US3910457A - Electronic water-activated parachute release and life vest inflator - Google Patents

Electronic water-activated parachute release and life vest inflator Download PDF

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US3910457A
US3910457A US467298A US46729874A US3910457A US 3910457 A US3910457 A US 3910457A US 467298 A US467298 A US 467298A US 46729874 A US46729874 A US 46729874A US 3910457 A US3910457 A US 3910457A
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battery
water
electrical
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sensing
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Roderick W Sutliff
David W Edwards
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H Koch and Sons Co
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H Koch and Sons Co
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D17/00Parachutes
    • B64D17/22Load suspension
    • B64D17/38Releasable fastening devices between parachute and load or pack

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  • ABSTRACT [22] Filed: May 6, 1974 p 7 An electronic water-activated package is described for automatically releasing a parachute canopy and inflating a life vest upon immersion in watenSeparate electronic water-activated packages are incorporated into 211 Appl. No.: 467,298
  • the electronic water-activated 9/319, 316, 320, 321, 323, 324, 325, 313, package includes an explosive squib and water sensing 336, 337, 338, 339; 244/149, 152; 307/246 circuitry which both detonates the explosive squib and minimizes current leakage from a power supply also [56] References Cited contained in the electronics package.
  • the invention relates to an electronic wateractivated package for energizing a parachute canopy release mechanism and an inflating assembly in a life vest upon immersion in water. More particularly, the invention relates to an electronics package with a selfcontained power source adapted to be integrally incor-,
  • Such life vests typically include a cannister of compressed gas with a mechanism for piercing the cannister to release the gas into the inflatable portion of the life vest.
  • piercing mechanisms require manual manipulation by the pilot.
  • a water-sensitive energizing apparatus wherein a silicon-controlled rectifier used as a thyristor switch interrupts a circuit loop having a battery and an explosive squib.
  • the McMain apparatus further includes two substantially parallel conductor plates of dissimilar metals to provide a galvanic element. The conductor plates are connected to the battery such that the electrical potential of the galvanic unit opposes that of the battery. Immersion of the plates in water completes the galvanic cell allowing current conduction which switches the thyristor to close the circuit loop between the battery and the explosive squib for detonating the squib.
  • the battery in the McMain circuit, the battery must have a sufficient current capacity to cause the squib to detonate.
  • the galvanic unit saps that current source.
  • the current conduction characteristics of the galvanic unit are temperature-dependent, thus making the entire circuit temperature-dependent.
  • Another defeet of the McMain circuit is that droplets of water. due to condensation and other debris. can accumulate between the conductor plates to cause a slow current leak which again saps the current capacity of the battery.
  • the primary disadvantage of the McMain circuit is that the power source has a relatively short shelf life because of current leakage and, for that reason, must be frequently checked. Such checks are easily forgotten or omitted by human personnel.
  • An electronic water-activated package which automatically energizes a webbing strap release mechanism and a cannister piercing mechanism upon immersion in water.
  • separate watersensitive electronic packages are integrally incorporated into break away webbing frames securing a parachute canopy to a parachute harness and into an inflation assembly at the bottom of each lapel of a life vest.
  • the water-activated electronics package includes a self-contained power source, an electrical explosive device, a capacitor discharge circuit for detonating the electrical explosive device, and a water-sensing circuit which, in addition to triggering the capacitor discharge circuit, also minimizes current leakage from the power source.
  • the invented electronic water-activated package when incorporated into the break away webbing frame and into the inflation assembly, are completely self-contained and do not require external connections and/or circuitry.
  • the elements of the circuit which mini mize current leakage from the power source give the invented electronics package a shelf life on the order of five to ten years.
  • the power source need only charge the capacitor and is not required to have sufficient current capacity to detonate the explosive device.
  • the invented release includes electronic elements which render it relatively insensitive to environmental temperature changes.
  • FIG. 1 is a schematic of the electronics package which is integrally mounted within a break away webbing frame.
  • FIG. 2 is a top view of a break away webbing frame showing the electronics package mounted therein.
  • the webbing frame illustrated also includes male prongs for insertion into a conventional manual release mechanism, also shown.
  • FIG. 3 is a right-side profile of the break away frame and manual release shown in FIG. 1.
  • FIG. 4 is a left-side profile of the break away webbing frame shown in FIG. 1 with the cover shield partially cut, away.
  • FIG. 5 is a partial cutaway, top view, of the release in a locked position.
  • FIG. 6 is a partial sectional view taken along lines 66 of FIG. 5.
  • FIG. 7 is a partial cutaway, topview, of the release in its break away configuration.
  • FIG. 8 is a cutaway sectional view taken along lines 88 of FIG. 7.
  • FIG. 9 is afrontal view of the life preserver showing the location of the automatic inflating assemblies incorporated into each lower lapel of the preserver.
  • FIG. 10 is an enlarged cross sectional view of the automatic inflating assembly (detail A of FIG. 9).
  • FIG. 11 is a cutaway sectional view taken along lines A-A of FIG. 10.
  • the ball lock detent mechanism includes a hollow cylindrical protrusion 31 extending perpendicularly inward into the webbing frame, 11 from the side bar 16. Coaxially mounted within the protrusion 31 is a springJoaded cylindrical release plunger 32, having a large diameter section 33, conically tapering to a small diameter section 34. A plurality of steel balls are disposed in an equal number of holes through the sidewall of the cylindrical protrusion 31 near its end.
  • the balls rest against the larger diameter section 33 of the release plunger 32.
  • the diameter of the balls 35 are chosen such that they extend beyond the sidewall of this'cylindrical protrusion 31 when resting on the larger diame ter section 33' of the release plunger 32.
  • a spring 37 holds the release plunger 32 in a normally locked" position.
  • a cylindrical receptable 38 in the webbing frame 11 receives the locking protrusion 31 of the side bar 16.
  • the receptacle 38 includes an annular shoulder 39 at its entrant end of a slightly smaller diameter than the receptacle for engaging the steel balls 35 of the cylindrical protrusion 31 when the protrusion is in a locking posture. (Sec FIG. 6).
  • the release plunger 32 is depressed against the spring 37 allowing the balls 35 to drop down in their respective holes 36 against the smaller diameter section .34 of the release plunger 32 where they cannot engage the annular shoulder 39 of the receptacle 38.
  • the release plunger is depressed by a piston actuator 41 of an electrical explosive cartride unit 40.
  • the cartridge unit includes a cylindrical chamber 42 for receiving the piston actuator 41.
  • An explosive charge 43 is disposed behind the piston actuator 41 and the chamber 42.
  • the unit 40 is secured to a mounting plate 21 and fits within a rectangular reeep tacle 44 within the webbing frame 11. V
  • the explosive charge is detonated by an electrical current pulse whereupon hot combustion gases drive the piston actuator 41 outward in its cylindrical chamber 42.
  • the extending piston actuator 41 first depresses the release plunger 32 sufficiently to allow the balls 35 to drop down into their respective holes 36, releasing the lock.
  • the extending piston 41 then engages the end of the cylindrical protrusion 31 to drive the side bar 16 outward to thereby free the end of the webbing pin 14.
  • the tensile force extant on the webbing strap 17 causes the webbing pin 14 to pivot outward-whereupon the strap 17 pulls free as shown in FIG. 7.
  • the water-sensing circuitry includes 'a battery BT-l with a positive and negative terminal and an intermediate positive voltage tap.
  • a PNP transistor Q-l switches a silicon-controlled switch Q-2 responsive to current conduction between the two electrodes, 22a and 22b, of the water sensor A-l.
  • the electrodes 22a and 2212 are connected to the positive and negative terminals of the battery BT'1 respectively.
  • the switch Q-2 serially interrupts the current pulsegenerating circuit between the negativeterminal of the battery and a capacitor; C-4. When the siliconcontrolled switch Q-2 is switched to a conducting status, the capacitor C4 is allowed to charge,
  • the current pulse-generating loop includes a siliconcontrolled switch Q-4 connected in series between the capacitor C-4 and a bridgewire of an electrical explosive device designated as EED-l.
  • the switch Q-4 is switched to a conducting state by a PNP transistor Q-3 which becomesconducting between the emitter and collector responsive to the potential difference across the capacitor C-4.
  • the switch ()4 discharges the charge buildup. across the. capacitor through the bridgewire EED-l to detonate the electri- 7 BT-I and the base of the transistors 0-1 and 0-3 cal explosive device.
  • the emitters of the transistors Q-l and Q-3 are connected directly to the positive voltage tap of the battery BT-l.
  • a temperature-compensating diode CR-l isconnected between the positive terminal of the battery .through resistances -R3 and R-6 respectively.
  • ' diode CR-l is also connected serially between the electrode 22a and the positive terminal of the battery BT-1.
