Abstract The blade has an aerofoil portion (16) having a first (23), a second (24), a third (25) and a fourth (26) internal spanwise passage for cooling air arranged in chordwise succession with the first passage being at the leading edge wall (17) of the blade. The first and third passages are connected to respective a cooling air supplies (14A,14B) at the root end (11) of the blade. At the tip (28) of the blade the third passage is connected to the second passage to introduce air, warmed on passing through the third passage, into the second passage and ameliorate undue cooling of the internal walls (19,20) between the first, second and third passages. The third passage is also connected to the fourth passage for supply of cooling air to the trailing region of the blade. The second passage has outlets (24A) to the exterior of the blade whereby the flow through the second passage is controllable independently of the air supply to the fourth passage, i.e. to the trailing region of the blade.
An aerofoil turbine blade for gas turbine engines, comprising two opposite side walls, a leading edge wall, a trailing edge wall and first, second, third and fourth internal walls extending transversely between the side walls; a first spanwise passage defined between the leading edge wall and a first internal wall; a second, a third and a fourth passage defined in succession by said first internal wall and by said second, said third and said fourth internal walls and portions of said side walls; a first and third passages each having an inlet for a cooling air supply at one spanwise end of the blade, the third passage being interconnected with each of the second and fourth passages at the other spanwise end of the blade, and the first, second and fourth passages each having outlets to the exterior of the blade.
Claim 2
Dependent Claim
141 words
An aerofoil turbine blade for gas turbine engines, comprising two opposite side walls, a leading edge wall, a trailing edge wall and first, second, third and fourth internal walls extending transversely between the side walls; a first spanwise passage defined between the leading edge wall and a first internal wall; a second, a third and a fourth passage defined in succession by said first internal wall and by said second, said third and said fourth internal walls and portions of said side walls; a first and third passages each having an inlet for a cooling air supply at one spanwise end of the blade, the third passage being interconnected with each of the second and fourth passages at the other spanwise end of the blade, and the first, second and fourth passages each having outlets to the exterior of the blade.
Claim 3
Dependent Claim
48 words
A blade according to claim 1, wherein the second passage has an end adjacent said one end of the blade, said end of the second passage is closed and the outlets of the second passage are in the form of openings along the length of the second passage.