IP Library › Granted Patent US 8,136,451
Granted Patent B2
US 8,136,451 · App. 13/075,018 · Granted Mar 20, 2012

Ammunition assembly with alternate load path

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 8,136,451
App. No.
13/075,018
Granted
Mar 20, 2012
Kind
B2
Abstract

An ammunition round assembly with alternate load path is disclosed herein. The ammunition round assembly includes a projectile, a body engaging the projectile, and a non-combustible base at least partially enclosing the body. A structural member having first and second engagement portions opposite to each other is positioned inside an interior space defined by the body and the base. The first engagement portion firmly engages the base, and the second engagement portion firmly engages the projectile to provide an alternate load path between the projectile and the base.

Claims (56)

1. An ammunition round assembly, comprising:

a projectile having a leading portion and a trailing portion opposite the leading portion;

a body made of a material configured to be consumed upon firing the ammunition round assembly, the body having an interior area, a first end portion coupled to the projectile, and a second end portion opposite the first end and spaced apart from the projectile;

a non-combustible base at least partially enclosing the second end portion of the body; and

a structural member positioned inside the interior area and having first and second engagement portions, the structural member forming an axially aligned structural interconnection between the base and the projectile, the first engagement portion securely coupled to the base and spaced apart from the projectile, and the second engagement portion securely coupled to the trailing portion of the projectile and spaced apart from the base, wherein the projectile, the structural member, and the base define a load path that substantially isolates the body from loads applied to the projectile or the base.

2. The ammunition round assembly of claim 1 , further comprising an ignition device extending through the base and securely engaging the structural member.

3. The ammunition round assembly of claim 1 wherein the first engagement portion includes a hollow portion adjacent to the base, and the base has a boss configured to engage the hollow portion of the first engagement portion.

4. The ammunition round assembly of claim 3 , further comprising an ignition device connectable to the base wherein the first engagement portion and the boss are configured to receive at least a portion of the ignition device.

5. The ammunition round assembly of claim 1 wherein the base has an alignment portion that aligns the structural member relative to the base.

6. The ammunition round assembly of claim 1 wherein at least one of the base and the structural member has an anti-rotation device that substantially blocks rotation of the structural member relative to the base.

7. The ammunition round assembly of claim 1 wherein the structural member further includes a portion adjacent to the base that has a plurality of apertures configured to allow ignition gases to pass therethrough to ignite a propellant in the interior area of the body.

8. The ammunition round assembly of claim 1 wherein the structural member is at least partially hollow and configured to contain an ignition device, the structural member having a plurality of ignition pathways in communication with the interior area of the body.

9. The ammunition round assembly of claim 1 , further comprising an ignition device connectable to the base and the structural member, the ignition device configured to hold the structural member in firm engagement with the base.

10. The ammunition round assembly of claim 1 wherein the second engagement portion includes a break-joint feature configured to break when the ammunition round is fired, thereby separating the projectile from the structural member.

11. The ammunition round assembly of claim 1 wherein the projectile includes a programmable portion, and further includes a communication data link extending between the base and the programmable portion and along a portion of the structural member.

12. The ammunition round assembly of claim 1 wherein the projectile includes a programmable portion, and further comprising a communication data link coupled to the programmable portion and extending through a portion of the structural member, the communication data link being connected to a connector configured to allow projectile programming data to pass therethrough.

13. The ammunition round assembly of claim 1 wherein the structural member has a conduit portion, and the projectile has a programmable fuse, and further comprising a communication data link disposed in the conduit portion of the structural member and coupled to the programmable fuse.

14. The ammunition round assembly of claim 1 where in the projectile has a programmable portion and further comprising a communication data link coupled to the programmable portion, the base having a contact portion operably coupled to the communication data link, the contact portion and communication data link being configured so the programmable portion can be programmed by data passing through the contact portion and the communication data link when the ammunition round assembly is in a firing device.

15. The ammunition round assembly of claim 1 wherein the first engagement portion is directly coupled to the base, and wherein the second engagement portion is directly coupled to the trailing portion of the projectile.

16. The ammunition round assembly of claim 15 , further comprising an intermediate feature between at least one of the first engagement portion and the base and the second engagement feature and the trailing portion of the projectile.