  • the diode .CR-l renders the described circuit rela-, tively insensitive to environmental temperature changes. Specifically, environmental changes affect the base. voltage potential at which the transistors 0-1 and 0-3 become conducting through their collectors and emitters respectively. In particular,
  • the transistors Q-l and Q-3 and the temperature compensating diode CR-l are chosensueh thatthe increased positive potential supplied by CR-l offsets the I decreased ?turn on potential between the bases and emitters of the transistors 0-1 and 0-3 as temperature increases.
  • the resistance R-11 between the silicon-controlled switch 0-2 and the capacitor C4 is optional. Specifically, it is designed to limit the amount of current flowing in the current loop defined by the battery and the electrical explosive device.
  • All of the circuitry elements are packaged in a unitized metal shield connectcd to the circuitry with a single high-point resistance R-IO to prevent electrostatic charge buildup in the capacitor C4 and to isolate the described circuit from strong electromagnetic fields.
  • the conductors to the electrodes 22a and 22b pass through the shield via ceramic low-pass filter feeds C-2.
  • a monolithic by-pass capacitor C-3 is connected directly to the base of the transistor Q-l and through resistances R-3 and R-6 to the base of the transistor Q-3.
  • the described circuit functions as follows: As the water-sensor A-l is immersed in water, the base of the transistor becomes negative due to conduction from the base of 0-1 through the resistance of R1, the water-sensor A-1 and the resistance R-2 to the negative terminal of the battery BT-l. When the potential difference between the base and emitter of Q-l reaches'its turn on threshold, a conduction path is provided through its emitter and collector from the positive voltage tap of the battery BT-l through the resistance R-2 to the negative terminal of the battery BT-l. The potential drop across the resistance R-S causes the gate of the silicon-controlled switch 0-2 to become positive through the resistance of R-4.
  • the gate of the switch Q-2 becomes positive, it switches to a conducting state allowing the capacitor C-4 to charge through the current-limiting resistance R-11.
  • the turn on potential difference be tween the base and emitter of the transistor Q-3 is reached, thereby allowing conduction through its emitter and collector from the positive voltage tap to the silicon-controlled switch Q-4.
  • the potential drop across R-8 causes the gate of the switch Q-4 to become positive, switching it to a conducting state.
  • the switch Q-4 Upon switching to a conducting state, the switch Q-4 allows the positive charge built up across the capacitor C-4 to discharge through the electrical explosive device EED-l to detonate the explosive charge.
  • the described water-sensing circuit not only switches the capacitor-discharge circuit to generate an electrical current pulse, but also minimizes current leakage from the battery BT-l. Specifically, absent a conduction path between the electrodes 22a and 22b of the watersensor A-l, current leakage from the battery BT-l occurs through three circuit elements: l The monolithic capacitor C3 connected between the positive voltage tap of the battery BT-l and the base of the transistor Q-l; (2) The transistor 0-1; and, (3) The siliconcontrolled switch Q-2.
  • the monolithic capacitor C-3 is chosen to have a minimum insulation resistance greater than 5,000 megohms, such that current leakage through it is reduced to an insignificant value. Evaluation of leakage currents through the transistor Q-I and the silicon-controlled switch Q-2 should be considered at the full-rated voltage of each device at 50. For example, ifQ-l is chosen to have a rated leakage of 35 nanoamps at 45 volts and the switch Q-2 rated to have a leakage of 90 nanoamps at volts, the total maximum leakage is'app'roximately 125 nanoamps at 50C. If the battery BT-] has an available life of 180 M.A.H., the nanoamp leakage represents only about 5.5 M.A.H. of the available battery life. This amount is approximately equal to 3% of the battery life lost in 5 years of storage.
  • the electrical circuitry components are mounted in a unitized metalcovered package and mounted within an L-shaped cavity 19 within the webbing frame 11.
  • the electrical components are sealed from the outside environment by a mounting plate 21 secured to the webbingframe 11.
  • Two water-sensing electrodes 22a and 22b are mounted on the exterior of the mounting plate 21 and are insulated therefrom by the low-pass ceramic feedthrough filters 23.
  • the perforated shield 24 covers the two electrodes 22a and 22b to prevent inadvertent shorting therebetween. The perforations in the shield 24 allow air bubbles to escape from the shiled when the release is immersed in water.
  • electrodes 22a and 22b extend perpendicularly through the mounting plate 21.
  • the post-like configuration of the electrodes 22a and 22b prevent and minimize inadvertent shorting and leakage therebetween due to water condensation or debris.
  • the electrodes are gold-plated to enhance their sensitivity to moisture and water vapor and to maximize their corrosion resistance.
  • the airman is provided with an inflatable life preserver 46 in which the automatic inflating assembly 47 is incorporated into the bottom section of each lapel of the preserver 46.
  • the automatic inflating assembly 47 includes a cannister 48 containing compressed gas at high pressure, a cannister piercing mechanism 49, and a water-sensing electronics actuator package 51.
  • the cannister piercing mechanism 49 comprises a cast structure 52 having a port 53 appropriately threaded for receiving the neck of a high pressure gas cannister 48.
  • a set screw 54 prevents the gas cannister 48 threaded into the port 53 from vibrating free.
  • a piercing pin 56 is located in a passageway 57 through the cast structure 52 in axial alignment with the gas cannister port 53.
  • the piercing pin 56 includes a piercing point 58, a shank 59, an annular shoulder 61, and a rounded head 62.
  • a bushing 63 disposed in the passageway 57, holds the piercing pin 56 in axial alignment with the cannister port 53.
  • a spring 64 is disposed between the bushing 63 and the annular shoulder 61 of the piercing pin 56.
  • An O-ring seal 66 is disposed around the piercing pin 56 between the annular shoulder 61 and the rounded head 62 of the pin.
  • the end of the passageway 57 proximate the gas cannister port 53 defines a gas plenum 67 having a vent 68 which ultimately communicates to the inflatable portion of the life preserver 46 (not shown).
  • the rounded head 62 of the piercing pin 56 extends out of the passageway 57 and engages a rotatable cam 69.
  • the cam 69 is adapted to rotate clockwise about a pivot pin 71, as indicated by the arrow 72.
  • a manual lever 73 also pivots on the pin 71 and is-adapted to rotate the cam 69 when pulled in the direction of the arrow 74.
  • the cam 69 is also adapted the piercing point 58 of the pin breaks the closure membrane 77 of the gascannister 48.
  • the cam 69 continues to rotate until the recessed section 75 is in alignment with the piercing pin 56, whereupon the combined effect of gas pressure in the cannister and the compressive force of the spring 64 force the pin back out, whereupon the rounded head 62 of the pin is received in the recessed section 75 of the cam 69.
  • the watersensing electronic actuator package 51 includes an enclosure 78 adapted to be mounted on the cannister piercing mechanism 49, above the manual actuator lever 73.
  • the package 51 includes a watertight container 79 for receiving batteries 81.
  • the water-sensing circuitry is mounted on a printed circuit board 82.
  • the enclosurc is then filled with a conventional potting compound 83, isolating the circuit from water and moisture.
  • the transfer plunger 76 of the actuator package 51 is disposed in a retainer sleeve 84.
  • An electrical in more detail, referring to FIG. 1 I, the water-sensing electrodes 22a and 22b, of the water-sensing circuit hereinbefore described each include a central conductive pin 87 extending through the enclosure wall 78 of the actuator package.
  • the extending pins. are surrounded by an insulative sleeve 88 having a relief 89 to expose a portion of the pin 87 to the environment.
  • the reliefs 89in the insulative sleeves face or open in opposite directions to preclude shorting of the electrodes by a small amount of water.
  • thc'entire automatic inflating assembly 47 is received in an enclosure integral with the life preserver 46.
  • the bottom of the enclosure containing the automatic inflating assembly is sealed from the environment by a stretched nylon, fabric 50. Accordingly, the sensing electrodes 22a and 22b of the water-sensing electronic acutatorpackage 51 are isolated from dust and dirt.
  • a water-sensitive energizing electrical circuit for detonating electrical explosive devices upon immersion in water comprising, in combination,
  • a switching means for minimizing current leakage from said current source prior to immersion of said circuit in water and for switching said first means to generate a current pulse responsive to immersion in water, said switching means being con-- nected between said current source and said first means,
  • said electrical current source comprises a battery having a positive terminal, a negative terminal and an intermediate positive voltage tap.
  • first means for generating an electrical current pulse comprises a capacitor connected between the positive and negative terminals of the battery in parallel with the electrical explosive device, sensing means for sensing electrical potential across said capacitor, said sensing means being connected to said temperature compensating means, a first controlled switching means having a conducting and a non-conducting state connected in series in a circuit loop defined by said capacitor and said and the sensing means and a second resistance connected serially between said gate connection and the negative terminal of the battery, said silicon-controlled switch having non-conducting state when a negative.
