. Since the velcroed area is small (about 1 - 2 sq. Inches), the said unloading gear easily comes off the substructure [27]. In case of human payloads, without limitation, two to three numbers of the said unloading gear [34] may be provided per unit.
  • the lower end (the legs) of the payload is lifted slightly upward and moved out of the unit and finally the head along with shoulder/chest of the payload is transferred out.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Animal Behavior & Ethology (AREA)
  • General Health & Medical Sciences (AREA)
  • Public Health (AREA)
  • Veterinary Medicine (AREA)
  • Emergency Lowering Means (AREA)

Abstract

Appareil et système efficaces, économiques, portables et repliables pour le transport et le transfert mains libres d'une pluralité de charges utiles, y compris d'êtres humains, de construction légère et escamotables sur le corps d'un sauveteur, lesdits appareil et système faisant partie intégrante de l'équipement/de la tenue personnel(e) du sauveteur et un système constitué de plusieurs unités pouvant être utilisé de manière efficace par un seul sauveteur simultanément. L'invention concerne également le(s) procédé(s) d'utilisation desdits appareil et système, y compris leurs adaptations, notamment lors d'opérations de sauvetage exigeantes, en particulier mais non exclusivement en forêt, en terrains accidentés et lorsqu'il s'agit de traverser des étendues d'eau.
PCT/IN2013/000055 2012-02-06 2013-01-28 Appareil repliable portable destiné au transport mains libres d'une pluralité de charges utiles, y compris d'êtres humains, et escamotable sur le corps du sauveteur, système et procédés associés WO2013118145A2 (fr)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
IN423/CHE/2012 2012-02-06
IN423CH2012 2012-02-06
IN668/CHE/2012 2012-02-23
IN668CH2012 2012-02-23

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WO2013118145A2 true WO2013118145A2 (fr) 2013-08-15
WO2013118145A3 WO2013118145A3 (fr) 2013-11-07

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Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3550997A (en) * 1968-10-01 1970-12-29 Helen R Strand Backpack trundling assembly
WO1992000866A1 (fr) * 1990-07-07 1992-01-23 Robin Christopher Lockwood Dispositif de transport
US5806878A (en) * 1996-09-17 1998-09-15 Double D Development Co. L.L.C. Collapsible wheelbarrow/stretcher
US5903997A (en) * 1998-03-20 1999-05-18 Jacob; James L. Hunting decoy blind and cart
CN2346418Y (zh) * 1998-09-28 1999-11-03 上海市医药管理局技工学校 可折叠成背包状的医用急救担架
US20100237111A1 (en) * 2007-10-16 2010-09-23 Mroczka David E Backpack with collapsible stretcher and collapsible wheel assembly
US20100299837A1 (en) * 2009-05-27 2010-12-02 Conax Florida Corporation Vacuum packed inflatable stretcher with frangible overwrap and method of deploying same

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3550997A (en) * 1968-10-01 1970-12-29 Helen R Strand Backpack trundling assembly
WO1992000866A1 (fr) * 1990-07-07 1992-01-23 Robin Christopher Lockwood Dispositif de transport
US5806878A (en) * 1996-09-17 1998-09-15 Double D Development Co. L.L.C. Collapsible wheelbarrow/stretcher
US5903997A (en) * 1998-03-20 1999-05-18 Jacob; James L. Hunting decoy blind and cart
CN2346418Y (zh) * 1998-09-28 1999-11-03 上海市医药管理局技工学校 可折叠成背包状的医用急救担架
US20100237111A1 (en) * 2007-10-16 2010-09-23 Mroczka David E Backpack with collapsible stretcher and collapsible wheel assembly
US20100299837A1 (en) * 2009-05-27 2010-12-02 Conax Florida Corporation Vacuum packed inflatable stretcher with frangible overwrap and method of deploying same

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