Turbine engine combustion assembly with a variable air supply
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
Aug 21, 2018
Grant Date -
Sep 3, 2015
app pub date -
Sep 17, 2013
filing date -
Oct 1, 2012
priority date (Note) -
In Force
status (Latency Note)
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Abstract
A turbine engine combustion assembly including a casing, a combustion chamber, and at least one fuel injector. The combustion chamber includes an internal wall and an external wall extending one inside the other and connected by an annular chamber base wall. The external wall of the chamber is secured to an annular external wall of the casing. The injector is attached to the annular external wall of the casing and includes a fuel ignition enclosure extending inside the casing successively through openings in the casing wall and in the external wall before opening into the chamber. At least one wall of the ignition enclosure extending between the casing wall and the combustion chamber wall includes at least one air intake port. The external wall of the combustion chamber is solidly connected to a device for plugging the air intake port according to a thermal expansion state of the combustion chamber.
First Claim
all claims..Other Claims data not available
Family
Country | kind | publication No. | Filing Date | Type | Sub-Type |
---|---|---|---|---|---|
FR | B1 | FR2996285 | Oct 01, 2012 | Patent | Grant |
Type : Patent Sub-Type : Grant | |||||
PATENT OF INVENTION (SECOND PUBLICATION) | ENSEMBLE DE COMBUSTION DE TURBOMACHINE A VARIATION D'ALIMENTATION D'AIR. | Sep 12, 2014 | |||
EP | B1 | EP2904324 | Sep 17, 2013 | Patent | Grant |
Type : Patent Sub-Type : Grant | |||||
Patent | ENSEMBLE DE COMBUSTION DE TURBOMACHINE A VARIATION D'ALIMENTATION D'AIR | Feb 20, 2019 | |||
CA | C | CA2886298 | Sep 17, 2013 | Patent | Grant |
Type : Patent Sub-Type : Grant | |||||
PATENT (SECOND LEVEL) | ENSEMBLE DE COMBUSTION DE TURBOMACHINE A VARIATION D'ALIMENTATION D'AIR | Apr 21, 2020 | |||
KR | B1 | KR102093954 | Sep 17, 2013 | Patent | Grant |
Type : Patent Sub-Type : Grant | |||||
PATENT SPECIFICATION | 공기 공급량 조절이 가능한 터빈 엔진 연소 어셈블리 | Mar 26, 2020 | |||
WO | A1 | WO2014053724 | Sep 17, 2013 | Patent | Application |
Type : Patent Sub-Type : Application | |||||
INTERNATIONAL APPLICATION PUBLISHED WITH INTERNATIONAL SEARCH REPORT | ENSEMBLE DE COMBUSTION DE TURBOMACHINE A VARIATION D'ALIMENTATION D'AIR | Apr 10, 2014 | |||
RU | C2 | RU2632353 | Sep 17, 2013 | Patent | Grant |
Type : Patent Sub-Type : Grant | |||||
PATENT FOR INVENTION ( 2ND PUBL.) | БЛОК КАМЕРЫ СГОРАНИЯ ГАЗОТУРБИННОГО ДВИГАТЕЛЯ С ПЕРЕМЕННОЙ ПОДАЧЕЙ ВОЗДУХА | Oct 04, 2017 | |||
CN | B | CN104718413 | Sep 17, 2013 | Patent | Grant |
Type : Patent Sub-Type : Grant | |||||
GRANTED PATENT FOR INVENTION | Have can changing air supply turbine engine fuel assembly | Jun 15, 2016 | |||
JP | B2 | JP6228607 | Sep 17, 2013 | Patent | Grant |
Type : Patent Sub-Type : Grant | |||||
PUBLISHED GRANTED PATENT (SECOND LEVEL) | 可変空気供給源を備えたタービンエンジン燃焼組立体 | Nov 08, 2017 | |||
IN | A | IN2015DN03280 | Apr 17, 2015 | Patent | Grant |
Type : Patent Sub-Type : Grant | |||||
PATENT OR PATENT OF ADDITION | TURBINE ENGINE COMBUSTION ASSEMBLY WITH A VARIABLE AIR SUPPLY | Oct 09, 2015 |
- 15 United States
- 10 France
- 8 Japan
- 7 China
- 5 Korea
- 2 Other
Patent Owner(s)
Patent Owner | Address | |
---|---|---|
SAFRAN HELICOPTER ENGINES | 64510 BORDES |
International Classification(s)

- 2013 Application Filing Year
- F02C Class
- 960 Applications Filed
- 829 Patents Issued To-Date
- 86.36 % Issued To-Date
Inventor(s)
Inventor Name | Address | # of filed Patents | Total Citations |
---|---|---|---|
Carrere, Bernard Joseph Jean Pierre | Pau, FR | 4 | 8 |
# of filed Patents : 4 Total Citations : 8 |
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- 0 Citation Count
- F02C Class
- 0 % this patent is cited more than
- 7 Age
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Maintenance Fees
Fee | Large entity fee | small entity fee | micro entity fee | due date |
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7.5 Year Payment | $3600.00 | $1800.00 | $900.00 | Feb 21, 2026 |
11.5 Year Payment | $7400.00 | $3700.00 | $1850.00 | Feb 21, 2030 |
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