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Air Defense Systems Division, Pomona, CA 1982 - 1991Accomplished integration of the U.S. Navy’s Standard Missile II Block-2 weapon systems aboard Kidd-Class Destroyers.
Farnam Sealing Systems, Troy, MI 1992 – 1995
Managed the design and application of an accelerated fatigue test stand that led to the successful root-cause detection for Ford Motor Company’s 2.0 Liter Head gasket cylinder chamber coolant/oil leak problem.
Patriot Sensors & Controls, Troy, MI
1995 - 1996
J32
4
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J1
J23
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TP2
TP3
TP4
G. Blowycky\data\951\circuit3.ds46-21-96 (Friday)
RX
TX
RS232 BufferIDL-1
TC232CPE
+ 5 vdc
PowerSupply
+ 5 vdc
-12 vdc
+12 vdc
Gnd+ 12.5 vdc
68HC711E9 Programmer Test Fixture
MODB / VSTBY
XIRQ / VPP
______RESET
+ 5 vdc
-12 vdc
+12 vdc
951C
PU
Boa
rd
330 ohm
10K
ohm
2N4401
1K o
hm
Aromat
DK1a1bE-5V
7
8
13
10
9
12
43
65
DS1233
Reset Chip
___Rst
Vcc3
2
1
Power On LEDJ5
1K ohm
Red
Black
Green
White
Black
J6
RX
TX
Sig. Gnd. PC
Com
Por
t
RTS
CTS
DTR (Reserved)
DSR (Reserved)
J4 DB-25
2
3
4
5
7
20
6
Yellow
J3
Orange
Green
Red
Black
Orange
Yellow
S1
J2Orange
Black
Red
J2
Green
J1
Yellow
Orange
Green
Black
Red
Yellow
Orange
11 141
34
515
.1uF
.1uF
6
2
.1uF
16
.1uF
+ 5 vdc
.1uF
1N4007
N.C.
1N4007
N.C.
1N4007
N.C.
1N4007
N.C.
1N4007
N.C.
8 1
5 6
8
8
8
8
5
5
5
5
1
1
1
1
6
6
6
6
ELECTRONIC HARDWARE PRODUCT SUPPORT TEST ENGINEER managed the successful design and application of a new production method to reliably download firmware to Motorola's 68HC711E9 Micro-Controller using a PC based system for the company’s Model 951 Linear Displacement Transducer (LDT).
Engine Technology, Auburn Hills, MI 1996 - 2006Test Cell Project Engineer for the design, proposal, installation, verification, commissioning, and systems support of twelve brand new $1.2 million dollar internal combustion engine dynamometer test stands as well as two NVH and two transient simulation test stands. Employing MTS’s ADAPT-Redline PLC.
Stratford, CT 2006- 2009
SENIOR ELECTRICAL INSTRUMENTATION PROJECT ENGINEER awarded special commendation for project management innovation of instrumentation and data acquisition systems used in the U.S. Army’s Blackhawk Systems Integration Laboratory.
Stratford, CT 2006- 2009
SENIOR ELECTRICAL INSTRUMENTATION PROJECT ENGINEER assigned to reactivate Sikorsky’s Tail Rotor Test Stand after a ten-year stand-down.
Tail Rotor Whirl Stand Beanie Wiring
DRAWN BY:
APPROVED BY:
CHECKED BY:
DESIGNER:G. Blowycky
G. Blowycky
DRAWING TITLE
REV.DWG NO.
SCALE:NA
SHEET
S-76D TAIL ROTOR TESTING AT WHIRL-STAND
TAIL ROTOR INSTRUMENTATION CONNECTIVITY TO BEANIE TO J -BOX
A
29 FEB 2008DATE:
TAIL ROTOR BEANIE
TR-WHIRL CONTROL ROOM
TREB1Sa TR Edgewise Spar Bending,Sta 4, Red Blade350FULL BENDING BRIDGE
J
A
E
N
B C D
F G H
K L M
P R S
T U V W
TAIL ROTOR GAGES
DB-15 (PC-1)
Rotating Patch Sequence A
BLK
BRN
RED
ORN
TR-WHIRL PEDESTAL TEST AREA
Rotating Pedestal J uction Box
DC-1 Terminal Strips
P-1MS3472W16-26P
TR SLIP RINGW60-19-100
Cables from TR Slip-Ring to J unction Box
Terminal Box DC-1 Strips
D
C
B
A
N
P
R
S
J
M
L
K
H
G
F
E
N
P
R
S
J
M
L
K
D
C
B
A
H
G
F
E
D
C
B
A
N
P
R
S
M
K
J
L
H
G
F
E
J -1MS3476W16-26S(Rotating Connector)
CAMU Rear RecepticalChannel Wiring
