Abstract: A system for ablating material in vein grafts includes an ablation burr that is rotated by a driveshaft. The ablation burr preferably includes one or more channels, blades or other mechanisms that direct ablated material and liquid proximally and/or outwardly against a vessel wall. Aspiration is used to remove ablated material and liquid from the treatment area. Finally, methods for treating vein grafts and original native arteries are disclosed.

Abstract: A method for treating loosely formed, friable or fragile lesions in a patient's blood vessel. A catheter having a pair of sealing mechanisms is advanced such that the sealing mechanisms are positioned distal to and proximal to the lesion. The sealing mechanisms are activated to seal the vessel on either side of the lesion. A medication is then delivered through the catheter to the sealed area of the vessel. The medication interacts with the lesion in order to partially or completely solidify it. Once the lesion is solidified, the catheter is removed and the lesion can be treated with a conventional intravascular device.

Abstract: Infusion liquid is expelled distally of an ablation burr for washing a blood vessel lesion being treated by the burr. The infusion liquid can be aspirated in a proximate direction to carry the infusion liquid and loose ablated particles of the lesion away from the treatment area. The infusion liquid can be supplied through one or more passages in the burr, In addition to distally extending passages, the burr can include transverse passages extending at least partly in a proximate direction, with the distally extending and proximately extending passages sized so that only a minor portion of the infusion liquid is expelled distally.

Abstract: Infusion liquid is expelled distally of an ablation burr for washing a blood vessel lesion being treated by the burr. The infusion liquid can be aspirated in a proximate direction to carry the infusion liquid and loose ablated particles of the lesion away from the treatment area. The infusion liquid can be supplied through one or more passages in the burr. In addition to distally extending passages, the burr can include transverse passages extending at least partly in a proximate direction, with the distally extending and proximately extending passages sized so that only a minor portion of the infusion liquid is expelled distally.

Abstract: A modular camera support and extension structure which removably mounts on the seat tracks of a conventional aircraft and extends through a cargo pod door during usage, including a box structure containing a plurality of vertical rails which support a tracking plate positioned inside the box structure with linear bearings around its periphery, slidably mounted on said rails for vertical movement from a retracted position to an extended position; a camera rotatably mounted on the bottom of said tracking plate about a vertical axis; a pair of actuating sprockets connected by a drive chain mounted on the box structure, the drive chain is connected to the tracking plate for moving the FLIR camera from its retracted position to its extended position; a box frame structure mounted on the aircraft skin which includes stops on the box frame which lockingly engage the tracking plate in its extended position.

Abstract: A modular camera support and extension structure which removably mounts on the seat tracks of a conventional aircraft and extends through a cargo pod door during usage, including a box structure containing a plurality of vertical rails which support a tracking plate positioned inside the box structure with linear bearings around its periphery, slidably mounted on said rails for vertical movement from a retracted position to an extended position; a camera rotatably mounted on the bottom of said tracking plate about a vertical axis; a pair of actuating sprockets connected by a drive chain mounted on the box structure, the drive chain is connected to the tracking plate for moving the FLIR camera from its retracted position to its extended position; a box frame structure mounted on the aircraft skin which includes stop means on the box frame which lockingly engages the tracking plate in its extended position and a drive means which forces the tracking plate against the stop means.