Fuel injector arrangement

A method of assembling a fuel injector arrangement for a gas turbine engine, the method comprising:

• providing a fuel spray nozzle comprising an engaging feature;
• and
• providing a burner sleeve comprising a swirler;
• wherein the burner sleeve comprises a connecting feature;
• wherein the method comprises bringing the engaging and connecting features into engagement so as to removably couple the fuel spray nozzle to the burner sleeve and inhibit relative movement between the fuel spray nozzle and the swirler.

Combustion equipment for a gas turbine engine, the combustion equipment comprising:

• a combustion chamber defined by a combustor liner having a combustor head, the combustor head having an aperture;
• a fuel spray nozzle comprising a fuel spray nozzle stem and a fuel spray nozzle head, the fuel spray nozzle head comprising an engaging feature;
• and
• a burner sleeve comprising a swirler;
• the burner sleeve being arranged in the aperture in the combustor head, wherein the burner sleeve comprises a connecting feature;
• wherein the engaging and connecting features are engageable so as to removably couple the fuel spray nozzle to the burner sleeve and inhibit relative movement between the fuel spray nozzle and the swirler.