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9
11
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10
13
15
16
14
9
12
11
10
13
14
15
16
4
3
2
5
6
7
8
1
D
C
B
E
F
G
H
A
PRECESSION SLIP RINGW102-100
J -1PT02E-16-26P
(Stationary Connector)
Cables from PrecessionTR Slip-Rings to CAMU
P-1MS3472W16-26S P-1
MS3471W16-26PJ -1MS3470W16-26S
D
C
B
A
N
P
R
S
J
M
L
K
F
G
H
E
D
C
B
E
F
G
H
A
J
L
K
M
N
S
P
R
C
B
D
E
H
F
G
A1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
N
S
P
R
J
L
K
M
C
B
D
E
H
F
G
A
Cables fromTerminal Box DC-1 Stripsto Precession Slip Rings
J -1MS3476W16-26S
P-1MS3472W16-26P
D
C
B
A
H
G
F
E
D
C
B
A
H
G
F
E
N
P
R
S
M
K
J
L
N
P
R
S
M
K
J
L
D
C
B
A
N
P
R
S
J
M
L
K
F
G
H
E
N
P
R
S
J
M
L
K
N
P
R
S
J
M
L
K
BRN
BRN / WHT
BRN / BLK
BRN / GRY
RED
RED / WHT
RED / BLK
RED / GRY
ORG
ORG / WHT
ORG / BLK
ORG / GRY
YEL
YEL / WHT
YEL / BLK
YEL / GRY
P-1
JT06
RE
18-3
2 S
J-1
JT02
RE
18-3
2P(S
tatio
nary
Con
nect
or)
D
C
B
A
N
P
R
S
J
M
L
K
F
G
H
E
D
C
B
A
N
P
R
S
J
M
L
K
F
G
H
E
P-1
MS
347 1
W1 6
-26 P
J-1
MS
3472
W16
-26S
BRN
BRN / WHT
BRN / BLK
BRN / GRY
RED
RED / WHT
RED / BLK
RED / GRY
ORG
ORG / WHT
ORG / BLK
ORG / GRY
YEL
YEL / WHT
YEL / BLK
YEL / GRY
BRN
BRN / WHT
BRN / BLK
BRN / GRY
RED
RED / WHT
RED / BLK
RED / GRY
ORG
ORG / WHT
ORG / BLK
ORG / GRY
YEL
YEL / WHT
YEL / BLK
YEL / GRY
BRN
BRN / WHT
BRN / BLK
BRN / GRY
RED
RED / WHT
RED / BLK
RED / GRY
ORG
ORG / WHT
ORG / BLK
ORG / GRY
YEL
YEL / WHT
YEL / BLK
YEL / GRY
C H 1
C H 2
C H 3
C H 4
(S60817)
(S60807)
(S60798)
(S60810)
1
4
2
3
9
11
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12
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16
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15
3
2
4
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1
P-3
MD
M-3
1PH
006B
J-3
MD
M-3
1SH
001P
(Rot
atin
g C
onne
ctor
)
PAGE 1
TRPBEAMaPitch Link Axial Load-Red Blade FULL BENDING BRIDGE(measuring axial load)
J-5
Circ
ular
Con
n.P
-5C
ircul
ar C
onn.
BLK/RED & RED/WHT
RED/WHT & RED/BLK
RED/BLK & RED
RED & BLK/RED
1
2
3
4
1
2
3
4
BLK
BRN
RED
ORN
TRNB1SaTR Noraml Spar Bending,Sta 4, RED Blade350HALF BENDING BRIDGE
DB-23 (PC-2)BLU
VIOGRY
YEL
GRN
BLU
VIOJ
A
E
N
B C D
F G H
K L M
P R S
T U V W
5
8
6
7
BLU
VIO
GRY
7
8
9
7
8
9
J
A
E
N
B C D
F G H
K L M
P R S
T U V W
DB-22 (PC-3)
9
11
10
12
TR145TS1TR SPAR TS1 (LE SIDE)Sta 14.5, Red Blade350Total Strain
13
16
14
15
(PC-4)
21WHT/RED
WHT/ORN
WHT/YEL
WHT/GRN22
WHT/BLK/RED
WHT/BLK/ORN
3
4
5
6
3
4
5
6
21
22
J-1
MD
M-5
1SH
048B
P-1
MD
M-5
1PH
048B
(PC-x) : PATCH CORD NUMBER(DB-x) : DEUTCH BLOCK NUMBER
RED
ORN
YEL
GRN
RED
ORN
YEL
GRN
GRY
WHT
WHT/BLK
WHT/BRN
DEUTSCH CONNECTOR P/N CTJ 122 E 05E 513
WHT/BLK/RED
DB-27
WHT/BLK/ORN
A
N
B
F G
K L
R
T U V W
D
H
M
S
D
H
M
S
T U V W
C
A
E
J
N
E
J
P
B
F
K
P
C
G
L
R
X
X
X PATCH CABLE SET A
PATCH CABLE SET B
PATCH CABLE SET C
DB-31
RED
WH
T
BLK
GR
N
National Railroad Passenger Corporation, New Haven, CT 2009-2010
ELECTRICAL ENGINEERNG TECHNICAL SPECIALIST - Successfully performed numerous diagnosis and repairs on locomotive systems while train is in active revenue service
National Railroad Passenger Corporation, Wilmington, DE 2014 -Present
ELECTRICAL ENGINEER / FLEET ENGINEERWork with Amtrak Program Office to commission 70 new Siemens ACS-64 Electric Locomotives for the Northeast Corridor (NEC).