  • said sensing means comprises a PNPtransistor having an emitter connected to said intermediate positive voltage tap of the battery, a base connected between said capacitor and said negative terminal of said battery and a collector connected to said first resistance; said PNP transistor having a turn on potential differencebetween the base and emitter at which electrical conduction occurs through the emitter and collector; said temperature-compensating means being connected serially with a resistance between said base of said transistor and said positive terminal of said battery for compensating a decreasing turn on potential difference between said base and said emitter of said transistor as temperature increases, whereby, upon said capacitor becoming fully charged, the potential difference between the base and emitter of the transistor reaches the turn on potential difference and allows conduction of a positive potential from said positive voltage tap through the emitter and collector of the transistor to be impressed upon said gate of said silicon-controlled switch.
  • a second controlled switching means for allowing current flow to said first means, said second con trolled switching means being serially connected between the negative terminal of said battery and said first means and having a gate connection, said second controlled switching means having a nonconducting state when a negative potential is im pressed upon said gate connection and a conducting state when a positive potential is impressed upon said gate connection, said gate connection being connected to said means for sensing current conduction between said first and second electrodes, whereby said means for sensing conduction between said electrodes impresses a positive potential on said gate of said second controlled switch causing it to become conducting, allowing current flow into first means.
  • said second controlled switching means comprises a siliconcontrolled switch connected serially between said first means and said negative terminal of said battery having a gate connection; a fourth resistance connected serially between said gate connection and said means for sensing current flow between said electrodes and a fifth resistance connected serially between fourth resistance and said negative terminal of said battery.
  • said means for Sensing current conduction between said electrodes comprises, in combination, a second PNP transistor having a base connected between said first electrode and said positive terminal of said battery, an emitter connected to said positive voltage tap of said battery and a collector connected to said fourth resistance; said second transistor having a turn on potential difference between said base and emitter at which electrical current conduction occurs through said emitter and collector; said temperature-compensation means being connected serially between the base of said second transistor and the positive voltage terminal of said battery for compensating a decreasing turn on" potential difference between the base and emitter of said second transistor as temperature increases, whereby current conduction between said first and second electrodes causes a turn on potential difference between said base and emitter of said second transistor allowing a positive potential from said voltage tap to be impressed through the emitter and collector of said second transistor on said gate of said second siliconeontrolled switch to thereby allow current conduction to said first means.
  • thermoelectricpensating means comprises a silicon diode and in that said PNP transistor is a silicon PNP transistor.
  • an inflating assembly for an inflatable life vest including a can nister containing high pressure gas, having a piercable closure membrane disposed across a necked section of said cannister, and a structure adapted to hermetically receive said necked section of said cannister for conveying gas from said cannister to said inflatable life vest, the structure comprising a piercing mechanism incorporated into said struc ture adapted to pierce said closure membrane and actuator means for operating said piercing mechanism, responsive to an electrical current pulse from said first means; said first means. said switching means and said actuatormeans being encapsulated in a unitary package adapted to be mounted on said structure.
  • said piercing mechanism comprises a piercing pin disposed in a passageway defined through said structure, said passageway communicating with the necked section of said cannister received in said structure, said pin having a point proximate said closure membrane across said necked section of said cannister and having a rounded head extending out of said passageway,
  • a rotatable cam pivotably mounted in said structure, adapted to drive the rounded head of said pin into said passageway upon rotation, to thereby pierce said closure membrane, said rotatable cam being adapted for rotation responsive to said actuator means.
  • a retainer sleeve having an open end and a closed end
  • a plunger disposed in said retainer sleeve adapted to extend out said open end of said sleeve responsive to gas pressure and engage and rotate said rotatable cam
  • an explosive charge for generating gas pressure upon detonation disposed within said sleeve between said plunger and said closed end of said sleeve,
  • said means for electrically detonating said explosive charge comprises a bridgewire which vaporizes upon conduction of an electrical current pulse therethrough, said bridgewire being imbedded in said said explosive charge, and in that said first means includes a selfcontained current source.
  • said switching means for switching said first means to temperature dependence of said first means and said switching means which means includes a silicon diode and a silicon PNP transistor.
  • said life vest includes an enclosure for receiving said inflating assembly, said enclosure having a stretched fabric membrane for allowing passage of water and for preventing passage of particulate debris.
  • a parachute strap release mechanism including a webbing frame, a webbing pin pivotably connected at one end to said frame, a side bar for releasably securing the free end of said webbing pin for holding a strap, and a latching means for securing said side bar to said frame, the combination comprising,
  • switching means for switching said first means to generate a current pulse responsive to immersion in water
  • actuator means for disengaging said latching means and for forcing said side bar outward to release said webbing pin responsive to an'electrical current pulse from said first means
  • a chamber having an open end and a closed end
  • a piston disposed in said chamber adapted to extend out said open end of said chamber responsive to gas pressure
  • an explosive charge for generating gas pressure upon detonation disposed within said chamber between said piston and said closed end of said chamber,
  • said means for electrically detonating said explosive charge comprise a bridgewire which vaporizes upon conduction of an electrical current pulse therethrough, and in that said first means includes a self con-l taincd current source.
  • said switching means for switching said first means to generate a current pulse responsive to immersion in water further includes a means for minimizing current leakage from said current source prior to immersion of said release in water.

Abstract

An electronic water-activated package is described for automatically releasing a parachute canopy and inflating a life vest upon immersion in water. Separate electronic water-activated packages are incorporated into frames of break away webbing releases securing the parachute canopy to the parachute harness, and into inflating assemblies located at the bottom of each lapel of a life vest. The electronic water-activated package includes an explosive squib and water sensing circuitry which both detonates the explosive squib and minimizes current leakage from a power supply also contained in the electronics package.

Description

United States Patent [111 3,910,457
Sutliff et al. Oct. 7, 1975 [54] ELECTRONIC WATER-ACTIVATED 3,426,942 2/1969 McMains et a1. 222/5 PARACHUTE RELEASE AND LIFE VEST 3,757,371 9/1973 Martin 222/5 X INFLATOR [75] Inventors: Roderick W. Sutliff, Petaluma; 'T Examlrfer R0bert Reeves David Edwards Novato both of Assistant Examiner-Joseph J. Rolla Calif Attorney, Agent, or Firm-George B. White [73] Assignee: H. Koch & Sons, Inc., Anaheim, I
Calif. [57] ABSTRACT [22] Filed: May 6, 1974 p 7 An electronic water-activated package is described for automatically releasing a parachute canopy and inflating a life vest upon immersion in watenSeparate electronic water-activated packages are incorporated into 211 Appl. No.: 467,298
[52] US. Cl. 222/5; 222/76; 9/316; f e f reak way webbing releases securing the 9/325; 307/246 parachute canopy to the parachute harness, and into [51] Int. Cl. B67B 7/24 inflating assemblies located at the bottom of each [58] Field of Search 222/5, 76 504; 9/83 E lapel of a life vest. The electronic water-activated 9/319, 316, 320, 321, 323, 324, 325, 313, package includes an explosive squib and water sensing 336, 337, 338, 339; 244/149, 152; 307/246 circuitry which both detonates the explosive squib and minimizes current leakage from a power supply also [56] References Cited contained in the electronics package.
UNITED STATES PATENTS 22 Claims, 11 Drawing Figures 3,227,309 l/1966 Segrest 222/5 X US. Patent Oct. 7,1975 Sheet 2 of6 3,910,457
US. Patent Oct. 7,1975 Sheet 3 of6 3,910,457
Fig.6. 32
US. Patent Oct. 7,1975 Sheet 4 of 6 3,910,457
FIG. .9.
'lIu'll U.S. Patent Oct. 7,1975 Sheet 6 of6 3,910,457
ELECTRONIC WATER-ACTIVATED PARACI-IUTE RELEASE AND LIFE VEST INFLATOR BACKGROUND OF THE INVENTION 1. Field of the Invention The invention relates to an electronic wateractivated package for energizing a parachute canopy release mechanism and an inflating assembly in a life vest upon immersion in water. More particularly, the invention relates to an electronics package with a selfcontained power source adapted to be integrally incor-,
porated into a break away webbing frame and into a gas cannister piercing mechanism which, upon immersion in water. triggers an electrical explosive device for energizing the break away release of the webbing frame and for driving the cannister piercing mechanism and which, prior to immersion in water, minimizes current leakage from the power source to give the package a long shelf life.