17. An ammunition round assembly, comprising:

a projectile having a longitudinal axis, a leading portion, and a trailing portion opposite the leading portion;

a body having an interior area and being made of a material configured to be consumed upon firing the ammunition round assembly;

a base connected to the body spaced apart from the projectile;

a structural member structurally interconnecting the trailing portion of the projectile and the base and configured to form a load path there between to substantially isolate the body from loads applied to the projectile on the base, the structural member being substantially axially aligned with the longitudinal axis of the projectile, wherein the structural member includes a hollow portion at the first engagement member;

a propellant charge disposed in the interior area of the body and around the structural member; and

an ignition device at least partially in the hollow portion of the structural member.

18. The ammunition round assembly of claim 17 wherein the structural member is substantially rigid.

19. The ammunition round assembly of claim 17 wherein the structural member includes a hollow tube having a plurality of apertures therein.

20. The ammunition round assembly of claim 17 wherein the structural member further includes a break-joint feature configured to disjoint at a specific tension loading.

21. The ammunition round assembly of claim 17 wherein the structural member includes a first cup-shaped structure having an inner wall surface, an outer wall surface, and a countersunk tapered surface extending between the inner and outer wall surfaces.

22. The ammunition round assembly of claim 21 wherein structural member further includes a pin extending from the countersunk tapered surface of the first cup-shaped structure.

23. The ammunition round assembly of claim 17 wherein the ignition device extends through the base and engages the structural member.

24. The ammunition round assembly of claim 17 , further comprising a programmable fuse coupled to the projectile, at least one communication port coupled to the base, and communication members extending through the hollow portion of the structural member between the programmable fuse and the communication port.

25. The ammunition round assembly of claim 17 wherein the hollow portion extends along an intermediate portion of the structural member between the projectile and the base.

26. An ammunition round assembly, comprising:

a projectile having a trailing portion and a leading portion;

a body made of a material configured to be consumed upon firing the ammunition round assembly, the body having an interior area, a first end portion coupled to the projectile, and a second end portion opposite the first end;

a non-combustible base at least partially enclosing the second end portion of the body;

a structural member positioned inside the interior area and having first and second engagement portions, the structural member axially aligned with the projectile and forming a structural interconnection between the base and the projectile, the first engagement portion securely coupled to the base and the second engagement portion securely coupled to the projectile, wherein the second engagement portion includes a break-joint feature configured to break when the ammunition round is fired to separate the projectile from the structural member and the base, and wherein the structural member is configured to substantially isolate the body from loads applied to the projectile or the base;

a propellant contained in the body and disposed about the structural member; and

an ignition device attached to the base and extending into a least a portion of the structural member, the structural member being configured to allow the ignition device to ignite the propellant upon ignition of the ignition device.

27. The ammunition round assembly of claim 26 wherein the first engagement portion includes a hollow portion adjacent to the base, and the base has a boss configured to engage the hollow portion of the first engagement portion.

28. The ammunition round assembly of claim 27 wherein the first engagement portion and the boss are configured to receive at least a portion of the ignition device.

29. The ammunition round assembly of claim 26 wherein the base has an alignment portion that aligns the structural member relative to the base.

30. The ammunition round assembly of claim 26 wherein at least one of the base and the structural member has an anti-rotation device that substantially blocks rotation of the structural member relative to the base.

31. The ammunition round assembly of claim 26 wherein the break-joint feature is a hollow tubular structure having a reduced wall thickness.

32. The ammunition round assembly of claim 26 wherein the projectile includes a programmable portion, and further includes a communication data link extending between the base and the programmable portion and along a portion of the structural member.

33. The ammunition round assembly of claim 26 wherein the structural member has an axial passageway therethrough, and the projectile includes a programmable portion, and further includes a communication data link extending between the base and the programmable portion through the axial passageway of the structural member.

