US3487810A - Emergency signaling device - Google Patents
Emergency signaling device Download PDFInfo
- Publication number
- US3487810A US3487810A US599784A US3487810DA US3487810A US 3487810 A US3487810 A US 3487810A US 599784 A US599784 A US 599784A US 3487810D A US3487810D A US 3487810DA US 3487810 A US3487810 A US 3487810A
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- United States
- Prior art keywords
- balloon
- boss
- housing
- conduit
- bore
- 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
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- G—PHYSICS
- G08—SIGNALLING
- G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
- G08B5/00—Visible signalling systems, e.g. personal calling systems, remote indication of seats occupied
- G08B5/002—Distress signalling devices, e.g. rescue balloons
Definitions
- the invention relates to an emergency signaling device containing an uninflated balloon and a supply of lighter-than-air balloon inflatlng gas and adapted to conveniently and expediently inflate and expel the balloon.
- the invention concerns an emergency signaling device of the type above described in which the balloon remains aloft and is tethered to the site of the emergency to provide a continuous communication or signaling means.
- Emergency signaling is a frequently used mode of communication. Persons lost while hiking or hunting improvise and utilize a wide variety of signaling methods. Most commonly, a lost person will resort to shouting and waving his arms. Those lost in an area where a fuel supply, brush, dead branches, and other natural combustionable tinder is available, will resort to building a fire. Hunters have a universal signal comprising three rapidly fired gun shots. While these methods may be nearly adequate under certain circumstances, they leave much to be desired. For example, shouting and waving the arms is an energyconsuming task with limited range both as to sound and visibility. Building a fire requires that the environment supply the required combustionable materials. Signaling with a weapon is dependent upon the required firearm and ammunition supply. The above-noted signaling methods presuppose that the distressed person is not disabled and therefore capable of perpetuating the signaling .method. Further, the signaling must be accomplished at the precise time that a searcher or search party is within visual or sound range.
- Mechanized units are usually equipped with more sophisticated signaling devices. These include mainly flares and flare guns and electronic communication apparatus.
- flares as with the methods noted above, are dependent upon human capabilities to employ such at the proper time.
- Electronic signaling devices either manually operated or automatically engaged, have inherent basic limitations. If the device was not, in fact, destroyed during the crash of the vehicle, the shock and vibration may have been sufiicient to render the device useless. Even if the device is operative, it is still dependent upon a continuous electric power supply.
- a further object of the present invention is the provision of a signaling device which is self-contained and not dependent upon an external power supply source.
- Another object of the invention is the provision of a signaling device that is compact, lightweight, and simple to use, especially by persons afoot.
- Yet a further object of the invention is to provide a signaling device to be homologated into the structure of a vehicle as, for example, an aircraft, to be triggered either manually or by the impact to display a continuous signal to aid in the location of the imperiled vehicle.
- FIG. 1 is a perspective vieW of the device chosen for purposes of illustrating a presently preferred, manually operated embodiment of the invention as the device would appear when ready for use;
- FIG. 2 is a perspective view of a preferred embodiment of the present invention when used as a permanent signaling and spotting device in connection with a downed disabled aircraft;
- FIG. 3 is an elevational view in section taken along line 3-3 of FIGURE 1 and illustrating the operative relationship of the components of the invention
- FIG. 4 is an elevational view in section of the device of FIG. 1 and illustrating the terminal phase of the operation thereof;
- FIG, 5 is an elevational view in section of another preferred embodiment of the present invention and illustrating the components thereof as adapted to be operated electromechanically.
- I provide a tubular housing in which is encased a deflated balloon. Attached to the housing is a pressurized supply of lighter-than-air balloon inflating gas.
- a conduit is disposed coaxially within the housing and communicates between the pressurized gas supply and the balloon.
- a valve and a means for actuating the valve is located at the union of the conduit and the gas tank to control the flow of gas therebetween.
- a resilient boss having a longitudinal bore with a check valve located therein slidably and frictionally receives the upper end of the conduit. After the valve is opened, gas is transmitted through the conduit into the balloon where it is retained by the check valve.
- a spring means disengages the boss from the conduit, allowing the balloon to ascend.
- a line supplied from a spool which is coaxially mounted around the conduit within the housing.
