초록 ▼

In an integrated gimbal and High-Powered Multiband Laser (HPMBL) for use in an infrared countermeasure apparatus in a pod mounted on an aircraft, the improvement comprises an optical bench that connects the optical path between side-by-side mounted gimbal and high power laser; and a kinematic mounti

In an integrated gimbal and High-Powered Multiband Laser (HPMBL) for use in an infrared countermeasure apparatus in a pod mounted on an aircraft, the improvement comprises an optical bench that connects the optical path between side-by-side mounted gimbal and high power laser; and a kinematic mounting system that prevents optical bench bending.

대표청구항 ▼

1. An integrated gimbal and laser for use in an infrared countermeasure apparatus in a pod mounted on an aircraft, wherein the improvement comprises an optical bench that connects the optical path between the gimbal and the laser, said optical bench including an internal light pipe within the optica

1. An integrated gimbal and laser for use in an infrared countermeasure apparatus in a pod mounted on an aircraft, wherein the improvement comprises an optical bench that connects the optical path between the gimbal and the laser, said optical bench including an internal light pipe within the optical bench, said laser and said gimbal being spaced apart on one surface of said optical bench and connected by said light pipe, said light pipe including an internal channel and a pair of reflectors and extending from the laser at said one surface of said optical bench, underneath said one surface, and exiting up through said one surface at said gimbal. 2. The apparatus of claim 1, wherein said pod is mounted on said aircraft using a kinematic mount, such that differences in the thermal co-efficient of expansion between the optical bench and the aircraft do not cause bending of the optical bench which would result in an optical misalignment between the gimbal and the laser. 3. The apparatus of claim 2, wherein the gimbal includes a directed infrared countermeasure head. 4. The apparatus of claim 2, wherein said kinematic mounting includes a three-point mount having two rigid mounting points for mounting said optical bench to said aircraft and a stiff but flexible mount spaced therefrom. 5. The apparatus of claim 4, wherein said stiff but flexible mount is more flexible than said optical bench, whereby flexure of said stiff but flexible mount does not cause flexing of said optical bench. 6. The apparatus of claim 5, wherein said stiff but flexible mount includes an element having an aperture therethrough, said optical bench including an aperture larger than said element, said element being mounted in said larger aperture, one end of said element being fixed to the bottom of said larger aperture, with an opposed end fixed to said aircraft, whereby thermal stressing causes said element to deform in said larger aperture to absorb any movement between said aircraft to said optical bench, such that said optical bench is not bent by any thermal stressing. 7. The apparatus of claim 6, wherein the aperture in said element is oval in shape. 8. The apparatus of claim 2, and further including locator pins and corresponding bushings attached respectively to said head and said optical bench and said laser and said optical bench to precisely locate said laser and said head on said optical bench and align the respective optical axes of said laser and said head to permit replacement without an alignment procedure. 9. A method for minimizing the intrusion of an infrared countermeasure system attached to the body of the aircraft and externally therefrom, comprising the steps of: side-by-side mounting a laser and a directed infrared countermeasure head on one surface of an optical bench; and,providing the optical bench with an internal light pipe defining an optical path between the laser and the head in the optical bench, the side by side mounting on a surface of the optical bench avoiding mounting the laser atop the head, whereby the laser and the head may be shrouded utilizing a conformal pod because of the side-by-side mounting, the optical bench being mounted to the aircraft airframe utilizing a kinematic mount to minimize bending of the optical bench and thus misalignment of the laser with the directed infrared countermeasure head during thermal stressing, the kinematic mounting system including rigid mounting points at one end of the optical bench and a stiff but flexible mounting point at the other end of the bench.