PAROI POUR CHAMBRE DE COMBUSTION DE TURBOMACHINE COMPRENANT UN AGENCEMENT OPTIMISE D'ORIFICES D'ENTREE D'AIR

A rotationally symmetrical wall for an aircraft turbomachine combustion chamber, including primary holes, dilution holes positioned downstream from the primary holes, and a plug installation aperture upstream from the primary holes, wherein each first primary hole, considered as one moves away circu...

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Hauptverfasser: COMMARET PATRICE, ANDRE, BUNEL JACQUES, MARCEL, ARTHUR, HERNANDEZ DIDIER, HIPPOLYTE
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creator COMMARET PATRICE, ANDRE
BUNEL JACQUES, MARCEL, ARTHUR
HERNANDEZ DIDIER, HIPPOLYTE
description A rotationally symmetrical wall for an aircraft turbomachine combustion chamber, including primary holes, dilution holes positioned downstream from the primary holes, and a plug installation aperture upstream from the primary holes, wherein each first primary hole, considered as one moves away circumferentially from the median axial plane (D) in either direction is positioned at a circumferential position between the circumferential positions of the first dilution hole and of the second dilution hole considered as one moves away circumferentially from the median axial plane (D), wherein the other primary holes are distributed equidistantly, at a predefined interval P, and the distance between the two primary holes is greater than the interval P separating two of the other adjacent primary holes.
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subjects BLASTING
CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION
COMBUSTION APPARATUS
COMBUSTION PROCESSES
GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS
GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
HEATING
LIGHTING
MECHANICAL ENGINEERING
TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE
WEAPONS
title PAROI POUR CHAMBRE DE COMBUSTION DE TURBOMACHINE COMPRENANT UN AGENCEMENT OPTIMISE D'ORIFICES D'ENTREE D'AIR
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