2. Description of the Prior Art Airmen are sometimes required to eject from a disabled aircraft over water and parachute to safety. To enhance his survival, the airman must, in addition' to executing other survival maneuvers, release himself from the parachute canopy as his feet contact the Water. Otherwise. the parachute canopy may settle around him and he may become entangled in the straps and canopy and drown. Also, the parachute canopy can drag the airman through the water where there are strong surface winds and/or air currents.
The airman must also, soon after contacting the water. inflate his life vest to preserve hisbuoyancy. Such life vests typically include a cannister of compressed gas with a mechanism for piercing the cannister to release the gas into the inflatable portion of the life vest. Typically, such piercing mechanisms require manual manipulation by the pilot.
Frequently, the airmen ejecting from the disabled aircraft are injured or unconscious when they enter the water and cannot carry out the proper manual maneuvers to ensure their survival.
In US. Pat. No. 3,426.942, issued on Feb. ll, I969, to B., D. McMains. et al., a water-sensitive energizing apparatus is described wherein a silicon-controlled rectifier used as a thyristor switch interrupts a circuit loop having a battery and an explosive squib. The McMain apparatus further includes two substantially parallel conductor plates of dissimilar metals to provide a galvanic element. The conductor plates are connected to the battery such that the electrical potential of the galvanic unit opposes that of the battery. Immersion of the plates in water completes the galvanic cell allowing current conduction which switches the thyristor to close the circuit loop between the battery and the explosive squib for detonating the squib.
However, in the McMain circuit, the battery must have a sufficient current capacity to cause the squib to detonate. The galvanic unit saps that current source. In addition, the current conduction characteristics of the galvanic unit are temperature-dependent, thus making the entire circuit temperature-dependent. Another defeet of the McMain circuit is that droplets of water. due to condensation and other debris. can accumulate between the conductor plates to cause a slow current leak which again saps the current capacity of the battery. Moreover. in the McMain circuit. there is a distinct possibility that sufficient water and debris can collect between the plates to cause the thyristor to fire prematurely.
The primary disadvantage of the McMain circuit is that the power source has a relatively short shelf life because of current leakage and, for that reason, must be frequently checked. Such checks are easily forgotten or omitted by human personnel.
SUMMARY OF THE INVENTION An electronic water-activated package is described which automatically energizes a webbing strap release mechanism and a cannister piercing mechanism upon immersion in water. Specifically, separate watersensitive electronic packages are integrally incorporated into break away webbing frames securing a parachute canopy to a parachute harness and into an inflation assembly at the bottom of each lapel of a life vest.
The water-activated electronics package includes a self-contained power source, an electrical explosive device, a capacitor discharge circuit for detonating the electrical explosive device, and a water-sensing circuit which, in addition to triggering the capacitor discharge circuit, also minimizes current leakage from the power source. The invented electronic water-activated package. when incorporated into the break away webbing frame and into the inflation assembly, are completely self-contained and do not require external connections and/or circuitry.
In addition, the elements of the circuit which mini mize current leakage from the power source give the invented electronics package a shelf life on the order of five to ten years. Moreover, by utilizing a capacitor discharge circuit todetonate the explosive device. the power source need only charge the capacitor and is not required to have sufficient current capacity to detonate the explosive device. Finally, the invented release includes electronic elements which render it relatively insensitive to environmental temperature changes.
DESCRIPTION OF THE FIGURES FIG. 1 is a schematic of the electronics package which is integrally mounted within a break away webbing frame.
FIG. 2 is a top view of a break away webbing frame showing the electronics package mounted therein. The webbing frame illustrated also includes male prongs for insertion into a conventional manual release mechanism, also shown.
FIG. 3 is a right-side profile of the break away frame and manual release shown in FIG. 1.
FIG. 4 is a left-side profile of the break away webbing frame shown in FIG. 1 with the cover shield partially cut, away.
FIG. 5 is a partial cutaway, top view, of the release in a locked position.
FIG. 6 is a partial sectional view taken along lines 66 of FIG. 5.
FIG. 7 is a partial cutaway, topview, of the release in its break away configuration.
FIG. 8 is a cutaway sectional view taken along lines 88 of FIG. 7.
FIG. 9 is afrontal view of the life preserver showing the location of the automatic inflating assemblies incorporated into each lower lapel of the preserver.
FIG. 10 is an enlarged cross sectional view of the automatic inflating assembly (detail A of FIG. 9).
FIG. 11 is a cutaway sectional view taken along lines A-A of FIG. 10.
DETAILED DESCRIPTION Description of the Structure of the Break Away Release the free end of the webbing pin and is locked to the I webbing frame 11 by a releasable ball lock detent mechanism 20. Referring to FIGS. 6 and 8, the ball lock detent mechanism includes a hollow cylindrical protrusion 31 extending perpendicularly inward into the webbing frame, 11 from the side bar 16. Coaxially mounted within the protrusion 31 is a springJoaded cylindrical release plunger 32, having a large diameter section 33, conically tapering to a small diameter section 34. A plurality of steel balls are disposed in an equal number of holes through the sidewall of the cylindrical protrusion 31 near its end. When the mechanism is in a locked position, as shown in FIG. 6, the balls rest against the larger diameter section 33 of the release plunger 32. The diameter of the balls 35 are chosen such that they extend beyond the sidewall of this'cylindrical protrusion 31 when resting on the larger diame ter section 33' of the release plunger 32., A spring 37 holds the release plunger 32 in a normally locked" position. V
A cylindrical receptable 38 in the webbing frame 11 receives the locking protrusion 31 of the side bar 16. The receptacle 38 includes an annular shoulder 39 at its entrant end of a slightly smaller diameter than the receptacle for engaging the steel balls 35 of the cylindrical protrusion 31 when the protrusion is in a locking posture. (Sec FIG. 6).
To release the ball lock detent mechanism 20, the release plunger 32 is depressed against the spring 37 allowing the balls 35 to drop down in their respective holes 36 against the smaller diameter section .34 of the release plunger 32 where they cannot engage the annular shoulder 39 of the receptacle 38.
As shown in FIG. 6, the release plunger is depressed by a piston actuator 41 of an electrical explosive cartride unit 40. The cartridge unit includes a cylindrical chamber 42 for receiving the piston actuator 41. An explosive charge 43 is disposed behind the piston actuator 41 and the chamber 42. The unit 40 is secured to a mounting plate 21 and fits within a rectangular reeep tacle 44 within the webbing frame 11. V
In operation, the explosive charge is detonated by an electrical current pulse whereupon hot combustion gases drive the piston actuator 41 outward in its cylindrical chamber 42. The extending piston actuator 41 first depresses the release plunger 32 sufficiently to allow the balls 35 to drop down into their respective holes 36, releasing the lock. The extending piston 41 then engages the end of the cylindrical protrusion 31 to drive the side bar 16 outward to thereby free the end of the webbing pin 14. The tensile force extant on the webbing strap 17 causes the webbing pin 14 to pivot outward-whereupon the strap 17 pulls free as shown in FIG. 7.
Description of the Electronics Referring to FIG. 1, the water-sensing circuitry includes 'a battery BT-l with a positive and negative terminal and an intermediate positive voltage tap. A PNP transistor Q-l switches a silicon-controlled switch Q-2 responsive to current conduction between the two electrodes, 22a and 22b, of the water sensor A-l. The electrodes 22a and 2212 are connected to the positive and negative terminals of the battery BT'1 respectively. The switch Q-2 serially interrupts the current pulsegenerating circuit between the negativeterminal of the battery and a capacitor; C-4. When the siliconcontrolled switch Q-2 is switched to a conducting status, the capacitor C4 is allowed to charge,
The current pulse-generating loopincludes a siliconcontrolled switch Q-4 connected in series between the capacitor C-4 and a bridgewire of an electrical explosive device designated as EED-l. The switch Q-4 is switched to a conducting state by a PNP transistor Q-3 which becomesconducting between the emitter and collector responsive to the potential difference across the capacitor C-4. Upon switching, the switch ()4 discharges the charge buildup. across the. capacitor through the bridgewire EED-l to detonate the electri- 7 BT-I and the base of the transistors 0-1 and 0-3 cal explosive device.
The emitters of the transistors Q-l and Q-3 are connected directly to the positive voltage tap of the battery BT-l. A temperature-compensating diode CR-l isconnected between the positive terminal of the battery .through resistances -R3 and R-6 respectively. The
' diode CR-l is also connected serially between the electrode 22a and the positive terminal of the battery BT-1.
