CONSTANT-VOLUME COMBUSTION SYSTEM FOR A TURBINE ENGINE OF AN AIRCRAFT ENGINE
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
N/A
Issued Date -
Feb 8, 2018
app pub date -
Feb 15, 2016
filing date -
Feb 17, 2015
priority date (Note) -
Published
status (Latency Note)
Importance
Abstract
A constant-volume combustion system is for a turbine engine. The system includes a plurality of combustion chambers regularly distributed around a longitudinal axis; a toroidal manifold including a radially oriented outlet for supplying compressed air, from a compressor, to each combustion chamber; a toroidal exhaust pipe including a radially oriented inlet for collecting the combustion gases from the combustion chambers, the combustion chambers being radially positioned between the outlet of the manifold and the inlet of the exhaust pipe; and a timing device for each chamber for drawing in compressed air from the outlet of the manifold and ejecting combustion gas towards the exhaust pipe.
First Claim
Family
International Classification(s)
- [Classification Symbol]
- [Patents Count]
Cited Art Landscape
Patent Citation Ranking
Recipient Email Address
Recipient Email Address
Comment
Recipient Email Address
Add to Portfolio(s)
To add this patent to one, or more, of your portfolios, simply click the add button.
This Patent is in these Portfolios:
Add to additional portfolios:
Last Refreshed On:
Changes done successfully