- FIG. 1 illustrates a presently preferred embodiment of the manually operated device of the invention chosen for purposes of illustration and shows the generally tubular outer housing 10.
- a cylindrical adapter 11 coaxially rotatable with said housing 10 depends downwardly from the lower end thereof.
- An elongate cylindrical tank 12 is atfixed to and extends downwardly from the adapter 11.
- a disc-like cover member 13 frictionally engages the outer diametrical surface of the outer housing 10.
- FIG. 2 graphically depicts the signaling device of the present invention as it would appear in connection with a downed aircraft 14.
- the balloon 17 is tethered to the aircraft 14 by a line 18. It is evident from this illustration that the balloon 17 presents a permanent signaling and spotting device to aid searchers in the location of the distressed aircraft. It will be readily understood that the signaling balloon could be used not only by aircraft but by any other manner of vehicle or by a distressed human. Further noted is the permanence of the display, not requiring the attention of any person.
- FIG. 3 illustrates the internal operative components of the device of FIG. 1.
- the outer housing has an open upper end 19 and a substantially closed lower end 20.
- An annular bearing surface 21 depends downwardly from the lower end 20.
- the circular upper end 22 of the adapter is rotatably journaled about the annular bearing surface 21.
- a tab 23 having an aperture therein depends downwardly from the lower surface 20.
- An extension 24 which corresponds with the tab 23 and having an aperture therein depends laterally outward from the upper surface 22 of the adapter 11.
- a breakable seal comprising a thin, wire-like member 27 extending through the apertures in the tab 23 and the extension 24 is secured at its loose ends by a coined or minted union 28.
- An annular extension 29 having an external thread 30 and an internal thread 31 and a central bore 32 extends coaxially upward from the upper surface of the tank 12, The lower end of the adapter 11 threadedly engages the external thread 30 of the extension 29.
- a tubular valve body 33 frictionally engaging the interior diametric surface of the adapter 11 has a threaded lower portion which engages the thread 31 of the extension 29.
- a rod-like extension 34 terminates the nethermost end of the valve body 33 and is coaxially housed within the bore 32.
- An O-ring 37 is carried annularly by the extension 34 and frictionally engages the bore 32 to create an airtight seal therebetween.
- a multi-diameter annular bore 38 extends centrally through the valve housing 33.
- a female thread 39 and a shoulder 40 are determined by the multi-diameter bore 38 within the valve body 33.
- An elongated cylindrical spindle 41 having-a central longitudinal bore 42 is disposed coaxially within the lower end of the housing 10 and extends through the adapter 11 and terminates within the valve body 33.
- An enlarged annular surface 43 of the spindle 41 is rotatably journaled within the adapter 11.
- a spiral screwflight 44 carried by the spindle 41 immediately below the enlarged section 43 threadedly engages the female thread 31 of the valve body 33.
- An annular O-ring 47 carried by the spindle 41 frictionally engages the bore 38 of the valve body 33 to create a second airtight seal.
- a series of resilient inserts 48 are compressed be tween the lower end 49 of the spindle 41 and the shoulder 40 within the bore 38 to create a valve arrangement to control the flow of pressurized gas contained within the tank 12.
- a tubular flanged pilot 50 is secured to the lower end 20 of the outer housing 10.
- a pair of driving arms 51 and 51a having mutually parallel inner terminal ends extend diametrically inward from the pilot 50 and mate with corresponding fiat sides 52 and 52a provided along a portion of the spindle 41.
- the spindle 41 is thereby allowed a degree of lateral movement within the pilot 50 and yet is rotatably engaged to be driven by the arms 51 and 51a.
- a nut 53 having a circular outer surface is threadedly engaged near the upper end of the spindle 41.
- a needlelike projection 54 extends upwardly to terminate the upper end of the spindle 41.
- a guide 57 coaxially and slidably encompasses the spindle 41 and the nut 53.
- An annular flange 58 circumvents the guide 57 approximately midway of the longitudinal axis thereof.
- a compression spring 59 is disposed coaxially around the guide 57 and bears against the upper surface of the pilot 50 in the undersurface of the flange 58.
- a generally elongate tubular spool 60 carrying the pivoting line 18 on its outer indented surface is coaxially disposed within the outer housing 10.
- the spool 60 is locationally secured at its lower end by engagement with the pilot 50.
- the flange 58 of the guide 57 is locationally and slidably journaled within the inner diametrical surface of the spool 60.
- a shoulder 61 is provided near the upper end of the spool 60 to coaxially oppose a flange 62 provided near the upper end of the guide 57.
- a compression spring 63 disposed between the shoulder 61 and the flange 62 coacts to retain the spool 60 within the lower portion of the outer housing 10.
- a shoulder 64 integral with the internal surface of the guide 57 abuts the undersurface of the nut 53 to retain the guide 57 in its operative location with the spindle 41 against the action of the springs 59 and 63.
- An elongate tubular balloon container 64 attached at its lower end to the guide 57 extends upwardly therefrom coaxially within the housing 10.
- a cylindrical resilient boss 67 having a central longitudinal bore 68 which slidably frictionally receives the needle-like end projection 54 of the spindle 41 is frictionally engaged within the internal diameter of the guide 57 and rests upon the nut 53.
- the flexible membrane 69 having a series of spaced apertures 70 positioned near its outer diameter encompasses the upper surface of the boss 67.
- the balloon 17, having an opened lower end, encompasses the outer diametrical surface of the boss 67 concurrent with the membrane 69.
- An annular band 71 encompasses the boss 67 to secure the membrane 69 and the balloon 17 in an airtight arrangement.
- a flexible cap 13 having a downwardly extending circular lip portion 72 frictionally engages the outer diametrical surface of the upper end 19 of the outer housing 10.
- the upper central portion of the balloon 17 abuts the undersurface of the cap 13 and is secured thereto by a resilient washer 73 located internal of the balloon and a rivet 74 extending through the cap 13, the balloon 17 and the washer 73
- the operator grasps either the gas tank 12 or the adapter 11 in one hand and the outer housing 10 in the other.
- a counter-rotating force is now applied to the components as depicted by the arrows A and B of FIG. 1. This movement breaks the thin wire-like seal 27 and allows the internal components of the device to interact without further manual manipulation.
- FIG. 4 depicts the interaction of the mechanical components of the previously described manually operated preferred embodiment of the present invention during the initial opertaive stages.
- the arms 51 rotationally drive the spindle 41.
- the threaded portion 44 thereof being in operative engagement with the thread 39 provided within the valve body 33, is forced rotationally upward.
- the spindle 41 retracts upwardly, the distance between the end 49 thereof and the shoulder 40 is increased relieving the pressure upon the spherical seal 48 and creating a gas permeable chamber C.
- the lighter-than-air balloon inflating gas contained under pressure within the tank 12 now flows into the bore 38 of the valve body 33 through the chamber C and continues upwardly through the longitudinal bore 42 within the spindle 41.
- the pressurized gas continues upwardly, it is expelled from the bore 42 and enters the bore 68 provided within the boss 67.
- the pressure of the gas causes the flexible membrane 69 to recede upwardly away from the top of the boss 67, thereby allowing communication with the apertures 70 through which the gas passes to inflate the balloon 17.
- an equalized atmospheric pressure condition exists within the balloon 17, the tank 12 and the conduit passages therebetween.
- the resilient membrane 69 which acts as a one-way checkvalve, now relaxes and abuts the boss 67, disrupting gas communication between the bore 68 and the apertures 70, thereby retaining the gas within the balloon 17.
- the balloon is now fully inflated.
- the lower end thereof and the attached boss 67 are still frictionally engaged within the internal diameter of the guide 57 and the needle-like extension 54 of the spindle 41 is still frictionally engaged within the bore 68 of the boss 67.
- Slight manual pressure is now exerted downwardly upon the container 64 compressing the springs 63 and 59.
- the boss 67 is prohibited from downward movement by abutment against the upper surface of the nut 53. This movement forces the boss 67 to be expelled from the inside diameter of the guide 57. As the boss is so expelled, its resiliency causes it to return to its natural free-form which is diametrically larger than the internal diameter of the guide 57. After the housing 64 and the guide 57 have been retracted sufliciently, the boss 67 is completely expanded whereupon the undersurface thereof abuts the upper surface of the guide 57. The downward pressure exerted upon the container 64 is now released whereupon the compressed springs 59 and 63 urge the guide and the container upwardly.
- the distressed person may now anchor the signaling device to his person, a bush, vehicle, or any other convenient anchorage and have a permanently displayed sig naling or marking device to aid searchers in his rescue.
