Apparatus for use in a fuel delivery system for a gas turbine engine
This patent describes a fuel delivery system for a gas turbine engine, apparatus secured to a structure which surrounds a combustion chamber, the apparatus comprising: a body having a first surface adapted to interface with a nozzle assembly and a second surface adapted to interface with the structure; the body having channels formed between the surfaces; the body further having a hole extending from the first surface to the second surface for receiving a fuel nozzle; the channels including a primary supply channel, a secondary supply channel and a drain channel extending through the body in directions sufficiently parallel to the first and second surfaces to avoid intersection therewith; the channels further including feed channels extending from the supply channels to the first surface; the body being adapted via the supply and drain channels to receive six conduits and, via the feed channels to provide fluid communication between the supply channels and the nozzle assembly; the body further being adapted for securement of the nozzle assembly thereto.
- Assignee:
- Allied-Signal Inc., Morris Township, Morris County, NJ (USA)
- Application Number:
- PPN: US 7-362182
- OSTI ID:
- 5661853
- Resource Relation:
- Patent File Date: 6 Jun 1989
- Country of Publication:
- United States
- Language:
- English
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