Torsional strain relief for borescope

• US 4,989,581 A
• Filed: 06/01/1990
• Issued: 02/05/1991
• Est. Priority Date: 06/01/1990
• Status: Expired due to Term

• Current Assignee: Everest Vit, Inc. (GE Aerospace)
• Original Assignee: Welch Allyn Incorporated
• Inventors: Knieriem, Alan S., Tamburrino, Richard A.
• Primary Examiner(s): Grieb, William H.
• Application Number:
  US07/531,557
• Time in Patent Office: 249 Days
• Field of Search: 128/4, 128/6, 358/98
• US Class Current: 600/103
• CPC Class Codes: A61B 1/0055 Constructional details of insertion parts, e.g. vertebral elements
• CPC Class Codes: G02B 23/2476 Non-optical details, e.g. housings, mountings, supports

Abstract

A torsional strain relief assembly is provided for absorbing torsional strain at the proximal end of an elongated flexible insertion tube of a borescope or endoscope. The insertion tube is torsionally stiff, i.e. is bendable but resists rotation or twisting about its axis. The strain relief has a tubular rigid sleeve that is attached at its proximal end to a frame or housing, and contains a helical torsion spring whose proximal end is rotationally affixed to the frame. A bushing is rotatably disposed within the distal end of the sleeve and joins the distal end of the spring to the proximal end of the insertion tube. A layer of low friction material such as PTFE can be interposed between the bushing and the inner surface of the rigid sleeve. Rotation of the insertion tube due to bending and twisting is taken up by the spring, and the spring returns the insertion tube to the original position when the twisting forces are relieved. The oeprator can track the orientation of the optical or video imager in the head of the insertion tube by viewing a reference mark or index at the proximal end of the insertion tube.

Claims

1. Torsional strain relief assembly for absorbing torsional strain at a proximal end of an elongated, flexible insertion tube of a borescope or endoscope and for mechanically coupling the insertion tube to a frame, said strain relief assembly comprising a tubular rigid sleeve;

means rigidly affixing a proximal end of the tubular rigid sleeve to said frame;

a helical torsional spring situated within said tubular rigid sleeve;

means rotationally affixing a proximal end of said spring to said frame;

a bushing rotationally affixed to a distal end of said spring and to a proximal end of said insertion tube and rotatably mounted within said rigid tubular sleeve, permitting rotation of said insertion tube over at least a substantial rotational angle with respect to said rigid sleeve and said frame;

such that said insertion tube is free to rotate over said substantial angle without significant twisting over the length of the insertion tube.

2. Torsional strain relief assembly according to claim 1, wherein said insertion tube has a torsionally stiff tubular sheath that is substantially constrained from twisting about its own axis.

3. Torsional strain relief assembly according to claim 1 wherein said insertion tube bears an index mark on its outer surface at least at its proximal end to indicate orientation of its distal end.

4. Torsional strain relief assembly according to claim 1 wherein said helical spring comprises at least three turns.

5. Torsional strain relief assembly according to claim 1 wherein said helical spring has a worm of rectangular cross section.

6. Torsional strain relief assembly according to claim 1 further comprising an elastomeric sleeve disposed on a radial outer surface of said spring.

7. Torsional strain relief assembly according to claim 1, further comprising stop means disposed in the distal end of said tubular rigid sleeve and cooperating means in said bushing to block mutual rotation of about one-half rotation either direction from a central rest position.