- FIG. 5 shows another preferred embodiment of the device of the present invention particularly adapted to be electromechanically operated.
- an elongate tubular outer housing comprising an upper section 81 and a lower section 82.
- a circular end panel 83 having a central longitudinal opening 84 is secured along the lower terminus of the outer housing 80.
- a cylindrical adapter is secured by its outer upper diametrical surface within the opening 84.
- the lower end of the adapter 87 is enjoined with a tank of pressurized lighter-than-air ballon inflating gas as previously illustrated in connection with the foregoing detailed description of the preferred manually operated embodiment of the present invention.
- a central bore 88 extending longitudinally through the adapter 87 communicates with the aforementioned pressurized gas tank.
- a valve body 89 is disposed coaxially within the lower portion of the lower section 82 of the outer housing 80 and threadedly engages the upper end of the adapter 87.
- An annular O-ring seal 90 is positioned between the union of the valve body 89 and the adapter 87 to insure an airtight seal therebetween.
- a central circular bore 91 extends the lower portion of the valve body 89.
- a cylindrical valve stem 92 is slidably located within the bore 91.
- the valve stem 92 has an enlarged conical head 93 which mates with an annular valve seat 94 carried by the valve body 89.
- a compression spring 97 encompassing the valve stem 92 acts to maintain continuous mating between the conical head 93 and the valve seat 94.
- a passage 98 extends coaxially a lateral portion of the valve stem 92, terminating below the conical head 93.
- a series of radial openings 99 communicate between the central passage and the external diametric surface of the valve stem 92.
- a carrier member 100 having an extended flange 101 is threadedly engaged at its lower end Within the upper end of the valve body 89.
- a plunger guide 102 having a threaded outer surface and a longitudinal extending bore is secured within the upper end of the carrier member 100.
- a series of electromagnets 103 are secured to and extend upwardly from the flange 101.
- a plunger 104 is slidably housed by the plunger guide 102.
- An annular flange 107 extends from the upper portion of the plunger 104.
- a series of magnet discs are carried by the flange 107 and are spaced so as to communicate with the electromagnets 103.
- a compression spring 109 encompasses the upper portion of the carrier member and bears against the flange 107 and the flange 101 to retain the electromagnet 103 and the magnet discs 108 in a spaced-apart relationship.
- a coaxial passage extends longitudinally through the plunger 104.
- An annular union 111 adjoins the upper section 81 and the lower section 82 to form the outer casing 80.
- a horizontal support member 112 is carried internally by the union 111.
- a gland 113 is carried by the support member 112 coaxially with the outer housing 80.
- a counterbore 114 slidably receives the upper end of the plunger 104.
- An annular O-ring 117 is carried by the upper end of the plunger 104 and frictionally engages the walls of the counterbore 114.
- a cylindrical upper guide 118 threadedly engages the upper end of the gland and extends upwardly therefrom.
- a tubular shuttle 119 is slidably housed within the lower diametrical bore of the upper guide.
- a cylindrical anvil 120 is slidably disposed within the shuttle 119.
- a central conduit 121 opening at the bottom of the anvil 120 terminates near the upper end thereof.
- a series of radial passages 122 communicate between the central conduit 121 and the chamber formed internal of the shuttle 119'.
- An annularly expanding spring 123 encompasses a recess provided in the outer surface of the anvil 120 within the shuttle 119.
- a compression spring 24 encompasses the lower extension of the anvil and bears against an intemal shoulder 127 within the gland 113 and a flange 128 integral with the anvil 120 to retain the upper surface of the anvil 120, the shuttle 119 and the annular expanding spring 123 within the upper guide 118.
- a series of passages 129 extend longitudinally through the upper surface of the shuttle 119.
- a bell housing 130 having a radial flange 131 extending from its lower end is threadedly engaged over the upper end of the upper guide 118.
- a needle-like conduit 132 is slidably journaled near its lower end within the upper guide 118 and near its upper end within the bell housing 130.
- a relatively thin flange 133 is carried by the lower end of the needle conduit 132 within the chamber D created by the hollow core of the lower end of the guide 118.
- a counterbore 134 extends coaxially downward from the upper end of the guide 118.
- An annular pilot 137 integral with the needle conduit 132 is slidably engaged within the counterbore 134.
