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时间:2011-03-27 16:55来源:蓝天飞行翻译 作者:航空
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 shroud to airfoil fillet radius
 (6) Missing or damaged hard coating on midspan  50 cycles
 shroud pressure faces more than 20 percent
 but less than 40 percent of coated area
 C. Fan disk
 (1) Wear greater than 50 percent of area on disk  100 cycles
 dovetail pressure faces
 D. Booster rotor blade for:

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(1) Piece missing:
 any number in area G, at leading edge and  50 cycles/75 hours
 trailing edge tip corners, 0.8 in. (20 mm)
 radial and 0.5 in. (12.5 mm) axial
 (2) Cracks and tears in area G, 0.8 in. (20 mm)  50 cycles/75 hours
 from tip : any number less than 0.8 in. (20
 mm) radial and less than 0.492 in. (12.5 mm)
 axial
 (3) Wear or local distortion of T/E and L/E tips  100 cycles/150
 if less than 15 blades 0.984 in. (25 mm)  hours
 radial and 0.59 in. (15 mm) axial
 (4) Nicks, dents, scratches for area E: any  50 cycles/75 hours
 number, less than 0.059 in. (1.5 mm) in
 diameter, protrusion acceptable, not thru
 (5) Nicks, dents, scratches for airfoil out of  50 cycles/75 hours
 area E, not L/E and T/E: any number, less
 than 0.236 in. (6 mm) in diameter, protrusion
 acceptable
 (6) Nicks, dents, scratches out of area E on L/E  50 cycles/75 hours
 and T/E: maximum axial length less than 0.059
 in. (1.49 mm)
 (7) Distorted L/E and T/E, out of area E maximum  50 cycles/75 hours
 circumference equals 0.275 in. (6.98 mm)
 radial length equals 0.708 in. (17.98 mm)
 E. Booster vanes (stage 1 only) for:
 (1) Piece missing:  50 cycles/75 hours
 maximum 20 blades more than 0.256 in. (6.5
 mm) axial, 0.728 in. (18.49 mm) radial, no
 cracks starting from damage area allowed in
 areas"A" and "B"
 (2) Cracks and tears in area C, any number, more  10 cycles/15 hours
 than 0.256 in. (6.5 mm) radial and 0.078 in.
 (1.98 mm) axial. In areas A and B, any number

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CONDITION  MAX EXTENSION
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more than 0.128 in. (3.25mm) radial and 0.039 in. (0.99 mm) axial
 (3) Distortion of T/E and L/E: any number, if the  50 cycles/75 hours length L is not more than 1 in. (25.4 mm) and the maximum dimension X along the chord width is not more than 0.492 in. (12.5 mm).

 (4) Nicks, dents, scratches for areas A and B ;  10 cycles/15 hours any number, less than 0.157 in. (3.99 mm) in diameter, protrusion permitted

 (5) Nicks, dents, scratches for area C: any  50 cycles/75 hours number, less than 0.295 in. (7.49 mm) in diameter, protrusion permitted

 (6) Nicks, dents, scratches L/E and T/E maximum  20 cycles/30 hours axial length less than 0.118 in. (2.99 mm) in diameter

 (7) Cracked inner shroud:  3000 hours/"C" Maximum of 4 cracks extending from the L/E to check the T/E of the inner shroud (passing through a recess) are permitted if there is a minimum separation of 3 non-cracked vane recesses between 2 cracked recesses.


 A sound check (see note below) done on the This extension may vanes at, and adjacent to the cracked inner be used again shroud area, must demonstrate no difference indefinitely in in tonality. intervals of 3000
 hours as long as there is no further deterioration of these conditions.
 NOTE : Sound Tonality Check Recommendation
____ A sound tonality check must be done to detect if the abradable material inside the inner shroud is still in contact with the root of the vane. Use a smooth-ended cylindrical tool made of steel with diameter of approximately 0.5 in. (12.6999 mm). (For example, a ratchet wrench extension bar). Tools made of aluminium, plastic or wood do not permit the detection of significant variation in the sound tone from one vane to the
 
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