as required , detailed embodiments of the present invention are disclosed herein ; however , it is to be understood that the disclosed embodiments are merely exemplary of the invention , which may be embodied in various forms . therefore , specific structural and functional details disclosed herein are not to be interpreted as limiting , but merely as a basis for the claims and as a representative basis for teaching one skilled in the art to variously employ the present invention in virtually any appropriately detailed structure . in fig1 , the fluid removal apparatus is generally shown at 10 . the venturi tube 11 may be of any length ( hereinafter tube ). tube 11 may be constructed of any suitable material known in the art capable of handling gases , liquids , or small particles . in the present embodiment the tube 11 was constructed of a clear flexible plastic . tube 11 may be attached to body 12 by any suitable known attachment method in the art , but not limited to velcro , adhesive , or adhesive tapes . tube 11 has a forward end 13 and a rear end 14 . in one embodiment tube 11 may have a valve 200 located on the outside rear - end portion 201 of hose 11 . valve 200 may act as a connection device for additional equipment , such as an external compressed gas container . tube 11 may have an attachment coupling 15 located on forward end 13 . any type of suitable attachment coupling may be used , but not limited to a ring or sleeve that creates a frictional fit between the inner surface of the sleeve or ring and the outer surface of the tube . conversely one may use an adhesive to attach coupling 15 to tube 11 . coupling 15 may be constructed of any suitable known material in the art but not limited to rubber , glass , metal , metal alloy , or plastic . in the present embodiment coupling 15 was constructed of plastic . there are a variety of different attachments that may be coupled to hose 11 . in the present embodiment an elongated hose with a means for removing debris was implemented . coupling 15 may provide a vacuum seal between hose 11 and attachment device . in one embodiment , as seen in fig1 , tube 11 may be permanently attached to body 12 , either on top surface 17 and / or side surface 18 . in another embodiment , tube 11 may be only attached to body 12 when vacuum device is being used . this may allow for cleaning and replacement of tube 11 . body 12 , as seen in fig1 , is of generally cylindrical shape , however any suitable known shape in the art may be implemented . body 12 has inside and outside surfaces , 201 and 202 respectively , which form cavity 203 . cavity 203 may be of such dimensions so as to be able to house one or multiple cans of propellant . in the present embodiment cavity 203 was constructed to house two cans of propellant 19 . in addition to housing propellant , body 12 may be adapted to receive a variety of different types of propellant , such as compressed gas or aerosol . furthermore , body 12 may be designed to harness propellant 19 in a multitude of methods , i . e . friction fit , threaded fit , or any other type of fastening means that are associated with aerosol or compressed gas cans . in the present embodiment body 12 was adapted to receive propellant via a frictional fit . depending on the nature of the intended use , the suction apparatus may be designed as a one shot disposable device or a rechargeable multi use device . in the present embodiment propellant 19 was readably replaceable when fully discharged . in addition , one may attach an outside source of compressed gas to valve 200 in situations where it is not practical to continuously replace individual cans of propellant ; e . g . in mass casualty situations , where constant changing of cans of propellant would waste valuable time , one could hook up a large tank of compressed gas such as oxygen to the portable fluid removal apparatus . each can of propellant 19 have a release valve 20 , which is connected to tube 11 by an export duct 21 . when activated , the release valves feed compressed gas into export duct 21 , which passes into tube 11 at inlet or port 22 . the export duct may be made of any suitable tubing material for handling a gaseous material . in addition export duct 21 extends longitudinally toward rear end of suction device 10 . as mentioned above , one of the disadvantages of the prior art is that the venturi effect is diminished during discharge do to heat loss . based on fundamental thermodynamic principles , the amount of heat added to effect the various phase changes is equal to the change in enthalpy ; the change of enthalpy between a liquid and a vapor phase is the latent heat of vaporization . as the propellant in the canister changes from a liquid to a gas , it requires and absorbs heat from the remaining liquid and the immediate area . when the propellant is released canister 22 cools , thus decreasing the internal pressure of the canister . the end result is excess propellant remaining in the canister . in order to compensate for this heat loss , one may implement an additional outside heat source , as seen in fig1 . between the cans of propellant 10 can be a battery 23 . the battery 23 may be connected to resistor wire 24 which is wrapped around each can . when activated , the current in the resistor wire heats the cans to increase the pressure of the gas inside the cans and thus increase the suction created . heat sensitive fuse blocks ( not shown ) may be employed to prevent overheating . in another embodiment one may implement a heat sink to heat the canister of propellant . generally , a heat sink is an environment or object capable of absorbing heat from another object with which it is in thermal contact ( either direct contact or radiational contact ). in common use , it is a device made of metal brought into contact with the hot surface of an object . in this type of embodiment one could wrap aluminum or copper , or any other good thermal conductor , around the outside surface of the canister and create a reverse heat sink , i . e . one could use the ambient temperature to heat the canister . in yet