- a compression spring 138 is disposed coaxially within the counterbore 134 and bears at its lower edge against the pilot 137.
- the upper end of the spring 138 bears against a washer 139 and an annular seal 140 which, in turn, abuts the internal flange 141 of the bell housing 130.
- the downward travel of the conduit 132 is delimited by the abutment of the pilot 137 against the seal 142.
- a spool 143 carrying line 144 is disposed coaxially about the upper guide 130 and the gland 113 Within the housing 80. The spool 143 is locationally retained by the support member 112 and the flange 131.
- a resilient boss 145 having a coaxial longitudinal bore 147 is frictionally engaged within the upper internal diametric surface of the bell housing 130.
- the bore 147 slidably and frictionally receives the upper end of the needle conduit 132.
- a flange 148 carried by the upper portion of the conduit 132 abuts the lower end of the resilient boss 145.
- a flexible membrane 149 having a series of spaced apertures 150 positioned near its outer perimeter encompasses the upper surface of the boss 145.
- a balloon 151 having an opened lower end encompasses the upper diametrical surface of the boss 145 concurrent with the membrane 149.
- An annular band 152 encompasses the boss 145 to secure the membrane 149 and the balloon 151 in an airtight arrangement.
- the loose end of the line 144 is also secured to the boss by the annular band 152.
- a flexible cap 153 having a downwardly extending circular lip portion 154 frictionally engages the inner diametrical surface of the upper end of the outer housing 80.
- the upper central portion of the balloon 151 abuts the undersurface of the cap 153 and is secured thereto by a resilient washer 157 which is retained by a fastener 158 extending through the cap 153 and into a rigid column 159 which rests on the upper surface of the boss 145.
- the electromagnets 103 are first given an electrical energizing pulse which attracts the magnet discs 108, pulling the plunger 104 downwardly.
- the plunger exerts downward pressure upon the valve stem 92, compressing the spring 97 and unseating the valve head 93 from the valve seat 94.
- the pressurized gas contained within the tank now flows through the bore 88 upwardly through the passage 98, out through the ports 99 and through the opened valves into the central passage 110 of the plunger 104.
- the pressurized gas exists the passage 110 into the counterbore 114 and continues upwardly through the conduit 121 in the anvil 120 and exits through the passages 122.
- the chamber D now becomes highly pressurized.
- the movable object of this pressure is the anvil 122.
- the anvil is pushed downwardly within the shuttle 119.
- the annular spring expands, abutting the undersurface of the shuttle and thereby retaining the anvil.
- the lower end of the anvil now abuts the upper end of the plunger 104 to retain the plunger in the position initially described in connection with the energization of the magnets 103.
- the electrical current supply to the electromagnets 103 may be discontinued. It will be readily understood by those skilled in the art that the above-described operative process is nearly instantaneous. Therefore, the electromagnets need only an initial energizing pulse.
- the pressurized gas within the system now has only a single avenue of escape.
- the gas therefore, travels upwardly through the needle conduit 132 and into the bore 147 of the boss 145.
- the pressurized gas now pushes the flexible membrane 149 away from the upper surface of the boss 145 and allows the gas to escape thorugh the apertures 150 into the balloon 151.
- pressure is directed to the underside of the column 159 causing the cover 153 to be urged upwardly and disengaging same from its frictional engagement with the outer housing 80.
- the boss 145 is still retained in its original position while the balloon 151 escapes through the open end of the outer housing 80 where inflation continues until the gas pressure in the balloon equalizes with the atmospheric pressure.
- the gas pressure within the system is equalized and the flexible membrane 149 resumes its original position against the upper surface of the boss 145 to act as a one-way check valve and disrupt the communication of gas between the bore 147 and the apertures 150.
- the diminished gas pressure can no longer overcome the force exerted by the compression springs'124, 109, and 97.
- the resultant force of the aforementioned springs drives the valve stem 92, the plunger 104, the anvil 120, and the shuttle 119 upwardly.
- the shuttle 119 abuts the flange 133, causing the needle conduit 132 to move upwardly, compressing the spring 138.
- the flange 148 being integral with the needle conduit 132 and disposed under the lower edge of the boss 145, urges the boss upwardly, disengaging it from its initial frictional location.
- the balloon is now free to ascend to a height limited by the line 144 supplied by the spool 143.
- a permanent signaling device is hereby displayed.
- the preferred electromechanical embodiment of the device of thepresent invention is highly adaptable to numerous situations. In its simplest form, it could merely be secured to a storage battery or other electrical impulse supply to provide a readily available stationary signaling device. In a more sophisticated adaptation, the device could be homologated into the external structure of an aircraft or other moving vehicle in connection with a sensory device designed to given an electrical impulse upon impact.
- Various other adaptations, modifications, and changes in the device herein chosen for purposes of illustration will readily occur to persons skilled in the art. Such modifications and variations while not explicitly denoted in the foregoing detailed specification do not deviate from the teachings of the present invention and are intended to be included in the spirit and scope thereof which is limited only by a fair interpretation of the following claims.
- An emergency signaling device comprising:
- valve means for controlling fluid communication between said tank and said first end of said conduit
- said balloon having an opening secured circumferentially around said boss
- (j) means responsive to the inflation of said balloon for expelling said balloon from said tubular housing.
- An emergency signaling device comprising:
- valve means within said adapter for controlling fluid communication between said tank and the longitudinal bore of said spindle;
- a spool of line disposed coaxially around said spindle within said housing, one end of said line being secured to said balloon;
- valve means means for opening said valve means such that fluid stored Within said tank flows through the longitudinal bore in said spindle, through the longitudinal bore in said boss, and through said check valve to inflate said balloon, and;
- (m) means responsive to the inflation of said balloon for expelling said balloon from said container and said housing.
- An emergency signaling device comprising:
- electromagnetically operated means for urging said plunger against and overcoming the force of said spring means such that said plunger is translated longitudinally into a second position, when said electromagnetic means is energized;
- valve means coupled to said plunger to open when said plunger is translated longitudinally to said second position in response to the energization of said electromagnetic means, said valve means connected to said tank to control the flow of fluid therefrom;
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Description
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US59978466A | 1966-12-07 | 1966-12-07 |
Publications (1)
Publication Number | Publication Date |
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US3487810A true US3487810A (en) | 1970-01-06 |
Family
ID=24401074
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US599784A Expired - Lifetime US3487810A (en) | 1966-12-07 | 1966-12-07 | Emergency signaling device |
Country Status (1)
Country | Link |
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US (1) | US3487810A (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3657752A (en) * | 1969-12-29 | 1972-04-25 | Proteus Inc | Locator devices |
US3929091A (en) * | 1973-04-10 | 1975-12-30 | Philippe Holder | Automatically inflating and liberating a balloon |
FR2473200A1 (en) * | 1980-01-02 | 1981-07-10 | Suas Claude | Distress signalling device using inflatable balloon - uses compressed gas to release balloon valve from inflation block and is packed to be worn on belt |
US4405099A (en) * | 1981-05-06 | 1983-09-20 | John Sawyer | Apparatus for activating system in response to impact |
US4482333A (en) * | 1982-04-30 | 1984-11-13 | Geri Engineering, Inc. | Automatic inflation system |
WO1987004133A1 (en) * | 1986-01-03 | 1987-07-16 | Cameron Robert W | Torpedo recovery device |
US4722498A (en) * | 1985-10-29 | 1988-02-02 | Cameron Robert W | Inflatable air foil |
US6477979B1 (en) * | 2001-03-30 | 2002-11-12 | Jonathan Sanchez | Emergency indicating and signaling device |