The diode .CR-l renders the described circuit rela-, tively insensitive to environmental temperature changes. Specifically, environmental changes affect the base. voltage potential at which the transistors 0-1 and 0-3 become conducting through their collectors and emitters respectively. In particular,
as temperature increases, a smaller potential difference is required between the bases and emitters of the transistors Q-l and Q-3 to turn on, i.e., become conducting between the emitter-collector connections. The effect of temperature on the transistors 0-1 and Q-3 iscompensated by the diode CR-l in that, as the temperature of the package increases, the forward dropvoltage of the diode CR-l decreases, raising the positive potential on its cathode. The increase of the positive potential on the cathode also increases the positive potential at the base of the PNP transistors Q-l and 0-3. The transistors Q-l and Q-3 and the temperature compensating diode CR-l are chosensueh thatthe increased positive potential supplied by CR-l offsets the I decreased ?turn on potential between the bases and emitters of the transistors 0-1 and 0-3 as temperature increases.
From the above. it should be obvious to those skilled I temperature optimize the function of the circuit. The resistance R-11 between the silicon-controlled switch 0-2 and the capacitor C4 is optional. Specifically, it is designed to limit the amount of current flowing in the current loop defined by the battery and the electrical explosive device.
All of the circuitry elements, including the battery BT-I, are packaged in a unitized metal shield connectcd to the circuitry with a single high-point resistance R-IO to prevent electrostatic charge buildup in the capacitor C4 and to isolate the described circuit from strong electromagnetic fields. The conductors to the electrodes 22a and 22b pass through the shield via ceramic low-pass filter feeds C-2. In addition, a monolithic by-pass capacitor C-3 is connected directly to the base of the transistor Q-l and through resistances R-3 and R-6 to the base of the transistor Q-3.
The described circuit functions as follows: As the water-sensor A-l is immersed in water, the base of the transistor becomes negative due to conduction from the base of 0-1 through the resistance of R1, the water-sensor A-1 and the resistance R-2 to the negative terminal of the battery BT-l. When the potential difference between the base and emitter of Q-l reaches'its turn on threshold, a conduction path is provided through its emitter and collector from the positive voltage tap of the battery BT-l through the resistance R-2 to the negative terminal of the battery BT-l. The potential drop across the resistance R-S causes the gate of the silicon-controlled switch 0-2 to become positive through the resistance of R-4. As the gate of the switch Q-2 becomes positive, it switches to a conducting state allowing the capacitor C-4 to charge through the current-limiting resistance R-11. when the capacitor C4 is fully charged, the turn on potential difference be tween the base and emitter of the transistor Q-3 is reached, thereby allowing conduction through its emitter and collector from the positive voltage tap to the silicon-controlled switch Q-4. The potential drop across R-8 causes the gate of the switch Q-4 to become positive, switching it to a conducting state. Upon switching to a conducting state, the switch Q-4 allows the positive charge built up across the capacitor C-4 to discharge through the electrical explosive device EED-l to detonate the explosive charge.
The described water-sensing circuit not only switches the capacitor-discharge circuit to generate an electrical current pulse, but also minimizes current leakage from the battery BT-l. Specifically, absent a conduction path between the electrodes 22a and 22b of the watersensor A-l, current leakage from the battery BT-l occurs through three circuit elements: l The monolithic capacitor C3 connected between the positive voltage tap of the battery BT-l and the base of the transistor Q-l; (2) The transistor 0-1; and, (3) The siliconcontrolled switch Q-2.
The monolithic capacitor C-3 is chosen to have a minimum insulation resistance greater than 5,000 megohms, such that current leakage through it is reduced to an insignificant value. Evaluation of leakage currents through the transistor Q-I and the silicon-controlled switch Q-2 should be considered at the full-rated voltage of each device at 50. For example, ifQ-l is chosen to have a rated leakage of 35 nanoamps at 45 volts and the switch Q-2 rated to have a leakage of 90 nanoamps at volts, the total maximum leakage is'app'roximately 125 nanoamps at 50C. If the battery BT-] has an available life of 180 M.A.H., the nanoamp leakage represents only about 5.5 M.A.H. of the available battery life. This amount is approximately equal to 3% of the battery life lost in 5 years of storage.
Referring now to FIGS. 4 and 5, the electrical circuitry components are mounted in a unitized metalcovered package and mounted within an L-shaped cavity 19 within the webbing frame 11. The electrical components are sealed from the outside environment by a mounting plate 21 secured to the webbingframe 11. Two water-sensing electrodes 22a and 22b are mounted on the exterior of the mounting plate 21 and are insulated therefrom by the low-pass ceramic feedthrough filters 23. The perforated shield 24 covers the two electrodes 22a and 22b to prevent inadvertent shorting therebetween. The perforations in the shield 24 allow air bubbles to escape from the shiled when the release is immersed in water.
As shown inFIG. 4, electrodes 22a and 22b extend perpendicularly through the mounting plate 21. The post-like configuration of the electrodes 22a and 22b prevent and minimize inadvertent shorting and leakage therebetween due to water condensation or debris. The electrodes are gold-plated to enhance their sensitivity to moisture and water vapor and to maximize their corrosion resistance.
Description of Structure of Life Preserver Inflating Assembly Referring now to FIG. 9, the airman is provided with an inflatable life preserver 46 in which the automatic inflating assembly 47 is incorporated into the bottom section of each lapel of the preserver 46. The automatic inflating assembly 47 includes a cannister 48 containing compressed gas at high pressure, a cannister piercing mechanism 49, and a water-sensing electronics actuator package 51. I
In more detail, referring to FIG. 10 showing the cross-sectional view of the automatic inflating assembly 47, the cannister piercing mechanism 49 comprises a cast structure 52 having a port 53 appropriately threaded for receiving the neck of a high pressure gas cannister 48. A set screw 54 prevents the gas cannister 48 threaded into the port 53 from vibrating free. A piercing pin 56 is located in a passageway 57 through the cast structure 52 in axial alignment with the gas cannister port 53. The piercing pin 56 includes a piercing point 58, a shank 59, an annular shoulder 61, and a rounded head 62. A bushing 63, disposed in the passageway 57, holds the piercing pin 56 in axial alignment with the cannister port 53. A spring 64 is disposed between the bushing 63 and the annular shoulder 61 of the piercing pin 56. An O-ring seal 66 is disposed around the piercing pin 56 between the annular shoulder 61 and the rounded head 62 of the pin. The end of the passageway 57 proximate the gas cannister port 53 defines a gas plenum 67 having a vent 68 which ultimately communicates to the inflatable portion of the life preserver 46 (not shown).
The rounded head 62 of the piercing pin 56 extends out of the passageway 57 and engages a rotatable cam 69. As shown in'FIG. 10, the cam 69 is adapted to rotate clockwise about a pivot pin 71, as indicated by the arrow 72. A manual lever 73 also pivots on the pin 71 and is-adapted to rotate the cam 69 when pulled in the direction of the arrow 74. The cam 69 is also adapted the piercing point 58 of the pin breaks the closure membrane 77 of the gascannister 48. The cam 69 continues to rotate until the recessed section 75 is in alignment with the piercing pin 56, whereupon the combined effect of gas pressure in the cannister and the compressive force of the spring 64 force the pin back out, whereupon the rounded head 62 of the pin is received in the recessed section 75 of the cam 69. Gas vents from the cannister 48 into the plenum 67, then through the vent 68 into the inflatable section of the life preserver.
Referring now to both FIGS. 10 and 11, the watersensing electronic actuator package 51 includes an enclosure 78 adapted to be mounted on the cannister piercing mechanism 49, above the manual actuator lever 73. The package 51 includes a watertight container 79 for receiving batteries 81. The water-sensing circuitry is mounted on a printed circuit board 82. The
enclosurc is then filled with a conventional potting compound 83, isolating the circuit from water and moisture..The transfer plunger 76 of the actuator package 51 is disposed in a retainer sleeve 84. An electrical In more detail, referring to FIG. 1 I, the water-sensing electrodes 22a and 22b, of the water-sensing circuit hereinbefore described each include a central conductive pin 87 extending through the enclosure wall 78 of the actuator package. The extending pins. are surrounded by an insulative sleeve 88 having a relief 89 to expose a portion of the pin 87 to the environment. The reliefs 89in the insulative sleeves face or open in opposite directions to preclude shorting of the electrodes by a small amount of water.
Referring back to FIG. .9, thc'entire automatic inflating assembly 47 is received in an enclosure integral with the life preserver 46. The bottom of the enclosure containing the automatic inflating assembly is sealed from the environment by a stretched nylon, fabric 50. Accordingly, the sensing electrodes 22a and 22b of the water-sensing electronic acutatorpackage 51 are isolated from dust and dirt. However, upon the immersion of the vest in water, water quickly percolates through the stretched nylon fabric 50, establishing electrical conduction between the sensing electrodes 22a and 22b, whereupon the circuit detonates the electrical ex+ plosion device 86 for energizing the transfer plunger76 emplary, representative and schematic embodiments, it should be apparent tothose skilled in;the art that numerous variations and modifications can be effected within the scope and spirit of the invention as described hereinabove and defined and setforth in the appended claims.
