Planar-shaped thermal balloon for mesenteric fat reduction
A surgical device for reducing visceral fat in the abdominal cavity comprises an elongate shaft and an inflatable member. The inflatable member comprises a small-profile deflated configuration for being advanced into the abdominal cavity and a large-profile inflated configuration comprising a planar distal treatment surface for treating the visceral fat. The thermal fluid, preferably a gas, is circulated through the inflatable member at a temperature range sufficient to cause cryolipolysis to the fat cells but not damage non-target tissues. The inflatable member can have several chambers, reinforcing members, and ports to provide controlled flow patterns that maintain the shape of the inflatable member when inflated.
1. A system for cooling tissue comprising:
a first surgical device comprising:
an elongate shaft;
an inflatable member, the inflatable member comprising a small-profile deflated configuration for being advanced into the abdominal cavity of the patient, and a large-profile inflated configuration comprising a planar distal treatment surface for treating the visceral fat;
a fluid inlet line to transport a thermal fluid to the inflatable member;
a fluid return line to transport the thermal fluid from the inflatable member; and
wherein the thermal fluid is circulated through the inflatable member by the inlet line and outlet line;
a temperature sensor arranged to measure temperature of the thermal fluid entering (or within) the inflatable member (Ti); and
a pressure control device to control the pressure of the thermal fluid transported to the inflatable member (Pi); and
a second surgical device comprising:
an elongate shaft;
an inflatable member, the inflatable member comprising a small-profile deflated configuration for being advanced into the abdominal cavity of the patient, and a large-profile inflated configuration comprising a planar distal treatment surface for treating the visceral fat;
a fluid inlet line to transport a thermal fluid to the inflatable member;
a fluid return line to transport the thermal fluid from the inflatable member; and
wherein the thermal fluid is circulated through the inflatable member by the inlet line and outlet line;
a temperature sensor arranged to measure temperature of the thermal fluid entering (or within) the inflatable member (Ti); and
a pressure control device to control the pressure of the thermal fluid transported to the inflatable member (Pi); and
wherein the distal treatment surface of each of the first surgical device and the second surgical device is provided with a positioning sensor;
a controller operable to:
determine thickness of the visceral fat based on signals from the positioning sensors;
compute a desired temperature and duration for applying cooling to the visceral fat based on the determine step; and
maintain, for each of the first surgical device and the second surgical device, the measured temperature (Ti) at the desired temperature by adjusting the Pi using the pressure control device for the duration.
2. The system as recited in claim 1 , wherein each said pressure control device is a regulator.
3. The system as recited in claim 1 , wherein the controller is operable to compute total energy removed to the visceral fat.
4. The system of claim 1 , wherein each said inflatable member comprises a treatment chamber separated from a supporting chamber by a divider, the divider comprises at least one opening for fluidly connecting the treatment chamber to the supporting chamber, and wherein the inlet line provides the thermal fluid to the treatment chamber via an inlet port and the outlet line transports the thermal fluid from the supporting chamber via an outlet port.
5. The system of claim 4 , wherein the inlet port is centrally located for each of the first and second surgical devices; and wherein the at least one opening comprises a plurality of openings.
6. The system of claim 5 , wherein the openings are arranged around the periphery of the divider.
7. The system of claim 4 , wherein the supporting chamber and the front chamber have a substantially equal volume.
8. The system of claim 5 , wherein, for each of the first and second surgical devices, the inlet port, outlet port, and plurality of openings are operable to create a first flow pattern in the treatment chamber and a second flow pattern in the support chamber, wherein the second flow pattern flows in an opposite direction to the first flow pattern.
9. The system of claim 8 , wherein the first flow pattern radiates from the centrally located inlet port; and wherein the second flow pattern converges from the circumference of the support chamber to the centrally located outlet port, serving to maintain flatness of the planar treatment surface and to direct the thermal fluid evenly therethrough such that the planar distal treatment surface has a substantially uniform temperature and remains planar even when applied against the visceral fat.
10. The system of claim 1 , wherein the positioning sensors are operable to transmit and receive signal from corresponding transmitters/sensors on the opposing distal treatment surface.
11. The system of claim 1 , wherein the controller maintains Ti for each of the first and second surgical device between −35° C. and −40° C.
12. The system of claim 1 , wherein each of the first and second surgical devices further comprises a plurality of reinforcing members to maintain the treatment surface in a fixed relation to the rear surface when the inflatable member is inflated.
13. The system of claim 12 , wherein each of the reinforcing members of each of the first and second surgical devices are closed cells extending from the rear surface to the treatment surface; wherein the reinforcing members are cylindrically-shaped.
14. The system of claim 12 , wherein each of the reinforcing members form a dimple at the treatment surface.
15. The system of claim 1 , wherein each said inflatable member has a square profile in the inflated configuration; and has a thickness between 5-10 mm when inflated.
16. The system of claim 1 , wherein each said first and second surgical device further comprises at least one sensor to monitor a property of the thermal fluid in the return line.
17. The system of claim 1 , wherein the thermal fluid is CO2.