IP Library Granted Patent US 8,558,878
Granted Patent B2
US 8,558,878 · App. 12/235,148 · Granted Oct 15, 2013

Steerable structure of catheter or endoscope type

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Quick Facts
Patent No.
US 8,558,878
App. No.
12/235,148
Granted
Oct 15, 2013
Kind
B2
Abstract

A steerable structure of the catheter or endoscope type is disclosed. The structure includes an elastically or deformable longitudinal body including at least one actuator of material of the shape memory type incorporated longitudinally with the body together with a Joule-effect heater enabling the actuator to be contracted longitudinally in order to cause the longitudinal body to bend. The actuator extends over at least one portion of the body that presents varying stiffness.

Claims (22)

1. A steerable structure of catheter or endoscope type for observing or treating a masked object, the structure comprising:

an elastically deformable longitudinal body having at least one actuator of shape memory type material incorporated longitudinally in the longitudinal body together with Joule-effect heater means enabling the actuator to be contracted longitudinally so as to cause the longitudinal body to bend,

wherein the actuator extends over at least one portion of the longitudinal body of a varying stiffness comprising at least one extra thickness of material, said portion of the longitudinal body being formed with at least one extra thickness varying the thickness of the body over said portion and said varying stiffness resulting from said extra thickness.

2. The structure according to claim 1 , wherein the varying stiffness of the longitudinal body is designed so that contraction of the actuator modifies and/or inverts the longitudinal or transverse curvature of the longitudinal body.

3. The structure according to claim 1 , wherein the longitudinal body comprises at least one tube.

4. The structure according to claim 3 , wherein the actuator extends longitudinally over an inside wall or an outside wall of the tube.

5. The structure according to claim 3 , wherein the tube has a diameter of the order of 2 mm to 6 mm.

6. The structure according to claim 1 , wherein the longitudinal body comprises a blade of elongate cross-section.

7. The structure according to claim 6 , wherein two parallel actuators are incorporated in the blade and extend along a longitudinal face of the blade.

8. The structure according to claim 6 , wherein the blade has a thickness ranging between 1 mm to 2 mm, a width of 1 cm, and a length ranging between 5 to 10 cm.

9. The structure according to claim 1 , wherein the actuator is a wire.

10. The structure according to claim 9 , wherein the diameter of the wire ranges between 0.1 mm to 0.5 mm.

11. The structure according to claim 1 , wherein the portion of varying stiffness and the extra thickness of material are made of polymer.

12. The structure according to claim 1 , wherein the actuator is made of an alloy of titanium and nickel.

13. The structure according to claim 1 , wherein the structure is of the telescopic type consisting in a plurality of elastically individual deformable bodies that are provided with actuators and that are engaged one in another.

14. The structure according to claim 13 , wherein the distal end is linked to a head provided with non-destructive inspection means via resilient means adapted to exert a longitudinal thrust on the head when the head is brought into contact with a surface.

15. The structure according to claim 14 , wherein the resilient means are helical springs.

16. The structure according to claim 15 , wherein the springs are made of shape memory type material and are connected to Joule-effect heater means.

17. The structure according to claim 14 , wherein the non-destructive inspection means are Foucault current probes or ultrasound probes.

18. The structure according to claim 13 , wherein one of the transverse dimensions of the structure varies from 8 mm at the proximal end to 1 mm at the distal end.

19. The structure according to claim 1 , wherein the structure comprises means for hanging on or bearing against surrounding stationary elements.

20. The structure according to claim 1 , wherein the heater means are connected to automatic control means.

Assignments (2)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →