PG632883.05_A_01_stamp.pdf
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- Wind Tunnel Compressor Rotor Blades Federal contract opportunity
- Solicitation number
- FA9101-17-R-1000
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A A
B B
C C
D D
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NOTES: (UNLESS OTHERWISE SPECIFIED)
1. DIMENSIONING AND TOLERANCING PER ASME Y14.5-2009.
SHT
BLADE CUFF - PU630917.01
BLADE ADAPTER - PG631713.01
SPACER - PG632883.01 - ROW A
PG632883.02 - ROW B
PG632883.03 - ROW C
COMPRESSOR ROTOR DISC - PG108745 ROW A
PG108760 ROW B
PG108761 ROW C
COMPRESSOR
AIR SIDE
INTERIOR
HUB SIDE
VIEW LOOKING UPSTREAM
ROTATION
GENERAL DISC ASSY
BLADE CUFF SHOWN IN NEUTRAL POSITION
SCALE " 1/16
(COMPRESSOR BLADES AND SPACER/CUFF SEALS OMMITED FOR CLARITY)
RE
D
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Drawing Approved Electronically
RELEASED FOR EXECUTION
09/21/2011
A pp ro ve d fo r P ub lic
R el ea se di st rib ut io n un lim ite d.
DETAIL A
SCALE 1 : 1
A A
B B
C C
D D
Ap pr ov ed b y:
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B C
NOTES: (UNLESS OTHERWISE SPECIFIED)
1. DIMENSIONING AND TOLERANCING PER ASME Y14.5-2009.
(11.116) ROW A
(11.101) ROW B
(11.085) ROW C
(11.318) ROW A
(11.305) ROW B
(11.291) ROW C
SHT
SUCTION SIDE OF
BLADE AND BLADE CUFF
PRESSURE SIDE OF
BLADE AND BLADE CUFF
SPACER/CUFF SEAL
BLADE ADAPTER FACE
BLADE CUFF PIN (CENTER OF ROTATION)
UPPER DOWNSTREAM CORNER
UPPER DOWNSTREAM CORNER
SPACER
SPACER
BLADE CUFF
SPACER/CUFF SEAL
SHT
SHT
RE
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COMPRESSOR ROTATION DIRECTION
CUFF ROTATION AT HIGH POWER
Drawing Approved Electronically
RELEASED FOR EXECUTION
09/21/2011
A pp ro ve d fo r P ub lic
R el ea rib ut io n un lim
DETAIL B
SCALE 8:1
DETAIL C
SCALE 8:1
A A
B B
C C
D D
Ap pr ov ed b y:
Dr aw in g
Nu m be r:
Dr aw n by
Jo b No
Sy st em E ng in ee r:
De sig ne d by
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(.218) ROW A
(.215) ROW B
(.215) ROW C
(.370) ROW A
(.369) ROW B
(.368) ROW C
90° 0'
90° 0'
SPACER CUFF
GAP MEASUREMENT LINE
GAP MEASUREMENT LINE
SPACER
CUFF
PRESSURE SIDE
SUCTION SIDE
NOTES: (UNLESS OTHERWISE SPECIFIED)
1. DIMENSIONING AND TOLERANCING PER ASME Y14.5-2009.
2. GAP MEASUREMENTS ARE APPROXIMATE FOR EACH ROW AND ARE DETERMINED USING THE VIEW LOOKING UPSTREAM ORIENTED PARALLEL TO THE BLADE ADAPTER FACE AS SHOWN IN DETAIL A (SHEET 2). A LINE IS DRAWN PERPENDICULAR TO THE DOWNSTREAM EDGE OF THE SPACER SEAL SURFACE FROM THE UPPER DOWNSTREAM CORNER INTERSECTING THE CUFF FACE AS SHOWN IN DETAILS B AND C.
THE LENGTH OF THIS LINE IS TAKEN AS THE GAP MEASUREMENT.
3. GAPS MEASURED WITH THE BLADE CUFF IN THE NEUTRAL POSITION - SHOWN WITH SEAL REMOVED FOR CLARITY
UPPER DOWNSTREAM CORNER
(.628°)
(1.571°)
UPPER DOWNSTREAM CORNER
SHT
SHT
SHT
SHT
RE
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RA
W
N F
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Drawing Approved Electronically
RELEASED FOR EXECUTION
09/21/2011
A pp ro ve d fo r P ub lic
R el ea rib ut io n un lim
DETAIL D
SCALE 10:1
DETAIL E
SCALE 8:1
A A
B B
C C
D D
Ap pr ov ed b y:
Dr aw in g
Nu m be r:
Dr aw n by
Jo b No
Sy st em E ng in ee r:
De sig ne d by
Dr aw in g
Ch ec k:
ofSh
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No
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Ch ec k:
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.628°
(.097)(.050)
LOCATION OF CUFF FACE
AT MINIMUM FULL LOAD BLADE SWING
DEFLECTION OF SPACER SEAL
SURFACE FACE AT MAX LOAD
NOTES: (UNLESS OTHERWISE SPECIFIED)
1. DIMENSIONING AND TOLERANCING PER ASME Y14.5-2009.
2. MINIMUM REQUIRED BLADE SWING ANGLES:
SUCTION SIDE : GENERATES 5000# BUMPER LOAD WITH 330,000 HP COMPRESSOR INPUT POWER.
PRESSURE SIDE : GENERATES 4000# LOAD WITH VACUUM ON THE PRESSURE SIDE AT SUB-SYNCHRONOUS OPERATION
3. MAXIMUM ADHESIVE THICKNESS
4. MAXIMUM SOLID SEAL HEIGHT
5. DIRECTION OF BLADE/CUFF ROTATION DURING SUB-SYNCHRONOUS OPERATION
6. DIRECTION OF BLADE/CUFF ROTATION DURING SYNCHRONOUS OPERATION
1.571°
(.080) (.050)
3 4
CUFFSPACER CUFF SPACER
DEFLECTION OF SPACER SEAL FACE
AT MAXIMUM LOAD
LOCATION OF CUFF FACE AT
MINIMUM FULL LOAD BLADE SWING
PRESSURE SIDE
SUCTION SIDE
SPACER/CUFF SEAL
SPACER/CUFF SEAL
SHT
SHT
NE
W
S
HE
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KN
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S
DIRECTION OF COMPRESSOR ROTATION
Drawing Approved Electronically
RELEASED FOR EXECUTION
09/21/2011
A pp ro ve d fo r P ub lic
R el ea rib ut io n un lim
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