another embodiment one may implement a pcm in the can of compressed gas . the pcm should be a material that is capable of latent heat storage . a pcm is a material that will stay relatively the same temperature during phase change . for example , pcm &# 39 ; s absorb and retain heat when changing from solid to liquid , but release heat when changing from a liquid to solid . some pcm &# 39 ; s that can be implemented with the can of compressed gas are paraffin waxes , normal paraffin , and fischer - tropsch hard waxes . preferably , the pcms have a melting point between about − 3 ° celsius and 100 ° celsius . when compressed gas is expelled from the can and the temperature decreases , the pcm will release heat , which may keep the suction effect constant . in still another embodiment , in order to maintain an enough heat to produce total vaporization of the propellant , one may mix the desired propellant with an additive . for example , in one embodiment , one may use a propellant such as tetrafluoroethane , r134a . however , any suitable known propellant in the art including but not limited to co 2 , as in the preferred embodiment , argon and the like may be implemented . co 2 was the preferred propellant , because of it &# 39 ; s non - flammability , and higher pressure , which can increase suction . during discharge , as the r134a in the canister changes from a liquid to a gas , it requires and absorbs heat from the remaining liquid and the immediate area , the latent heat of vaporization for r134a is 216 . 8 kj / kg . as the canister cools , the vapor pressure of the propellant greatly decreases which reduces the outward flow and diminishes the venturi effect to zero in about 15 seconds ( assuming 3 . 5 ounces of r134a in canister ). this results in ˜ 100 ml of water suctioned up into a collection bag , and about 1 ounce of r134a left in the container . as mentioned previously , one may implement any of the above methods for increasing heat to increase internal pressure . however , one may also use an additive to increase the latent heat of vaporization . in the present embodiment equal parts of pure water and r134a were mixed , which resulted in ˜ 200 ml of water being suctioned up into the collection bag and an additional ˜ 1 . 8 ounces of r134a being vaporized . there are a multitude of propellants and additives that may be implemented to achieve similar results , and as such this embodiment is for illustrative purpose and is should not be limited to the above suggestions . in one embodiment activation means 26 runs along side surface 18 of body 12 . at one end 25 , the activation means 26 may be in the vicinity of or attached to export duct 21 . at a second end 27 , the activation means 26 may be attached to a first end 29 of a trigger 28 . at a second end 30 of trigger 28 is a depression means 31 . depression means 31 may be molded as a hand grip , with a finger indentation to allow the user to grip and squeeze easily . the trigger 28 is operated as a lever with a fulcrum 32 resting , or hingedly attached , to the bottom surface 33 of body 12 . fig2 depicts another embodiment of the present invention at 101 . in this embodiment , only a single can of compressed gas 102 is preferably utilized . while the tube 103 placement is similar to the previous embodiment , the release of compressed gas differs . device 101 may attach to a can of compressed propellant 102 by an airtight cap 104 . cap 104 encapsulates the release valve 105 on the top of can of compressed propellant 102 . a trigger mechanism 106 similar , to the trigger mechanism in our previous embodiment , may be implemented . trigger 106 may attach to release valve 105 , as seen in fig2 - 5 , or trigger 106 may rest on release valve 105 as seen in fig6 - 10 . in either embodiment trigger 106 is depressed via the user &# 39 ; s digit , thus releasing the propellant out of the canister and into airtight pocket 107 . pocket 107 maintains airtight integrity , which forces the propellant out through export duct 108 into venturi tube 103 . export duct 108 is adjacent to pocket 107 and longitudinally extends toward the rear end of suction device 101 , as in previous embodiments . venturi tube 103 is of basic design ; a tube comprising of a conduit and an inlet . in simplest form when a fluid moves through an inlet , a low pressure develops at the inlet , if the pressure is sufficiently low relative to the external pressure ; a partial vacuum is created , as mentioned previously . in the prior art the venturi device is located on the top forward end of the suction device . in the present invention , the inlet of the venturi tube is located toward the distal end of cap 104 , near the rear end of suction device 101 . it is understood that the body , tube , and can of propellant or compressed gas may be of any size , shape , or material . preferably , the tube will be soft plastic and the body will be hard plastic for easy maintenance and cleaning . additionally , the body may have a clip for attachment top a belt or strap of a bag . also , in the present invention the cans of propellant or compressed gas are easily replaceable , by either removing them from the body , or removing the clip . in any embodiment , a container ( not shown ) may be attached to rear end 14 of tube 11 . preferably , the container is a bag or pouch that will enable the user to collect any fluid or debris that is suctioned through tube 11 . the container may have an open end , which will preferably create an airtight seal around rear end 14 of tube 11 . in some manner , the bag may allow gas to escape , while suctioning liquid , debris or polluted air . in one embodiment the container will be equipped with an attachment port , which can mate with a filter . the filter may allow gas to escape , while retaining liquid , debris , or polluted air . in a second embodiment , the container itself may be manufactured from a gas - permeable , liquid retaining compound . in a further embodiment , the container may be equipped with vents that will allow gas to escape . in each embodiment , the container may be equipped with a sealing means , which will allow the user to remove and seal the container . a sealing means , which may be an adhesive strip or cap , can be used if the container houses hazardous material , or a liquid that can be reused after being filtered . as mentioned previously the present invention may include a variety of different attachments , such as a collection , isolation and test attachment 300 . attachment 300 may further include flexible hose 310 , immunoassay test strip 320 , filter portion 330 and test tube buffer 340 , as seen in fig1 . drawing one &# 39 ; s attention again to fig . 12 is hose 310 . hose 310 may have a front end 311 b and a rear end 311 a . rear end 311 a may be any suitable shape known in the art . for example rear end 311 a can be circular , square or rectangular in shape . the shape of rear end 311 a will depend on the shape of the couple used to attach collection device 300 to one of the aforementioned suction devices . in a preferred embodiment one used a generally rounded shape for rear end 311 a . rear end 311 a may be connected to any of the aforementioned suction devices via any suitable connection methods known in the art including but not limited to press fitting , screwing and the like . with any connection methods used rear end 311 a may be either the male or female end . in a preferred embodiment rear end 311 a was press fitted into the suction device , i . e . rear end 311 a was the male end , this ensures that no collected matter can escape between the outside coupling surface and the inside surface of rear end 311 a . front end 311 b may be generally circular in shape , however any suitable shape known in the art may be used . in the preferred embodiment front end 311 b has aperture 313 . aperture 313 may be any suitable shape known in the art , including but not limited to a square , rectangle and the like . aperture 313 may taper off in a direction toward filter portion 330 , also seen in fig1 , this ensures that the gathered matter is confined to filter portion 330 . also aperture 313 may have a diameter equal to or less then front end 331 of filter 330 . filter 330 may be any suitable type of filter known in the industry . in the preferred embodiment a highly dense non - reactive material was used . the length and amount of filter 330 will depend on the desired use , i . e . the type of matter being collected , contained and tested . filter 330 may have a front end 331 and a rear end 332 . front end 331 of filter 330 , as mentioned above is adjacent to front end 331 a of hose 310 , this ensures that the matter being collected and contained does not get exhausted out the rear . inside of hose 310 may be immunoassay test strip 320 . in one embodiment test strip 320 may be attached to rear end 332 of filter 330 and extend the entire length of hose 310 , or only partially therefrom . in the preferred embodiment test strip 320 was adjacent to rear 332 , but not attached and it extended the entire length of flexible hose 310 . test strip 320 may have one color indicator , or many color indicators , this will also depend on the matter to be collected . in the preferred embodiment one used a test strip with 3 color bands 321 , as may be seen in fig1 . test strip 320 can be designed to detect a multitude of different toxins and / or pathogens , in the preferred embodiment it was desirous to detect the presence of anthrax and ricin . as mentioned previously attachment 300 may include a test tube 340 . test tube 340 may be seen in more detail in fig1 . test tube 340 may any suitable test tube shape known in the art . it shall be pointed out now that in the preferred embodiment test tube 340 will fit snuggly around hose 310 . to ensure this snug fit one used a test tube with a tapered inside surface . test tube 340 may also contain a buffer solution , the type of solution used will depend on the type of chemical reaction desired . for example , there can be one type of buffer solution for detecting anthrax and a different type of buffer solution to detect ricin . in normal operation , when the user desires to collect , isolate and test suspicious foreign matter , the user will connect attachment 300 to one of the aforementioned suction devices . the user will then place the suction device in the vicinity of the suspicious foreign matter . the user will then activate the suction device in a manner described previously . the vacuum created by the suction device will then pull the suspicious foreign matter up through aperture 313 of tube 310 . as the foreign matter is being sucked up it will become trapped into anterior filter 330 . the user will then remove the buffer test tube cap and place it over tube 310 . the buffer solution will then be contact anterior filter 330 where it will dissolve and stabilize the trapped foreign matter . the reactive solution will then be absorbed up through test strip 320 . if a toxin and / or pathogen are present it will cause one of the color indicators to develop . if a toxin and / or pathogen are not present then the color indicators will not develop . as various changes could be made in the above constructions without departing from the scope of the invention , it is intended that all matter contained in the above description shall be interpreted as illustrative and not in a limiting sense . in the view above it will be seen that several objects of the invention are achieved and other advantageous results attained .
an improved suction apparatus , which may be used by health care providers , emergency medical teams , or a corpsmen , to remove debris , fluid and other foreign matter from the airways and / or wounds of injured persons . the suction apparatus which includes : a venturi tube having a forward end , a rear end and an inlet , a valve located on the top rear end portion of the venturi tube , a body for housing at least one can of propellant or compressed gas , an airtight cap , and a trigger mechanism . the improved suction apparatus that forces the propellant passed the inlet of the venturi tube , wherein the inlet is located toward the distal end of the cap .