We claim:
1. A water-sensitive energizing electrical circuit for detonating electrical explosive devices upon immersion in water comprising, in combination,
a source of electrical current, I
a first meansof generating an electrical current pulse at an output,
a switching means for minimizing current leakage from said current source prior to immersion of said circuit in water and for switching said first means to generate a current pulse responsive to immersion in water, said switching means being con-- nected between said current source and said first means,
and a temperature compensation means for minimiz-- ing temperature dependence of said first means and said switching means respectively, said temperature compensation, means being connected be tween said current source and each of said means respectively.
2. The circuit of claim I further defined in that said electrical current source comprises a battery having a positive terminal, a negative terminal and an intermediate positive voltage tap.
3. The circuit of claim 2 further defined in that first means for generating an electrical current pulsecomprises a capacitor connected between the positive and negative terminals of the battery in parallel with the electrical explosive device, sensing means for sensing electrical potential across said capacitor, said sensing means being connected to said temperature compensating means, a first controlled switching means having a conducting and a non-conducting state connected in series in a circuit loop defined by said capacitor and said and the sensing means and a second resistance connected serially between said gate connection and the negative terminal of the battery, said silicon-controlled switch having non-conducting state when a negative.
potential is impressed on said gate connection and having a conducting state when a positive potential is impressed upon said gate.
5. The circuit of claim 4 further defined in that said sensing means comprises a PNPtransistor having an emitter connected to said intermediate positive voltage tap of the battery, a base connected between said capacitor and said negative terminal of said battery and a collector connected to said first resistance; said PNP transistor having a turn on potential differencebetween the base and emitter at which electrical conduction occurs through the emitter and collector; said temperature-compensating means being connected serially with a resistance between said base of said transistor and said positive terminal of said battery for compensating a decreasing turn on potential difference between said base and said emitter of said transistor as temperature increases, whereby, upon said capacitor becoming fully charged, the potential difference between the base and emitter of the transistor reaches the turn on potential difference and allows conduction of a positive potential from said positive voltage tap through the emitter and collector of the transistor to be impressed upon said gate of said silicon-controlled switch.
6. The circuit of claim 2 further defined in that said switching means for minimizing current leakage from said current source prior to immersion of said circuit in water and for switching said first means to generate a current pulse comprises, in combination,
a first water-sensing electrode electrically connected to the positive terminal of said battery,
a second water-sensing electrode electrically connected to the negative terminal of said battery,'
means for sensing electrical conduction between said first and second electrodes,
a second controlled switching means for allowing current flow to said first means, said second con trolled switching means being serially connected between the negative terminal of said battery and said first means and having a gate connection, said second controlled switching means having a nonconducting state when a negative potential is im pressed upon said gate connection and a conducting state when a positive potential is impressed upon said gate connection, said gate connection being connected to said means for sensing current conduction between said first and second electrodes, whereby said means for sensing conduction between said electrodes impresses a positive potential on said gate of said second controlled switch causing it to become conducting, allowing current flow into first means.
7. The circuit of claim 6 further defined in that said second controlled switching means comprises a siliconcontrolled switch connected serially between said first means and said negative terminal of said battery having a gate connection; a fourth resistance connected serially between said gate connection and said means for sensing current flow between said electrodes and a fifth resistance connected serially between fourth resistance and said negative terminal of said battery.
8. The circuit of claim 7 further defined in that said means for Sensing current conduction between said electrodes comprises, in combination, a second PNP transistor having a base connected between said first electrode and said positive terminal of said battery, an emitter connected to said positive voltage tap of said battery and a collector connected to said fourth resistance; said second transistor having a turn on potential difference between said base and emitter at which electrical current conduction occurs through said emitter and collector; said temperature-compensation means being connected serially between the base of said second transistor and the positive voltage terminal of said battery for compensating a decreasing turn on" potential difference between the base and emitter of said second transistor as temperature increases, whereby current conduction between said first and second electrodes causes a turn on potential difference between said base and emitter of said second transistor allowing a positive potential from said voltage tap to be impressed through the emitter and collector of said second transistor on said gate of said second siliconeontrolled switch to thereby allow current conduction to said first means.
9. The circuit of claim 8 further defined in that said temperature-compensating means comprises a silicon diode and in that said PNP transistor is a silicon PNP transistor.
10. The invention specified in claim 1, and an inflating assembly for an inflatable life vest including a can nister containing high pressure gas, having a piercable closure membrane disposed across a necked section of said cannister, and a structure adapted to hermetically receive said necked section of said cannister for conveying gas from said cannister to said inflatable life vest, the structure comprising a piercing mechanism incorporated into said struc ture adapted to pierce said closure membrane and actuator means for operating said piercing mechanism, responsive to an electrical current pulse from said first means; said first means. said switching means and said actuatormeans being encapsulated in a unitary package adapted to be mounted on said structure.
11. The device of claim 10 wherein said piercing mechanism comprises a piercing pin disposed in a passageway defined through said structure, said passageway communicating with the necked section of said cannister received in said structure, said pin having a point proximate said closure membrane across said necked section of said cannister and having a rounded head extending out of said passageway,
a rotatable cam ,pivotably mounted in said structure, adapted to drive the rounded head of said pin into said passageway upon rotation, to thereby pierce said closure membrane, said rotatable cam being adapted for rotation responsive to said actuator means.
12. The device of claim 11 further defined in that said actuator means comprises, in combination,
a retainer sleeve having an open end and a closed end,
a plunger disposed in said retainer sleeve adapted to extend out said open end of said sleeve responsive to gas pressure and engage and rotate said rotatable cam,
an explosive charge for generating gas pressure upon detonation disposed within said sleeve between said plunger and said closed end of said sleeve,
and means for electrically detonating said charge whereby said plunger moves outward from said sleeve responsive to gas pressure generated by said exploding charge to rotate said cam and drive said piercing pin through said closure membrane of said cannisterv 13. The device of claim 12 further defined in that said means for electrically detonating said explosive charge comprises a bridgewire which vaporizes upon conduction of an electrical current pulse therethrough, said bridgewire being imbedded in said said explosive charge, and in that said first means includes a selfcontained current source.
14. The device of claim 13 further definedin that said switching means for switching said first means to temperature dependence of said first means and said switching means which means includes a silicon diode and a silicon PNP transistor.
17. The device of claim 16 further defined in that said life vest includes an enclosure for receiving said inflating assembly, said enclosure having a stretched fabric membrane for allowing passage of water and for preventing passage of particulate debris.
18. The device of claim 14 here further defined in that said current source comprises a battery.
19. ln a parachute strap release mechanism, including a webbing frame, a webbing pin pivotably connected at one end to said frame, a side bar for releasably securing the free end of said webbing pin for holding a strap, and a latching means for securing said side bar to said frame, the combination comprising,
a first means for generating an electrical current pulse at an output,
switching means for switching said first means to generate a current pulse responsive to immersion in water,
actuator means for disengaging said latching means and for forcing said side bar outward to release said webbing pin responsive to an'electrical current pulse from said first means,
and temperature-compensating means for minimizing the temperature dependence of said first means and said switching means; said first means, said switching means, said actuator means and said temperature-compensating means being encapsulated in a unitary package .mounted integrally within said webbing frame.
20. The device of claim 19 further defined in that said actuator means comprises, in combination,
a chamber having an open end and a closed end,
a piston disposed in said chamber adapted to extend out said open end of said chamber responsive to gas pressure,
an explosive charge for generating gas pressure upon detonation disposed within said chamber between said piston and said closed end of said chamber,
and means for electrically detonating said charge whereby said piston moves outward from said chamber responsive to gas pressure generated by said charge to disengage said latching means and to force said side bar outward to thereby release said webbing pin.
21. The device described in claim 20 further defined.
in that said means for electrically detonating said explosive charge comprise a bridgewire which vaporizes upon conduction of an electrical current pulse therethrough, and in that said first means includes a self con-l taincd current source.
22. The device described in claim 21 further defined in that said switching means for switching said first means to generate a current pulse responsive to immersion in water further includes a means for minimizing current leakage from said current source prior to immersion of said release in water.
l= l l

Claims (22)

1. A water-sensitive energizing electrical circuit for detonating electrical explosive devices upon immersion in water comprising, in combination, a source of electrical current, a first means of generating an electrical current pulse at an output, a switching means for minimizing current leakage from said current source prior to immersion of said circuit in water and for switching said first means to generate a current pulse responsive to immersion in water, said switching means being connected between said current source and said first means, and a temperature compensation means for minimizing temperature dependence of said first means and said switching means respectively, said temperature compensation means being connected between said current source and each of said means respectively.
