IP Library › Granted Patent US 8,499,779
Granted Patent B2
US 8,499,779 · App. 12/014,889 · Granted Aug 6, 2013

Systems, methods and apparatus of a nitinol valve

Inventor: Rebecca A. Gillespie (Pittsburgh, PA)
Assignee: The United States of America as represented by the Administrator of the National Aeronautics Space Administration
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 8,499,779
App. No.
12/014,889
Granted
Aug 6, 2013
Kind
B2
Abstract

Systems, methods and apparatus are provided through which in some embodiments a non-pyrotechnic valve includes an inlet piece, an actuator comprising a shape-memory metal, and an outlet attached to the inlet piece. In some examples, the shape-memory metal includes Nitinol.

Claims (10)

1. A method to fabricate a valve, the method comprising:

sliding an actuator over a first portion of a metallic inlet piece, the first portion of the metallic inlet piece having an outer proportion that is about equal to an inner proportion of an inside of the actuator, the longitudinal length of the actuator being less than the longitudinal length of the first portion of the metallic inlet piece to the extent that an end of the first portion of the metallic inlet piece extends beyond the actuator, the actuator comprising a shape-memory metal; and

attaching a flow passage piece to the end of the first portion of the metallic inlet piece.

2. The method of claim 1 , wherein the attaching further comprises orbital welding.

3. The method of claim 1 , wherein the shape-memory metal further comprises a nickel-titanium alloy.

4. The method of claim 3 , further comprising:

attaching at least one filler to the metallic inlet piece in a space proximally between an end of the actuator, and the attaching being performed to a portion of the flow passage piece that is wider than the outer proportion of the metallic inlet piece.

5. The method of claim 4 , wherein the at least one filler further comprises two Titanium filler halves, wherein the flow passage piece further comprises a metallic flow passage piece and wherein the attaching of the two Titanium filler halves to the metallic inlet piece and the metallic flow passage piece further comprises welding the two Titanium filler halves to the metallic inlet piece and welding the two Titanium filler halves to the metallic flow passage piece.

6. The method of claim 2 , further comprising:

mounting an outlet piece over a second portion of the metallic inlet piece that has a longitudinal length that is greater than the longitudinal length of the first portion of the metallic inlet piece.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 17, 2008
From: GILLESPIE, REBECCA A., MS.
To: UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
Reel/Frame 020377/0055 →
Continuity (1)
Related Publication 20130167377A1 · Jul 4, 2013