This application claims priority to Australian Patent Application No. 2014902833 filed on Jul. 22, 2014 and Australian Patent Application No. 2014903335 filed on Aug. 25, 2014, each of which is incorporated by reference herein in their entirety.
The present invention generally relates to a military stretcher system, and in particular to an aero-medical military stretcher system.
The reference to any prior art in this specification is not, and should not be taken as an acknowledgement or any form of suggestion that the prior art forms part of the common general knowledge.
Medevac field stretchers commonly known as NATO type stretchers are designed in accordance with NATO and other military standards and are used in the evacuation of military or other casualties (e.g. during a natural disaster) to hospital in a helicopter or aeroplane. A NATO type military field stretcher includes a pair of rails terminating in handles, and a carrier sheet (normally canvass) extending between the rails to carry a patient. In practice, loaded NATO type stretchers are rested on fixed racking in aircraft during air transportation.
However, the applicant has perceived that NATO type stretchers are less than ideal. Whilst improved stretchers are available to improve the comfort and security of a transported patient, the use of standard aircraft restraints and racking systems to suit the NATO type stretcher has impeded the use of such improved stretchers in medevac operations. This issue is particularly significant when considering the widespread adoption of these restraints and racking systems throughout the full suite of military transportation assets, on land, at sea and in aviation.
The applicant also recognizes the deficiencies of the present NATO type stretchers in use, including but not limited to the following deficiencies. The NATO type stretcher exhibits:
Embodiments of the present invention provide for improved stretchers and associated devices in medevac operations.
According to a first aspect of the present invention, there is provided a military stretcher system including:
Advantageously, the adaptor may adapt the hand-carried stretcher to fasten to the holder conventionally used to hold a known NATO type stretcher. The holder may include aircraft racking.
Preferably, the stretcher includes carbon fibre material. The stretcher may include other material (such as Kevlar for example). The stretcher may be lightweight, not weighing more than 15 kg, and preferably less than 10 kg. The stretcher may include a carbon fibre composite chassis. The chassis may be molded. The stretcher may further include a backrest or headrest. The stretcher may further include a lifter for lifting the rest from the chassis to an inclined position. The lifter may include a sealed gas strut. The stretcher may also include a support mattress, for patient comfort during stretchering. The stretcher material may be fire or flame resistant.
The stretcher may include at least one pin for being received in a receptacle of the adaptor. The stretcher may include a locking actuator for locking the stretcher to the adaptor. The actuator may be a hydraulic actuator.
The adaptor may include a frame. The frame may include a pair of rails for extending between arms of the holder. The adaptor may include one or more docks for docking the stretcher. Each dock may include a tapered guide for guiding a sliding stretcher. Each dock may define at least one female receptacle for receiving a pin of the stretcher. The receptacle may be retractable. The adaptor may include a quartet of rests.
The system may include at least one male-female fastening arrangement for fastening the stretcher to the adaptor. The system may include a locking mechanism for locking the stretcher to the adaptor. The locking mechanism may include a retractable locking pin for being received by the adaptor.
The adaptor may include a ballistic shield for shielding ballistic material (e.g. bullets or shrapnel). The shield may be releasably fastened to an underside of the adaptor. The shield may clip to the adaptor. The shield may include a sheet. The sheet may receive replacable inserts of ballistic protection material. The ballistic protection material may include carbon fibre and/or Kevlar and/or ceramic material of suitable composite construction to protect the patient on the stretcher.
The system may further include a medical life support module for interconnecting between the adaptor and stretcher. The medical module may include a life support system. The medical module may include an oxygen tank and regulator, and/or suction systems. The medical module may also include a power inverter and supply outlets.
The system may further include another adaptor for adapting a non-military stretcher (e.g. conventional civilian stretcher) to fasten to the adaptor. The adaptors may form a locking arrangement for releasably locking together. The other adaptor may include a guide for guiding wheels of the non-military stretcher. The guide may include a pair of channel rails. The other adaptor may include a fastening mechanism for fastening the non-military stretcher. The fastening mechanism may include at least one catch. The catch may be retractable.
The system may further include a workbench for fastening to the adaptor. The workbench may include carbon fibre, Kevlar or metal alloys.
The system may further include the racking system. The racking may include a pair of arms for supporting the adaptor. Each arm may include one or more receptacles for receiving respective handles of the adaptor.
According to a second aspect of the present invention, there is provided a military adaptor for adapting a military hand-carried stretcher to fasten to a military transportation stretcher holder.
According to a third aspect of the present invention, there is provided an adaptor system including the military adaptor, and another adaptor for adapting a non-military stretcher (e.g. conventional civilian stretcher) to fasten to the adaptor.
According to a fourth aspect of the present invention, there is provided an adaptor configured to adapt a non-military stretcher (e.g. conventional civilian stretcher) to fasten to a military adaptor.
According to a fifth aspect of the present invention, there is provided a military hand-carried stretcher configured to be fastened to an adaptor, in turn, fastened to a military transportation stretcher holder.
According to a sixth aspect of the present invention, there is provided a military evacuation method involving:
According to a seventh aspect of the present invention, there is provided a military stretcher system including:
According to an eight aspect of the present invention, there is provided a medical stretcher including a carbon fibre composite frame and/or chassis.
Advantageously, carbon fibre composite stretchers are lightweight when compared with conventional steel, alloy or aluminum stretchers. Preferably, the stretcher is a hand-carried stretcher which is carried by hand when loaded.
The stretcher may include an impermeable patient support fastened to the frame which is more readily cleaned and more sanitary than fabric of NATO type-stretchers. The patient support may include carbon fibre composite material. The patient support may include cutouts though which seatbelts can advantageously pass to secure the patient. The frame may be at least partially exposed which advantageously allows ready visual inspection or damage. The stretcher may further includes a movable backrest or head rest for patient comfort. The stretcher may further include a lifter for lifting the backrest or headrest. The lifter may be hydraulic. The stretcher may include underside locking arrangements for locking the stretcher in place.
According to a ninth aspect of the present invention, there is provided a stretcher system including:
According to a tenth aspect of the present invention, there is provided a life support module including a coupler for coupling a medical stretcher. The coupler may include a docking arrangement. The coupler may include a lock.
Any of the features described herein can be combined in any combination with any one or more of the other features described herein within the scope of the invention.
Preferred features, embodiments and variations of the invention may be discerned from the following Detailed Description which provides sufficient information for those skilled in the art to perform the invention. The Detailed Description is not to be regarded as limiting the scope of the preceding Summary of the Invention in any way. The Detailed Description will make reference to a number of drawings as follows:
According to an embodiment of the present invention, there is provided an aero-medical military stretcher system 100 for front-line services as shown in
The stretcher 102 includes a molded carbon fibre composite chassis 108 including carbon fibre and Kevlar. The stretcher 102 is extremely lightweight, not weighing more than 15 kg, and preferably less than 10 kg. The stretcher 102 further includes a pivoting backrest (or head rest) 110 to enable the patient to sit up for optimum care. The stretcher 102 further includes a pneumatic, hydraulic or electric lifter 112 for lifting the rest 110 from the chassis 108 and to an inclined position. The lifter 112 includes a retractable sealed gas strut. The stretcher 102 also includes a support mattress (not shown), for patient comfort during stretchering. The stretcher materials can be fire or flame resistant.
Turning to
As can best be seen in
Each dock 204 includes a locking mechanism 212 for locking the stretcher 102 to the adaptor 104. The locking mechanism 212 includes the locking receptacle 802 for received the near stretcher pin 700. The locking receptacle 802 is spring biased to be retracted and unlocked to facilitate stretcher loading. Once the stretcher 102 is fully slid and loaded into the adaptor 104, a carer can manually push up the locking receptacle 802 so that the locking receptacle 802 protrudes from the adaptor 104.
As shown in
The stretcher locking arrangement 702 is hydraulically operated and the complementary adaptor locking mechanism 212 is manually operated independently, although these can alternatively be mechanically, pneumatically or electrically operable, or operated together with a single actuator. The adaptor 104 also includes a quartet of rests 214 extending beneath respective junctions of the rails 202 and docks 204.
Turning to
Turning to
Turning to
Returning to
The system 100 is used in aero-medical military evacuations including during natural disasters, but also during battle or war. In use, the adaptor 104 is fastened to aircraft racking. In turn, the medical stretcher 102 carrying the patient is slid into the docks 204 and locked, with locking mechanisms 212, to the adaptor 104 for transport.
As can best be seen in
As can best be seen in
Turning to
The top adaptor 1100 includes a linear guide for guiding wheels 1202, 1204 of the non-military stretcher 1200. The guide includes a pair of channel rails 1206 and may include releasable ramps extending from respective channels 1206.
The top adaptor 1100 also includes a fastening mechanism for fastening the non-military stretcher 1200. In particular, the fastening mechanism includes a pair of fixed rear fasteners 1102, a pair of intermediate retractable fasteners 1104 and a front retractable fastener 1106. Each fastener is a catch or hooked for catching on a bar of the non-military stretcher 1200. The top adaptor 1100 also includes a hydraulic pull actuator 108 for protracting the retractable fasteners 1104, 1106.
The fastening mechanism of the top adaptor 1100 of
A person skilled in the art will appreciate that many embodiments and variations can be made without departing from the ambit of the present invention.
In one embodiment, purpose built aircraft racking 106′ may include the adaptor docks 212′ as shown in
In compliance with the statute, the invention has been described in language more or less specific to structural or methodical features. It is to be understood that the invention is not limited to specific features shown or described since the means herein described comprises preferred forms of putting the invention into effect.
Reference throughout this specification to ‘one embodiment’ or ‘an embodiment’ means that a particular feature, structure, or characteristic described in connection with the embodiment is included in at least one embodiment of the present invention. Thus, the appearance of the phrases ‘in one embodiment’ or ‘in an embodiment’ in various places throughout this specification are not necessarily all referring to the same embodiment. Furthermore, the particular features, structures, or characteristics may be combined in any suitable manner in one or more combinations.
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2014902833 | Jul 2014 | AU | national |
2014903335 | Aug 2014 | AU | national |
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