# US 9,518,809 B2 · Electro-mechanical fuze for a projectile > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 9,518,809 B2 - Document ID: US9518809B2 - Status: Granted - Kind: B2 - Application number: 14/844,005 - Filed: 2015-09-03 - Published: 2015-12-31 - Granted: 2016-12-13 - Earliest claimed: 2011-04-02 - Assignees: Advanced Material Engineering Pte Ltd - Applicants: Advanced Material Engineering Pte Ltd - Inventors: Cheng Hok Aw; Juan Kiat Jeremy Quek; Yong Lim Thomas Ang; Siwei Huang; Soo Chew Sie - Web page: https://patentgrep.com/patent/US9518809B2 ## CPC - F42C 1/02: with firing-pin structurally combined with fuze - F42C 9/16: for self-destruction of ammunition {(F42C9/141 - F42C9/148 take precedence)} - F42C 11/00: Electric fuzes ({in combination with other fuzes F42C9/14}; proximity fuzes F42C13/00; {safety or arming effected by electric means F42C15/40; electric contact parts for fuzes F42C19/06}; electric igniters F42C19/12, {F42B3/12 - F42B3/18; optical initiators F42B3/113}) - F42C 11/008: {Power generation in electric fuzes (F42C11/02, F42C11/04 and F42C15/295 take precedence)} - F42C 11/02: with piezo-crystal - F42C 15/188: using a rotatable carrier - F42C 15/40: wherein the safety or arming action is effected electrically - F42C: AMMUNITION FUZES (blasting cartridge initiators F42B3/10; chemical aspects C06C); ARMING OR SAFETY MEANS THEREFOR (filling fuzes F42B33/02; fitting or extracting primers in or from fuzes F42B33/04; containers for fuzes F42B39/30) ## Abstract The present invention describes an electronic fuze operable to complement a mechanical point impact fuze. The electronic fuze includes a voltage generator circuit, micro-controller, a piezo-electric sensor, a firing circuit and a safety lockout circuit. When a projectile strikes a target at an optimum angle, the mechanical point impact fuze is activated; when the strike angle is oblique, the mechanical point impact fuze may be ineffective but the piezo-electric sensor is operable to trigger the firing circuit. The safety lockout circuit ensures the firing circuit is operative only after a predetermined delay time when an n-channel FET is turned OFF. The micro-controller also generates a TIME-OUT signal, which provides for self-destruction of a projectile that has failed to explode. ## Claims ### Claim 1 A method of controlling a fuze for a projectile, said method comprising: coupling a signal of a piezo-electric sensor and a safety lockout circuit to an electronic firing circuit; wherein the safety lockout circuit is safety locking out the electronic firing circuit to ground until said projectile has been propelled through a tactical distance; during the propelled flight, said piezo-electric sensor generating and sending a firing signal to said electronic firing circuit; said electronic firing circuit setting off an electric detonator in an impact sensing mode, depending on said safety lockout circuit, or in a self-destruct mode; and detonating said electric detonator in turn to actuate a firing pin to set off a stab detonator disposed in said projectile, with said electric detonator being disposed co-axially with said firing pin. ### Claim 2 (depends on 1) The method according to claim 1, wherein said coupling a signal of said piezo-electric sensor to said electronic firing circuit comprises sending said signal to control a gate of a silicon-controlled rectifier (SCR). ### Claim 3 (depends on 1) The method according to claim 1, wherein coupling a safety lockout circuit to said electronic firing circuit comprises controlling a gate voltage line of an n-channel field-effect transistor (FET), whose drain is connected to a gate of a silicon-controlled rectifier (SCR) and source is connected to ground, said FET gate voltage supplied by a voltage pulse Vin from a set-back generator is initially high enough to turn ON said n-channel FET so that said firing signal is pulled to ground to disarm said electronic firing circuit; and after a predetermined time when said projectile has reached the tactical distance, said FET gate voltage becomes too low to hold said n-channel FET in conduction, said n-channel FET is turned OFF and results in said safety lockout circuit being deactivated and said firing signal is then sent to said gate of said SCR to turn said SCR ON, which in response is operable to set off said electric detonator. ### Claim 4 (depends on 3) The method according to claim 3, further controlling said firing circuit by a micro-controller, which outputs ARM, piezo enable (or PIEZO_EN) and piezo clear (or PIEZO-CLR) signals according to predetermined clock periods set in said micro-controller. ### Claim 5 (depends on 4) The method according to claim 4, further comprises inputting a spin-loss signal to said micro-controller for said micro-controller to output a TIME_OUT self destruct signal. ### Claim 6 (depends on 5) The method according to claim 5, further comprises latching said PIEZO_EN signal to provide a PIEZO_TRG output signal in response to a clock signal provided by output of said piezo electric sensor and a piezoelectric clear (or PIEZO_CLR) signal from said micro-controller. ### Claim 7 (depends on 6) The method according to claim 6, further comprises comparing output voltage of said piezo-electric sensor with a reference voltage. ### Claim 8 (depends on 7) The method according to claim 7, wherein said micro-controller outputting a digital-to-analogue (DAC) signal, which is operable to drive said reference voltage. ### Claim 9 (depends on 8) The method according to claim 8, wherein said DAC signal is time varied from a high to a relative low level, so that sensitivity of said piezoelectric sensor is responsively increased as said projectile approaches its target. ### Claim 10 (depends on 4) The method according to claim 4, further comprises connecting said ARM signal to said gate voltage line of said n-channel FET. ### Claim 11 (depends on 10) The method according to claim 10, wherein said ARM signal comprises a high-to-low signal. ### Claim 12 (depends on 1) The method according to claim 1, further comprises rotating a stab detonator disposed on a safe-and-arm assembly unit to be in line with said firing pin after said projectile has been propelled to a minimum muzzle safety distance. ### Claim 13 (depends on 12) The method according to claim 12, wherein said firing pin is operable to set off said stab detonator in a point detonating mode and said electronic firing circuit is operable to set off said electric detonator in an impact sensing mode or in a self-destruct mode.