The present invention relates primarily to the field of tactical or guided rockets and missiles, and more particularly, to a hybrid electronic and electromechanical arm-fire device.
The prior art arm and fire devices used in rockets and missiles fall into two categories: electronic, and electromechanical. The prior art electronic devices lack means to mechanically move the detonators to align and misalign them with the pickups, and therefore the detonators are always aligned with the pickups. Consequently, errors in the electronics could lead to inadvertent firing. On the other hand, the prior art electromechanical devices utilize sliding electrical contacts that move past each other. Over time, physical degradation of the contacts (caused for example by polymerization through exposure to vaporous low weight molecular organic compounds) can impair performance of the contacts in testing and/or use.
The salient features of a hybrid electronic and electromechanical arm-fire device according to the present invention are a moving mechanical element having a safe position and an armed position, one or more pyrotechnic detonators each mounted on the moving mechanical element and having an output, a pickup adjacent to the detonator output(s) that is in alignment therewith when the moving mechanical element is in the armed position but is not so aligned when the moving mechanical element is in the safe position, and electronic circuitry including a logic core having an electronic switch. In a separate and independent aspect of the invention, the electronic circuitry may also include an electronic sensor such as a photointerruptor.
Electromechanical
Referring to
To effect arming, the AFD utilizes a torque rotary motor 130 including a magnet 126 and a shaft 138, with a spring biased against the motor to return it to a safe position when the motor is not energized. The motor, a circuit board 122 (attached to the motor with bolts 176, and including various circuitry), and an insert-molded detonator assembly 136 are contained within a main housing 132, to which the motor is bolted with bolts 124 through bolt eyes 166, and which is closed by a housing closure 120 (both metallic). Exposed at the top of the molded detonator assembly 136 are two detonator outputs 160.
A pickup housing 154 (capped by a pickup housing cap 156) is welded to the main housing 132, and includes donor charges 142 (made of, e.g., CH6 pellets) pressed in corresponding cavities in the pickup housing 154 and covered by a mylar disc 140, receptor charges 146 (made of, e.g., CH6 pellets) pressed in corresponding cavities in the pickup housing 154, a pickup charge 148 (made of, e.g., BKNO3), and pyrotechnic pellets 150 (made of, e.g., BKNO3) pressed in corresponding cavities in the pickup housing 154. The pickup housing also includes a pickup output cavity 156, and axial shockwave transmission gaps 144. See generally assignee's U.S. Pat. No. 4,592,281, the disclosure of a pickup assembly of which is incorporated herein by reference.
As shown specifically in
Electronic
a) Power to Logic Core
Power to the logic core can be obtained directly from the ARM signal (as shown in the AFD circuitry 54 in
b) ARM Sensor Circuitry
The ARM sensor circuitry may include two slotted photointerruptors cooperatively interacting with the fins 162. ARM power activates the motor, causing the fins 162 to obstruct the photointerruptors' slots; without ARM power, a spring biases the device to the safe position, in which the fins do not obstruct the photointerruptors' slots. By appropriate biasing of the photointerruptor circuits 56 and 58 (see
c) Safe-Arm Indicator Circuitry
The safe-arm indicator circuitry, by default, may be a conductive short (e.g., <0.5 ohm) across the SAFE electrical terminals or a more elaborate indicator such as the indicator circuit 62 shown in
d) Logic Core
The logic core is the main logic controller that determines the arming/safing of the AFD circuitries and dictates the final firing of the detonators via closing of the MOSFETs in series with the detonators and FIRE signal. The logic core can be constructed using discrete logic components 72 (
e) Firing Circuits
As shown in
Operation
The ARM signal simultaneously energizes the torque motor and powers the logic core. The AFD's electronics must detect the ARM signal and arming power before the firing MOSFETs in the firing circuits can be turned on. The firing circuits are only enabled after the logic core receives proper feedback from the photo-sensors monitoring rotor position. The ARM command connects only with a logic core, which passes only a small, current-limited signal (insufficient to fire a detonator) to the firing circuitry. This current-limited signal is isolated from the firing circuitry by an optoisolator. Electrical energy on the arming circuitry could not be coupled into the firing circuit without simultaneous unlikely failures. As can be seen in Table 2, the AFD will not fire even if it improperly “sticks” in the armed position, unless both an arm command and a fire command were applied:
Without ARM power, the firing circuit's MOSFETs are in the off state, so there is no complete path for any current to flow from FIRE signals to the detonators. The mechanical shunts across the detonators provide an auxiliary protection against FIRE signals when the device is not in a proper armed state. When ARM power is applied, the rotary torque motor removes the mechanical shunts on the detonators and simultaneously powers the logic core and causes the fins to obstruct the photointerruptors' slots. The photointerruptors in turn send an ARM signal to the firing circuits by turning on the optoisolators, which subsequently switch on the various firing MOSFETs.
Although the present invention has been described in detail in the context of a preferred embodiment of a hybrid electronic and electromechanical arm-fire device, one skilled in the art will appreciate that numerous variations, modifications, and other applications are also within the scope of the present invention. For example, the invention could be employed in a safe and arm or arm and fire device in grenades, mines, military detonators, torpedoes, aerial ordnances or naval weapons. Thus, the foregoing detailed description is not intended to limit the invention in any way, which is limited only by the following claims and their legal equivalents.
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