Initiator

Abstract

An initiator including a housing adapted to be received in an igniter or rocket motor, at least one charge at a distal end of the housing, an electro-explosive device behind the charge for detonating the charge when subject to a voltage HV, and a pressure bulkhead behind the electro-explosive device. An electronic subsystem in the housing is connected to the electro-explosive device through the bulkhead and includes a lead for providing the voltage HV to the electro-explosive device to initiate it, and a switch in the lead which does not conduct if errant voltages are present on the lead to prevent initiation of the electro-explosive device until the correct voltage HV is present.

Claims

1. An initiator comprising: a housing adapted to be received in an igniter or rocket motor; at least one charge at a distal end of the housing; an electro-explosive device behind the charge for detonating the charge when subject to a voltage; a pressure bulkhead behind the electro-explosive device, and an electronic subsystem in the housing connected to the electro-explosive device through the bulkhead and including: a lead for providing the voltage to the electro-explosive device to initiate it, and a switch in the lead which does not conduct if errant voltages are present on the lead to prevent initiation of the electro-explosive device until the correct voltage is present.

2. The initiator in claim 1 in which there are two charges in the distal end of the housing.

3. The initiator of claim 2 in which one charge is a pyrotechnic material and the other charge is a detonating material.

4. The initiator of claim 3 in which the pyrotechnic material includes BKNO.sub.3 and the detonating material includes HNS-IV.

5. The initiator of claim 1 in which the electro-explosive device is an exploding foil initiator.

6. The initiator of claim 1 in which the switch is a spark gap.

7. The initiator of claim 6 in which the electronic subsystem further includes a resistance in series with the spark gap for limiting current.

8. The initiator of claim 6 further including a capacitance charged by a voltage on the lead.

9. The initiator of claim 7 further including a resistance in parallel with the capacitance.

10. An initiator comprising: a housing adapted to be received in an igniter or rocket motor; at least one charge in the distal end of the housing; an electro-explosive device behind the charge for detonating the charge when subject to a voltage; a pressure bulkhead behind the electro-explosive device, and an electronic subsystem in the housing connected to the electro-explosive device through the bulkhead and including: a lead for providing the voltage HV to the electro-explosive device to initiate it, and means for preventing errant voltages from initiating the electro-explosive device.

11. The initiator of claim 10 in which said means includes a spark gap.

Description

BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS

(1) Other objects, features and advantages will occur to those skilled in the art from the following description of a preferred embodiment and the accompanying drawings, in which:

(2) FIG. 1 is a highly schematic three-dimensional side view of an example of an initiator in accordance with the subject invention;

(3) FIG. 2 is a schematic cross-sectional side view of the initiator shown in FIG. 1;

(4) FIG. 3 is a circuit diagram showing an example of an over voltage protection circuit for an initiator in accordance with this invention;

(5) FIGS. 4-7 are circuit diagrams showing examples of other possible over voltage protection circuits for an initiator in accordance with the subject invention; and

(6) FIGS. 8-9 are schematic cross-sectional diagrams showing another example of an initiator in accordance with the subject invention.

DETAILED DESCRIPTION OF THE INVENTION

(7) Aside from the preferred embodiment or embodiments disclosed below, this invention is capable of other embodiments and of being practiced or being carried out in various ways. Thus, it is to be understood that the invention is not limited in its application to the details of construction and the arrangements of components set forth in the following description or illustrated in the drawings. If only one embodiment is described herein, the claims hereof are not to be limited to that embodiment. Moreover, the claims hereof are not to be read restrictively unless there is clear and convincing evidence manifesting a certain exclusion, restriction, or disclaimer.

(8) Initiator 10, FIG. 1, in one example, includes housing 12 (typically metal) with three sections. Distal charge section 14 (usually including threads 15) is typically received in an igniter itself received in a motor. Or, initiator 10 may include an igniter in which case section 14 would be received in the rocket motor. Pressure bulkhead 16 separates charge section 14 from proximal end electronic section 18 which has leads, such as leads 20a and 20b (e.g., wire or pins). Initiator 10 is in compliance with MIL-STD-1901A in that if a voltage 500 volts or less is present on leads 20a or 20b, initiator 10 will not deflagrate as explained below.

(9) FIG. 2 shows one preferred design of initiator 10. In this example, charge section 14 includes output charge 30 (e.g., a pyrotechnic material such as BKNO.sub.3) and detonating charge 32 (an energetic material such as HNS-IV) behind end wall 33. U.S. Pat. No. 6,546,837 by the assignee hereof, incorporated herein by this reference, describes how two such charges can be consolidated, if desired. An electro-explosive device 34 such as an exploding foil initiator (chip slapper) detonates charge 32 when subject to a high voltage (HV) (e.g. 1200V). U.S. Pat. No. 6,178,888 by the assignee hereof and also incorporated herein by this reference discloses barrel connector 35 which may be used if desired as well as the other components of a preferred exploding foil initiator.

