Combustor of gas turbine

A combustor of a gas turbine comprising:

• wall means of double wall construction including an outer plate member and an inner plate member located at least in one part of the combustor;
• connector means including a multiplicity of connector pins formed of heat conductive material for connecting together the outer plate member and inner plate member of the wall means;
• and
• cooling air flow aperture means including a multiplicity of cooling air inlet apertures formed in the outer plate member to introduce cooling air therethrough from outside into a spaced defined between the outer and inner plate members perpendicularly to an outer surface of the inner plate, and a multiplicity of cooling air outlet apertures formed in the inner plate member to allow the cooling air to flow along an inner surface of the inner plate after being released into the interior of the combustor from the space between the outer and inner plate members, said cooling air outlet apertures formed in said inner plate member being inclined and said cooling air inlet apertures formed in said outer plate member being greater in diameter but smaller in total area than said cooling air outlet apertures.