Multiple payload expendable device
This disclosure relates generally to a Multiple Payload Expendable Device consisting of a set of cylindrical multiple payload casings, each payload casing exhibiting circular symmetry fluid passages in relation to firing squibs and voltage coded squib actuating circuit that converts existing single payload expendable device systems to multiple payload expendable device systems.
1. A chaff deployment device for deploying chaff from an airborne vehicle, comprising:
an assembly of multiple chaff deployment cylindrical payload cartridges, said payload cartridges for receiving and containing chaff for inducing radiofrequency interference upon being deployed by said chaff deployment device;
a plurality of firing squibs for generating a mechanical force for forcing said chaff from said chaff deployment cylindrical payload cartridges;
a firing circuit for firing said firing squibs for inducing the generation of said mechanical force;
a plurality of fluid passages associated with said payload cartridges for transmitting said mechanical force to said chaff, said plurality fluid passages in fluid communication with said firing squibs, said plurality of fluid passages formed in circular symmetry with respect to the longitudinal axis of said multiple chaff deployment cylindrical payload cartridges, said circular symmetry providing for said plurality of firing squibs to be first mounted within said assembly of multiple chaff deployment cylindrical payload cartridges irrespective of the installation orientation of said plurality of firing squibs; and
wherein said firing circuit applies a first low voltage electrical signal to a first one of said firing squibs for deploying chaff from one of said multiple chaff deployment payload cartridges and said firing circuit apples a second higher voltage electrical signal to a second one of said plurality of firing squibs for deploying chaff from a second one of said multiple chaff deployment payload cartridges.
2. The chaff deployment device of claim 1 , wherein said first low voltage electrical signal and said second low voltage electrical signal are of arbitrary polarity both independently and to one another.
3. The chaff deployment device of claim 1 , wherein said first low voltage electrical signal and said second low voltage electrical signal provide controllable inputs for firing said firing squibs at controllably different times.
4. The chaff deployment device of claim 1 , wherein firing circuit for generating said first low voltage electrical signal and said second low voltage electrical signal provide an open circuit condition of at least 500 ohms following generation and transmission of said first low voltage electrical signal or said second low voltage electrical signal.
5. The chaff deployment device of claim 1 , wherein said firing circuit is voltage polarity insensitive for eliminating errors upon installing said firing squibs to said assembly of multiple chaff deployment cylindrical payload cartridges.
6. The chaff deployment device of claim 1 , wherein chaff further comprises objects from the group consisting of electromagnetic radiation absorbing elements, electromagnetic radiation reflecting elements, physical objects for interfering with approaching missiles or other flying devices, glass objects capable of breaking and forming Neff surfaces upon contact with the ground or other objects, and other obstructive objects capable of interfering with attempts to hit or damage the flying vehicle deploying said objects.
7. The chaff deployment device of claim 1 , wherein said assembly of multiple chaff deployment cylindrical payload cartridges permits mechanical orientation of said squibs to said cylindrical payload cartridges to be insensitive to cylindrical orientation, thereby eliminating the need for mechanically orienting said squibs to said cylindrical payload cartridges during assembly.
8. The chaff deployment device of claim 1 , wherein said assembly of multiple chaff deployment cylindrical payload cartridges permits conversion of a prior existing single payload air expendable decoy device to use said assembly of multiple chaff deployment cylindrical payload cartridges within the existing hardware and software systems of a military vehicle.
9. A method for deploying chaff from an airborne vehicle using a chaff deployment device, comprising the steps of:
receiving and containing chaff for inducing radiofrequency interference upon being deployed by said chaff deployment device using an assembly of multiple chaff deployment cylindrical payload cartridges, said payload cartridges for;
generating a mechanical force for forcing said chaff from said chaff deployment cylindrical payload cartridges using a plurality of firing squibs;
inducing the generation of said mechanical force using a firing circuit for firing said firing squibs;
transmitting said mechanical force to said chaff a plurality of fluid passages associated with said payload cartridges, said plurality fluid passages in fluid communication with said firing squibs, said plurality of fluid passages formed in circular symmetry with respect to the longitudinal axis of said multiple chaff deployment cylindrical payload cartridges, said circular symmetry providing for said plurality of firing squibs to be first mounted within said assembly of multiple chaff deployment cylindrical payload cartridges irrespective of the installation orientation of said plurality of firing squibs; and
applying a first low voltage electrical signal to a first one of said firing squibs for deploying chaff from one of said multiple chaff deployment payload cartridges and said firing circuit apples a second higher voltage electrical signal to a second one of said plurality of firing squibs for deploying chaff from a second one of said multiple chaff deployment payload cartridges, using said firing circuit.
