Turbomachine combustion chamber
View Patent ↗A turbomachine combustion chamber in which a chamber end wall presents an opening for receiving a pre-vaporization bowl, and including a device for injecting air and fuel mounted on the axis thereof, the bowl being floatingly mounted relative to the chamber end wall to move in a predetermined radial direction and flaring downstream so as to form a collar, a deflector forming a thermal shield being made integrally with the bowl beside the chamber end wall so that the floating movement of the bowl-and-deflector assembly takes place in a sliding plane situated between the deflector and the chamber end wall.
1. A turbomachine combustion chamber comprising: at an upstream end relative to a gas flow direction, a chamber end wall presenting an opening;
a pre-vaporization bowl received in said opening, the pre-vaporization bowl which has an axis and a generally annular shape being floatingly mounted relative to the chamber end wall to move in a predetermined radial direction and being flared downstream so as to form a collar, the collar having a periphery;
an air and fuel injector device mounted on the axis of said pre-vaporization bowl; a deflector forming a heat shield being situated around the collar of the bowl on a downstream side of the chamber end wall; and
guiding means for guiding movement of the bowl in translation along the predetermined radial direction,
wherein the bowl and the deflector are made as a single piece, and the floating movement of the bowl-and-deflector assembly takes place in a sliding plane situated between the deflector and the chamber end wall,
wherein the guiding means comprises a threaded portion provided around the bowl to receive a retaining nut bearing against the chamber end wall, the nut being screwed so as to leave the bowl-and-deflector assembly free to float in translation in the predetermined radial direction.
2. A combustion chamber according to claim 1 , wherein the bowl-and-deflector assembly is made of a ceramic matrix composite material.
3. A combustion chamber according to claim 1 , wherein the deflector presents a substantially plane general shape extending parallel to the chamber end wall and is separated by an empty annular space from at least one wall of the combustion chamber.
4. A combustion chamber according to claim 3 , wherein at least one cooling orifice is formed in the chamber end wall in register with the empty annular space between the deflector and the combustion chamber wall.
5. A combustion chamber according to claim 1 , further comprising means for preventing the nut from loosening.
6. A combustion chamber according to claim 5 , wherein the means for preventing the nut from loosening comprises a plurality of through holes formed radially through the nut and configured to coincide with orifices formed radially through the threaded portion, the through holes and the orifices being configured, on coinciding, to receive a blocking pin.
7. A combustion chamber according to claim 1 , further comprising anti-rotation means of complementary shapes for preventing rotation between the chamber end wall and the bowl-and-deflector assembly.
8. A turbomachine, comprising a combustion chamber according to claim 1 .
9. A combustion chamber according to claim 1 , wherein said guiding means is fixed to the bowl-and-deflector assembly so as to leave said bowl-and-deflector assembly free to float in translation in the predetermined radial direction, and wherein an inner peripheral zone of the chamber end wall is interposed between said fixed guiding means and a portion of a peripheral zone of the deflector.
10. A turbomachine combustion chamber comprising:
at an upstream end relative to a gas flow direction, a chamber end wall presenting an opening;
a pre-vaporization bowl received in said opening, the pre-vaporization bowl which has an axis and generally annular shape being floatingly mounted relative to the chamber end wall to move in a predetermined radial direction and being flared downstream so as to form a collar, the collar having a periphery;
an air and fuel injector device mounted on the axis of said pre-vaporization bowl;
a deflector forming a heat shield being situated around the collar of the bowl on a downstream side of the chamber end wall; and
guiding means for guiding movement of the bowl in translation along the predetermined radial direction,
wherein the bowl and the deflector are made as a single piece, and the floating movement of the bowl-and-deflector assembly takes place in a sliding plane situated between the deflector and the chamber end wall, and
wherein the deflector presents a substantially plane general shape extending parallel to the chamber end wall and is separated by an empty annular space from at least one wall of the combustion chamber.
11. A combustion chamber according to claim 10 , wherein said guiding means comprises a threaded portion provided around the bowl to receive a retaining nut bearing against the chamber end wall, the nut being screwed so as to leave the bowl-and-deflector assembly free to float in translation in the predetermined radial direction and is fixed to the bowl-and-deflector assembly so as to leave said bowl-and-deflector assembly free to float in translation in the predetermined radial direction, wherein the deflector has a peripheral zone extending radially beyond the periphery of the collar,
wherein said guiding means comprises a portion of said peripheral zone of the deflector, and
wherein an inner peripheral zone of the chamber end wall is interposed between said fixed guiding means and said portion of the peripheral zone of the deflector.
12. A combustion chamber according to claim 10 , wherein the guiding means comprises a threaded portion provided around the bowl to receive a retaining nut bearing against the chamber end wall, the nut being screwed so as to leave the bowl-and-deflector assembly free to float in translation in the predetermined radial direction.