COMBUSTION CHAMBER
Assignee
UNITED TECHNOLOGIES CORPORATION, A CORP. OF DE
Filed
Jun 12, 1992
Granted
Apr 18, 1995
Location
MANCHESTER CT US
Abstract
A combustion chamber 42 for an axial flow rotary machine 10 is disclosed. Various construction details are developed for controlling the production of emissions such as carbon monoxide, unburnt hydrocarbons and oxides of nitrogen. In one embodiment, the combustion chamber has a pilot zone 108 which extends axially and a main zone 106 axially adjacent to the pilot zone which has a divergent outer wall having a divergent end region 178 through which locally swirling gases are injected into swirling gases from the pilot zone 108.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Feb 17, 1993
Rescinded
May 13, 1993
Duration
2 months
Inventor
- 1RICHARD L. MARSHALL
Record Details
- Patent number
- US 5406799
- Application
- 07898053
- Aerospace match
- No
- Dataset source
- 35 USC §181 SO records
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