2. The circuit of claim 1 further defined in that said electrical current source comprises a battery having a positive terminal, a negative terminal and an intermediate positive voltage tap.
3. The circuit of claim 2 further defined in that first means for generating an electrical current pulse comprises a capacitor connected between the positive and negative terminals of the battery in parallel with the electrical explosive device, sensing means for sensing electrical potential across said capacitor, said sensing means being connected to said temperature compensating means, a first controlled switching means having a conducting and a non-conducting state connected in series in a circuit loop defined by said capacitor and said electrical explosive device and having a gate connected to said sensing means whereby said first controlled switching means changes from a non-conducting to a conducting state responsive to a signal from said sensing means allowing electrical charge buildup across said capacitor to discharge through said electrical explosive device.
4. The circuit of claim 3 further defined in that said first controlled switching means comprises a silicon-controlled switch having a gate connection; a first resistance connected serially between the gate connection and the sensing means and a second resistance connected serially between said gate connection and the negative terminal of the battery, said silicon-controlled switch having a non-conducting state when a negative potential is impressed on said gate connection and having a conducting state when a positive potential is impressed upon said gate.
5. The circuit of claim 4 further defined in that said sensing means comprises a PNP transistor having an emitter connected to said intermediate positive voltage tap of the battery, a base connected between said capacitor and said negative terminal of said battery and a collector connected to said first resistance; said PNP transistor having a ''''turn on'''' potential difference between the base and emitter at which electrical conduction occurs through the emitter and collector; said temperature-compensating means being connected serially with a resistance between said base of said transistor and said positive terminal of said battery for compensating a decreasing ''''turn on'''' potential difference between said base and said emitter of said transistor as temperature increases, whereby, upon said capacitor becoming fully charged, the potential difference between the base and emitter of the transistor reaches the ''''turn on'''' potential difference and allows conduction of a positive potential from said positive voltage tap through the emitter and collector of the transistor to be impressed upon said gate of said silicon-controlled switch.
6. The circuit of claim 2 further defined in that said switching means for minimizing current leakage from said current source prior to immersion of said circuit in water and for switching said first means to generate a current pulse comprises, in combination, a first water-sensing electrode electrically connected to the positive terminal of said battery, a second water-sensing electrode electrically connected to the negative terminal of said battery, means for sensing electrical conduction between said first and second electrodes, a second controlled switching means for allowing current flow to said first means, said second controlled switching means being serially connected between the negative terminal of said battery and said first means and having a gate connection, said second controlled switching means having a non-conducting state when a negative potential is impressed upon said gate connection and a conducting state when a positive potential is impressed upon said gate connection, said gate connection being connected to said means for sensing current conduction between said first and second electrodes, whereby said means for sensing conduction between said electrodes impresses a positive potential on said gate of said second controlled switch causing it to become conducting, allowing current flow into first means.
7. The circuit of claim 6 further defined in that said second controlled switching means comprises a silicon-controlled switch connected serially between said first means and said negative terminal of said battery having a gate connection; a fourth resistance connected serially between said gate connection and said means for sensing current flow between said electrodes and a fifth resistance connected serially between fourth resistance and said negative terminal of said battery.
8. The circuit of claim 7 further defined in that said means for sensing current conduction between said electrodes comprises, in combination, a second PNP transistor having a base connected between said first electrode and said positive terminal of said battery, an emitter connected to said positive voltage tap of said battery and a collector connected to said fourth resistance; said second transistor having a ''''turn on'''' potential difference between said base and emitter at which electrical current conduction occurs through said emitter and collector; said temperature-compensation means being connected serially between the base of said second transistor and the positive voltage terminal of said battery for compensating a decreasing ''''turn on'''' potential difference between the base and emitter of said second transistor as temperature increases, whereby current conduction between said first and second electrodes causes a ''''turn on'''' potential difference between said base and emitter of said second transistor allowing a positive potential from said voltage tap to be impressed through the emitter and collector of said second transistor on said gate of said second silicon-controlled switch to thereby allow current conduction to said first means.
9. The circuit of claim 8 further defined in that said temperature-compensating means comprises a silicon diode and in that said PNP transistor is a silicon PNP transistor.
10. The invention specified in claim 1, and an inflating assembly for an inflatable life vest including a cannister containing high pressure gas, having a piercable closure membrane disposed across a necked section of said cannister, and a structure adapted to hermetically receive said necked section of said cannister for conveying gas from said cannister to said inflatable life vest, the structure comprising a piercing mechanism incorporated into said structure adapted to pierce said closure membrane and actuator means for operating said piercing mechanism, responsive to an electrical current pulse from said first means; said first means, said switching means and said actuator means being encapsulated in a unitary package adapted to be mounted on said structure.
11. The device of claim 10 wherein said piercing mechanism comprises a piercing pin disposed in a passageway defined through said structure, said passageway communicating with the necked section of said cannister received in said structure, said pin having a point proximate said closure membrane across said necked section of said cannister and having a rounded head extending out of said passageway, a rotatable cam pivotably mounted in said structure, adapted to drive the rounded head of said pin into said passageway upon rotation, to thereby pierce said closure membrane, said rotatable cam being adapted for rotation responsive to said actuator means.
12. The device of claim 11 further defined in that said actuator means comprises, in combination, a retainer sleeve having an open end and a closed end, a plunger disposed in said retainer sleeve adapted to extend out said open end of said sleeve responsive to gas pressure and engage and rotate said rotatable cam, an explosive charge for generating gas pressure upon detonation disposed within said sleeve between said plunger and said closed end of said sleeve, and means for electrically detonating said charge whereby said plunger moves outward from said sleeve responsive to gas pressure generated by said exploding charge to rotate said cam and drive said piercing pin through said closure membrane of said cannister.
13. The device of claim 12 further defined in that said means for electrically detonating said explosive charge comprises a bridgewire which vaporizes upon conduction of an electrical current pulse therethrough, said bridgewire being imbedded in said said explosive charge, and in that said first means includes a self-contained current source.
14. The device of claim 13 further defined in that said switching means for switching said first means to generate a current pulse in response to immersion in water further includes a means for minimizing current leakage from said current source prior to immersion of said assembly in water.
15. The device of claim 14 wherein said piercing mechanism further includes a lever pivotably mounted on said structure for rotating said rotatable cam, whereby said piercing mechanism can be operated manually by said lever.
16. The device of claim 15 further comprising a temperature-compensating means for minimizing the temperature dependence of said first means and said switching means which means includes a silicon diode and a silicon PNP transistor.
17. The device of claim 16 further defined in that said life vest includes an enclosure for receiving said inflating assembly, said enclosure having a stretched fabric membrane for allowing passage of water and for preventing passage of particulate debris.
18. The device of claim 14 here further defined in that said current source comprises a baTtery.
19. In a parachute strap release mechanism, including a webbing frame, a webbing pin pivotably connected at one end to said frame, a side bar for releasably securing the free end of said webbing pin for holding a strap, and a latching means for securing said side bar to said frame, the combination comprising, a first means for generating an electrical current pulse at an output, switching means for switching said first means to generate a current pulse responsive to immersion in water, actuator means for disengaging said latching means and for forcing said side bar outward to release said webbing pin responsive to an electrical current pulse from said first means, and temperature-compensating means for minimizing the temperature dependence of said first means and said switching means; said first means, said switching means, said actuator means and said temperature-compensating means being encapsulated in a unitary package mounted integrally within said webbing frame.
20. The device of claim 19 further defined in that said actuator means comprises, in combination, a chamber having an open end and a closed end, a piston disposed in said chamber adapted to extend out said open end of said chamber responsive to gas pressure, an explosive charge for generating gas pressure upon detonation disposed within said chamber between said piston and said closed end of said chamber, and means for electrically detonating said charge whereby said piston moves outward from said chamber responsive to gas pressure generated by said charge to disengage said latching means and to force said side bar outward to thereby release said webbing pin.
21. The device described in claim 20 further defined in that said means for electrically detonating said explosive charge comprise a bridgewire which vaporizes upon conduction of an electrical current pulse therethrough, and in that said first means includes a self contained current source.
22. The device described in claim 21 further defined in that said switching means for switching said first means to generate a current pulse responsive to immersion in water further includes a means for minimizing current leakage from said current source prior to immersion of said release in water.
