Claims
- 1. A regulator assembly for rendering a high pressure gas source compatible with a lower pressure use point comprising:
- (A) a regulator body having a receiving conduit;
- (B) a regulator within said regulator body in flow communication with said receiving conduit, said regulator comprising a spring-loaded piston, a sensing chamber at one end of the piston, and a sealing plug at the other end of the piston, said sealing plug capable of stopping gas flow from the receiving conduit;
- (C) a lower pressure outlet in flow communication with said receiving conduit downstream of said regulator and a first passage means within the piston, said first passage means capable of permitting gas flow between the receiving conduit, the lower pressure outlet and the sensing chamber;
- (D) second passage means communicating between the spring area and the outside of the regulator body; and
- (E) a lower pressure burst disc assembly communicating between the lower pressure outlet and the outside of the regulator body.
- 2. The assembly of claim 1 wherein the spring area is isolated on either side by O-ring seals concentric with the piston.
Parent Case Info
This application is a division of prior U.S. application Ser. No. 098,997, filed Sept. 21, 1987, now U.S. Pat. No. 4,844,111 issued July 4, 1989.
US Referenced Citations (12)
Non-Patent Literature Citations (2)
Entry |
Executive Mark II--Scott Aviation Products, Lancaster N.Y. 14086, May 1975. |
Stage 1 Adapter--Western Enterprises, Westlake Ohio 44145, 1986. |
Divisions (1)
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Number |
Date |
Country |
Parent |
98997 |
Sep 1987 |
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