WO2004092774A2 (en) * | 2003-04-11 | 2004-10-28 | Ada Technologies, Inc. | Balloonsonde launcher |
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US2392199A (en) * | 1945-02-05 | 1946-01-01 | Maywood Chemical Works | Wire supporting device and gas generator for use therewith |
US2786599A (en) * | 1954-11-01 | 1957-03-26 | Herbert H Higbee | Automatic inflating device for life preservers |
US2862531A (en) * | 1956-09-10 | 1958-12-02 | Frank S Walker | Balloon distress signal |
US3002490A (en) * | 1958-09-23 | 1961-10-03 | Michael F Murray | Survival kit |
FR1344133A (en) * | 1963-01-21 | 1963-11-22 | Safety and signaling device for dives | |
US3142063A (en) * | 1961-03-28 | 1964-07-21 | Jr William M Goetzmann | Balloon mounted antenna with reeling and storage container |
US3171128A (en) * | 1962-11-08 | 1965-02-23 | Myron W Nixon | Emergency antenna having balloon means to erect antenna automatically in response to impact or immersion |
US3174455A (en) * | 1963-04-16 | 1965-03-23 | Gayle O Peterson | Inflatable signal balloon |
US3279419A (en) * | 1965-05-03 | 1966-10-18 | Michael A Demarco | Signal balloon device |
US3310024A (en) * | 1965-10-23 | 1967-03-21 | Robert C Mcconnell | Signal balloon |
US3381655A (en) * | 1966-07-07 | 1968-05-07 | Donald G. Rozzelle | Rescue balloon |
-
1966
- 1966-12-07 US US599784A patent/US3487810A/en not_active Expired - Lifetime
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US2392199A (en) * | 1945-02-05 | 1946-01-01 | Maywood Chemical Works | Wire supporting device and gas generator for use therewith |
US2786599A (en) * | 1954-11-01 | 1957-03-26 | Herbert H Higbee | Automatic inflating device for life preservers |
US2862531A (en) * | 1956-09-10 | 1958-12-02 | Frank S Walker | Balloon distress signal |
US3002490A (en) * | 1958-09-23 | 1961-10-03 | Michael F Murray | Survival kit |
US3142063A (en) * | 1961-03-28 | 1964-07-21 | Jr William M Goetzmann | Balloon mounted antenna with reeling and storage container |
US3171128A (en) * | 1962-11-08 | 1965-02-23 | Myron W Nixon | Emergency antenna having balloon means to erect antenna automatically in response to impact or immersion |
FR1344133A (en) * | 1963-01-21 | 1963-11-22 | Safety and signaling device for dives | |
US3174455A (en) * | 1963-04-16 | 1965-03-23 | Gayle O Peterson | Inflatable signal balloon |
US3279419A (en) * | 1965-05-03 | 1966-10-18 | Michael A Demarco | Signal balloon device |
US3310024A (en) * | 1965-10-23 | 1967-03-21 | Robert C Mcconnell | Signal balloon |
US3381655A (en) * | 1966-07-07 | 1968-05-07 | Donald G. Rozzelle | Rescue balloon |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3657752A (en) * | 1969-12-29 | 1972-04-25 | Proteus Inc | Locator devices |
US3929091A (en) * | 1973-04-10 | 1975-12-30 | Philippe Holder | Automatically inflating and liberating a balloon |
FR2473200A1 (en) * | 1980-01-02 | 1981-07-10 | Suas Claude | Distress signalling device using inflatable balloon - uses compressed gas to release balloon valve from inflation block and is packed to be worn on belt |
US4405099A (en) * | 1981-05-06 | 1983-09-20 | John Sawyer | Apparatus for activating system in response to impact |
US4482333A (en) * | 1982-04-30 | 1984-11-13 | Geri Engineering, Inc. | Automatic inflation system |
US4717092A (en) * | 1985-10-29 | 1988-01-05 | Cameron Robert W | Torpedo recovery device |
US4722498A (en) * | 1985-10-29 | 1988-02-02 | Cameron Robert W | Inflatable air foil |
WO1987004133A1 (en) * | 1986-01-03 | 1987-07-16 | Cameron Robert W | Torpedo recovery device |
US6477979B1 (en) * | 2001-03-30 | 2002-11-12 | Jonathan Sanchez | Emergency indicating and signaling device |
WO2004092774A2 (en) * | 2003-04-11 | 2004-10-28 | Ada Technologies, Inc. | Balloonsonde launcher |
US20050006523A1 (en) * | 2003-04-11 | 2005-01-13 | Patrick French | Balloonsonde launcher |
WO2004092774A3 (en) * | 2003-04-11 | 2006-07-13 | Ada Technologies Inc | Balloonsonde launcher |
US20070199503A1 (en) * | 2003-04-11 | 2007-08-30 | Ada Technologies, Inc. | Balloonsonde launcher |
US7275496B2 (en) * | 2003-04-11 | 2007-10-02 | Ada Technology, Inc. | Balloonsonde launcher |
US7648102B2 (en) | 2003-04-11 | 2010-01-19 | Ada Technologies, Inc. | Balloonsonde launcher |
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