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Cited By (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4382231A (en) * 1980-11-17 1983-05-03 Conax Corporation Fluid conductivity sensor
US4464128A (en) * 1980-12-03 1984-08-07 Yanmar Diesel Engine Company Ltd. Seal arrangement between an outdrive unit and a hull of a vessel
US4513248A (en) * 1980-11-17 1985-04-23 Conax Corporation Fluid conductivity sensor
FR2609178A1 (en) * 1986-12-30 1988-07-01 Conax Florida Corp Fluid conductivity detector
FR2610723A1 (en) * 1987-02-11 1988-08-12 Conax Florida Corp SENSOR FOR CONDUCTIVITY OF A FLUID
US4927057A (en) * 1989-05-30 1990-05-22 Inflation Technologies & Innovation Automatic inflator for inflatable articles
US4972971A (en) * 1989-06-29 1990-11-27 Inflation Technologies & Innovation Automatic inflator for inflatable articles
US5035345A (en) * 1990-05-07 1991-07-30 Apoc, Inc. Automatic inflator for inflatable articles
US5400922A (en) * 1992-07-14 1995-03-28 Halkey-Roberts Corporation Electric autoinflator
US5509576A (en) * 1992-07-14 1996-04-23 Halkey-Roberts Corporation Electric autoinflator
US5839933A (en) * 1997-08-14 1998-11-24 Davis, Sr.; Claude D. Inflatable life vest
WO2003022367A2 (en) 2001-09-07 2003-03-20 Halkey-Roberts Corporation Bobbin for automatic inflator
WO2003022631A2 (en) 2001-09-07 2003-03-20 Halkey-Roberts Corporation Automatic inflator with status indicator
US20060160444A1 (en) * 2005-01-19 2006-07-20 Campbell Richard A Automatic inflation device having a moisture activated trigger and release system with reduced force applied to the degradable element
WO2007038863A2 (en) * 2005-10-05 2007-04-12 Irvin Aerospace Canada Limited Heavy payload parachute ground disconnecting device
US20070277903A1 (en) * 2006-05-16 2007-12-06 Halkey-Roberts Corporation Heat sealable inflator
US20110000550A1 (en) * 2009-04-15 2011-01-06 Rogier Stephen J Manual Inflator With Cylinder Connector and Status Indicator
US20110260005A1 (en) * 2007-01-05 2011-10-27 Airborne Systems Canada Ltd. Parachute ground disconnecting device
WO2014110631A1 (en) * 2013-01-21 2014-07-24 Zactill Intellectual Property Pty Ltd Safety device and adapter therefor
US9071387B1 (en) 2014-01-08 2015-06-30 Timothy Patrick Dunnigan Threat response signal inhibiting apparatus for radio frequency controlled devices and corresponding methods
US10017231B2 (en) 2015-03-23 2018-07-10 Halkey-Roberts Corporation Indicator for manual inflator
US10730595B2 (en) 2018-06-13 2020-08-04 Halkey-Roberts Corporation Disposable inflator
US10994818B2 (en) 2018-04-06 2021-05-04 Halkey-Roberts Corporation Bobbin for automatic inflator
US11014641B1 (en) 2019-11-11 2021-05-25 Aerial Machine & Tool Corporation Wearable flotation device
US11180230B2 (en) * 2018-06-13 2021-11-23 Halkey-Roberts Corporation Disposable Inflator
US11346690B2 (en) * 2020-01-10 2022-05-31 Boston Engineering Corporation Device with water-activated, automatic disconnect

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US3227309A (en) * 1964-08-18 1966-01-04 Jack L Hearrell Inflating device with means for testing the condition of a charging cartridge
US3426942A (en) * 1967-07-31 1969-02-11 Jay El Products Inc Water-responsive energizing apparatus
US3757371A (en) * 1970-12-21 1973-09-11 J Martin Survival or like packs particularly suitable for airmen

Cited By (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4382231A (en) * 1980-11-17 1983-05-03 Conax Corporation Fluid conductivity sensor
US4513248A (en) * 1980-11-17 1985-04-23 Conax Corporation Fluid conductivity sensor
US4464128A (en) * 1980-12-03 1984-08-07 Yanmar Diesel Engine Company Ltd. Seal arrangement between an outdrive unit and a hull of a vessel
FR2609178A1 (en) * 1986-12-30 1988-07-01 Conax Florida Corp Fluid conductivity detector
FR2610723A1 (en) * 1987-02-11 1988-08-12 Conax Florida Corp SENSOR FOR CONDUCTIVITY OF A FLUID
US4927057A (en) * 1989-05-30 1990-05-22 Inflation Technologies & Innovation Automatic inflator for inflatable articles
US4972971A (en) * 1989-06-29 1990-11-27 Inflation Technologies & Innovation Automatic inflator for inflatable articles
US5035345A (en) * 1990-05-07 1991-07-30 Apoc, Inc. Automatic inflator for inflatable articles
US5400922A (en) * 1992-07-14 1995-03-28 Halkey-Roberts Corporation Electric autoinflator
US5509576A (en) * 1992-07-14 1996-04-23 Halkey-Roberts Corporation Electric autoinflator
US5839933A (en) * 1997-08-14 1998-11-24 Davis, Sr.; Claude D. Inflatable life vest
WO2003022367A2 (en) 2001-09-07 2003-03-20 Halkey-Roberts Corporation Bobbin for automatic inflator
WO2003022631A2 (en) 2001-09-07 2003-03-20 Halkey-Roberts Corporation Automatic inflator with status indicator
US6589087B2 (en) 2001-09-07 2003-07-08 Halkey-Roberts Corporation Automatic inflator with status indicator
US6705488B2 (en) 2001-09-07 2004-03-16 Halkey-Roberts Corporation Bobbin for automatic inflator
US7572161B2 (en) 2001-09-07 2009-08-11 Halkey-Roberts Corporation Bobbin for automatic inflator
US20060160444A1 (en) * 2005-01-19 2006-07-20 Campbell Richard A Automatic inflation device having a moisture activated trigger and release system with reduced force applied to the degradable element
US7357689B2 (en) 2005-01-19 2008-04-15 Campbell Richard A Automatic inflation device having a moisture activated trigger and release system with reduced force applied to the degradable element
WO2007038863A3 (en) * 2005-10-05 2007-11-08 Irvin Aerospace Canada Ltd Heavy payload parachute ground disconnecting device
US20070080259A1 (en) * 2005-10-05 2007-04-12 Irvin Aerospace Canada Limited Heavy payload parachute ground disconnecting device
WO2007038863A2 (en) * 2005-10-05 2007-04-12 Irvin Aerospace Canada Limited Heavy payload parachute ground disconnecting device
US20070277903A1 (en) * 2006-05-16 2007-12-06 Halkey-Roberts Corporation Heat sealable inflator
US7475711B2 (en) 2006-05-16 2009-01-13 Halkey-Roberts Corporation Heat sealable inflator
US20110260005A1 (en) * 2007-01-05 2011-10-27 Airborne Systems Canada Ltd. Parachute ground disconnecting device
US20110000550A1 (en) * 2009-04-15 2011-01-06 Rogier Stephen J Manual Inflator With Cylinder Connector and Status Indicator
US8360276B2 (en) 2009-04-15 2013-01-29 Halkey-Roberts Corporation Manual inflator with cylinder connector and status indicator
US20150314843A1 (en) * 2013-01-21 2015-11-05 Zactill Intellectual Property Pty Ltd Safety Device and Adapter Therefor
CN105026258A (en) * 2013-01-21 2015-11-04 达科迪尔知识产权私人有限公司 Safety device and adapter therefor
WO2014110631A1 (en) * 2013-01-21 2014-07-24 Zactill Intellectual Property Pty Ltd Safety device and adapter therefor
EP2945855A4 (en) * 2013-01-21 2016-11-16 Zactill Intellectual Property Pty Ltd Safety device and adapter therefor
US9071387B1 (en) 2014-01-08 2015-06-30 Timothy Patrick Dunnigan Threat response signal inhibiting apparatus for radio frequency controlled devices and corresponding methods
US9716566B2 (en) 2014-01-08 2017-07-25 Timothy Patrick Dunnigan Threat response signal inhibiting apparatus for radio frequency controlled devices and corresponding methods
US10103836B2 (en) 2014-01-08 2018-10-16 Timothy Patrick Dunnigan Threat response signal inhibiting apparatus for radio frequency controlled devices and corresponding methods
US10017231B2 (en) 2015-03-23 2018-07-10 Halkey-Roberts Corporation Indicator for manual inflator
US10994818B2 (en) 2018-04-06 2021-05-04 Halkey-Roberts Corporation Bobbin for automatic inflator
US10730595B2 (en) 2018-06-13 2020-08-04 Halkey-Roberts Corporation Disposable inflator
US11180230B2 (en) * 2018-06-13 2021-11-23 Halkey-Roberts Corporation Disposable Inflator
US11014641B1 (en) 2019-11-11 2021-05-25 Aerial Machine & Tool Corporation Wearable flotation device
US11346690B2 (en) * 2020-01-10 2022-05-31 Boston Engineering Corporation Device with water-activated, automatic disconnect

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