(10) Electronics subsection 36 is behind bulkhead 16 within housing section 18 and is electrically connected to exploding foil initiator 34 via leads 21a and 21b extending through pressure bulkhead 16. A glass to metal sealing material as shown at 38 may be used to seal leads 21a and 21b with respect to the metal bulkhead material. Leads 20a and 20b are electrically connected to electronic subsystem 36 though proximate housing closure disk or end wall 48.

(11) Electronics subsystem 36 includes means such as a switch which does not conduct if errant voltages less than 500 volts are present on lead 20a. This feature renders initiator 10 compliant with MIL-STD-1901A. Typically, electronic subsystem 36 includes a circuit board or integrated circuitry for the various circuits and components of the electronics subsystem.

(12) In one example shown in FIG. 3, the switch is a spark gap 40 configured to not conduct if a voltage less than 1,000 volts is present on high voltage lead 20a. Any voltage less than this breakdown voltage will charge capacitor 42 (e.g. a 0.1 microfarad capacitor) but will not allow any current to flow to electro-explosive device 34. Moreover, even if spark gap 40 fails so the breakdown voltage is less than 500 volts, resistor 46, FIG. 3 (e.g., 10-100 KO) provides a current limit. As shown, resistor 44 is in parallel with capacitor 42 between high voltage lead 20a and common lead 20b. Resistor 46 is in series with spark gap 40.

(13) Instead of spark gap 40, a solid state switch could be used, which conducts only when it receives a predetermined voltage level or a signal. A high voltage zener diode could also be used. Other switches and related circuitry are known to those skilled in the art.

(14) FIG. 4 shows another configuration of an electronic subsystem with capacitor bleeder resistor 51 that could be printed on the high voltage capacitor. FIG. 4 also shows a resistor divider 50 in parallel with the bleeder resistor that provides redundant bleeding as well as providing a scaled down indication of the charge voltage. Typical for these resistors might be 40 M for R2 and 100 K for R3. FIG. 4 also shows a high voltage diode 52 in-line with the input voltage.

(15) FIG. 5 shows another electronic configuration. This configuration is designed to take a lower AC voltage and multiply it (by a factor of 2) to arrive at a larger voltage. FIG. 6 shows a configuration incorporating a high voltage switch 60 such as a MOS Controlled Thyristor (MCT). The MCT 60 is off until driven to conduction by a gate driver. The gate driver requires an input voltage plus a trigger signal to drive the MCT. FIG. 7 shows a similar configuration to FIG. 6, except that the MCT 60 is automatically switched when the main charge capacitor reaches a predetermined voltage.

(16) In this way, the long felt need for MIL-STD-1901A compliant high-voltage initiator is realized. The initiator is easily fitted into existing rocket motors, is fairly simple in design, and is easy to install.

(17) FIGS. 8-9 show an initiator 100 in accordance with another example. Housing portion 102 includes the over voltage protection circuitry 103 (see FIGS. 3-6). Electro-explosive device 104 with exploding foil initiator 106 and charge 108 (e.g., HNS-IV) at the distal end of housing portion 102 and within housing portion 105 is electrically connected to circuitry 103 via pins 110a and 110b received in sockets 112a and 112b, respectively, through pressure bulkhead 114.

(18) This initiator assembly is received in igniter 116 which includes charge 118a (e.g., HNS-IV) and charge 118b (e.g., BKNO.sub.3). When the proper voltage is applied to exploding foil initiator 106, charge 108 detonates and the resulting shock wave through igniter housing wall 120 detonates charge 118a which detonates charge 118b. In one design, housing portion 102 is integrated with housing portion 116.

(19) Although specific features of the invention are shown in some drawings and not in others, this is for convenience only as each feature may be combined with any or all of the other features in accordance with the invention. The words including, comprising, having, and with as used herein are to be interpreted broadly and comprehensively and are not limited to any physical interconnection. Moreover, any embodiments disclosed in the subject application are not to be taken as the only possible embodiments.

(20) In addition, any amendment presented during the prosecution of the patent application for this patent is not a disclaimer of any claim element presented in the application as filed: those skilled in the art cannot reasonably be expected to draft a claim that would literally encompass all possible equivalents, many equivalents will be unforeseeable at the time of the amendment and are beyond a fair interpretation of what is to be surrendered (if anything), the rationale underlying the amendment may bear no more than a tangential relation to many equivalents, and/or there are many other reasons the applicant can not be expected to describe certain insubstantial substitutes for any claim element amended.

(21) Other embodiments will occur to those skilled in the art and are within the following claims.