10. The method of claim 9 , further comprising the step of providing said first low voltage electrical signal and said second low voltage electrical signal at arbitrary polarity both independently and to one another.
11. The method of claim 9 , further comprising the step of providing said first low voltage electrical signal and said second low voltage electrical signal provide controllable inputs for firing said firing squibs at controllably different times.
12. The method of claim 9 , further comprising the step of generating said first low voltage electrical signal and said second low voltage electrical signal and then establishing in said firing circuit an open circuit condition of at least 500 ohms following generation and transmission of said first low voltage electrical signal or said second low voltage electrical signal.
13. The method of claim 9 , further comprising the step of using said firing circuit to provide a voltage polarity insensitive for eliminating errors upon installing said firing squibs to said assembly of multiple chaff deployment cylindrical payload cartridges.
14. The method of claim 9 , further comprising the step of providing chaff comprising objects from the group consisting of electromagnetic radiation absorbing elements, electromagnetic radiation reflecting elements, physical objects for interfering with approaching missiles or other flying devices, glass objects capable of breaking and forming Neff surfaces upon contact with the ground or other objects, and other obstructive objects capable of interfering with attempts to hit or damage the flying vehicle deploying said objects.
15. The method of claim 9 , further comprising the step of providing permits mechanical orientation of said squibs to said cylindrical payload cartridges so as to be insensitive to cylindrical orientation, thereby eliminating the need for mechanically orienting said squibs to said cylindrical payload cartridges during assembly.
16. The method of claim 9 , further comprising the step of providing said assembly of multiple chaff deployment cylindrical payload cartridges permits conversion of a prior existing single payload air expendable decoy device to use said assembly of multiple chaff deployment cylindrical payload cartridges within the existing hardware and software systems of a military vehicle.
17. An airborne military vehicle capable of deploying chaff using a chaff deployment device for deploying chaff from an airborne vehicle, comprising:
an airborne military vehicle for containing a chaff deployment device, said chaff providing multiple chaff deployment capability using a multiple chaff deployment device formed to fit with the physical, electrical, and instructional frame of a single chaff deployment device;
said chaff deployment device, further comprising:
an assembly of multiple chaff deployment cylindrical payload cartridges, said payload cartridges for receiving and containing chaff for inducing radiofrequency interference upon being deployed by said chaff deployment device;
a plurality of firing squibs for generating a mechanical force for forcing said chaff from said chaff deployment cylindrical payload cartridges;
a firing circuit for firing said firing squibs for inducing the generation of said mechanical force;
a plurality of fluid passages associated with said payload cartridges and in fluid communication with said firing squibs, said plurality of fluid passages formed in circular symmetry with respect to the longitudinal axis of said multiple chaff deployment cylindrical payload cartridges, said circular symmetry providing for said plurality of firing squibs to be first mounted within said assembly of multiple chaff deployment cylindrical payload cartridges irrespective of the installation orientation of said plurality of firing squibs; and
wherein said firing circuit applies a first low voltage electrical signal to a first one of said firing squibs for deploying chaff from one of said multiple chaff deployment payload cartridges and said firing circuit apples a second higher voltage electrical signal to a second one of said plurality of firing squibs for deploying chaff from a second one of said multiple chaff deployment payload cartridges.
18. The airborne military vehicle of claim 17 , wherein said first low voltage electrical signal and said second low voltage electrical signal are of arbitrary polarity both independently and to one another.
19. The airborne military vehicle of claim 17 , wherein said first low voltage electrical signal and said second low voltage electrical signal provide controllable inputs for firing said firing squibs at controllably different times.
20. The airborne military vehicle of claim 17 , wherein chaff further comprises objects from the group consisting of electromagnetic radiation absorbing elements, electromagnetic radiation reflecting elements, physical objects for interfering with approaching missiles or other flying devices, glass objects capable of breaking and forming Neff surfaces upon contact with the ground or other objects, and other obstructive objects capable of interfering with attempts to hit or damage the flying vehicle deploying said objects.