34. An ammunition round assembly, comprising:

a projectile having a leading portion, a trailing portion opposite the leading portion, and a programmable portion;

a body having an interior area, a first end portion coupled to the projectile, and a second end portion opposite the first end, wherein the body is made of a material configured to be consumed upon firing the ammunition round assembly;

a non-combustible base at least partially enclosing the second end portion of the body;

a structural member within the interior area of the body and coaxially aligned with the projectile, the structural member having a first engagement portion, a second engagement portion opposite the first engagement portion, and a conduit between the first and second engagement portions, the first engagement portion connected to the base and spaced apart from the projectile, the second engagement portion connected to the trailing portion of the projectile and spaced apart from the base, the structural member forming an axially aligned structural interconnection between the base and the projectile such that the projectile, the structural member, and the base define a load path that substantially isolates the body from loads applied to the projectile or the base;

a propellant charge in the interior area of the body; and

at least one communication link extending through the conduit of the structural member and connected to the programmable portion of the projectile, wherein the conduit is configured to substantially isolate the communication link from the propellant charge.

Assignments (11)
RELEASE OF PATENT SECURITY AGREEMENT RECORDED APRIL 3, 2019 AT REEL/FRAME 048788/0581 Recorded Jun 6, 2024
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE
To: TRANSDIGM INC.; TRANSDIGM GROUP INCORPORATED; AEROSONIC LLC; MOUNTAINTOP TECHNOLOGIES, INC.; AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; SHIELD RESTRAINT SYSTEMS, INC.; AMSAFE, INC.; ARKWIN INDUSTRIES, INC.; AVIONIC INSTRUMENTS, INC.; AEROSONIC CORPORATION; AVTECHTYEE, INC.; BREEZE-EASTERN LLC; BRUCE AEROSPACE INC.; CEF INDUSTRIES, LLC; CHAMPION AEROSPACE LLC; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; PURE TECHNOLOGIES LTD.; HARCO LABORATORIES, INC.; HARCO LLC; HARCO TECHNOLOGIES CORPORATION; CORRPRO COMPANIES, INC.; HARCO CORPORATION; HARTWELL CORPORATION; MARATHONNORCO AEROSPACE, INC.; PNEUDRAULICS, INC.; SCHNELLER LLC; SEMCO INSTRUMENTS, INC.; TACTAIR FLUID CONTROLS, INC.; TEAC AEROSPACE TECHNOLOGIES, INC.; TELAIR INTERNATIONAL GMBH; TELAIR INTERNATIONAL AB; NORDISK AVIATION PRODUCTS AS; TURNTIME TECHNOLOGIES AB; AEROCONTROLEX GROUP, INC.; TRANSICOIL INC.; SOUTHCO, INC.; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; ARMTEC COUNTERMEASURES CO.; ADVANCED INPUT DEVICES, INC.; ARMTEC DEFENSE PRODUCTS COMPANY; JOSLYN SUNBANK COMPANY LLC; LEACH INTERNATIONAL CORPORATION; SOURIAU USA, INC.; NMC GROUP, INC.; TA AEROSPACE CO.; MASON ELECTRIC CO.; KORRY ELECTRONICS CO.; PALOMAR PRODUCTS, INC.; ROLLS-ROYCE PLC; MEMTRON TECHNOLOGIES CO.; CHELTON, INC. (N/K/A CHELTON AVIONICS, INC.); SIMPLEX MANUFACTURING CO.; APICAL INDUSTRIES, INC.; AERO-INSTRUMENTS CO., LLC; AIRBORNE SYSTEMS NA, INC.; HARCOSEMCO LLC; HARCO, LLC (N/K/A HARCOSEMCO LLC); PEXCO AEROSPACE, INC.; TELAIR US LLC; CALSPAN AERO SYSTEMS ENGINEERING, INC.; CALSPAN SYSTEMS, LLC; ADAMS RITE AEROSPACE, INC.; ACME AEROSPACE, INC.; SCHNELLER, INC.; CEF INDUSTRIES, INC.
Reel/Frame 067640/0237 →
CORRECTIVE ASSIGNMENT TO CORRECT THE NATURE OF CONVEYANCE PREVIOUSLY RECORDED AT REEL: 064961 FRAME: 0671. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT OF PATENT AND TRADEMARK SECURITY INTEREST. Recorded Oct 5, 2023
From: CREDIT SUISSE AG, CAYMAN ISLANDS BRANCH, AS PREDECESSOR COLLATERAL AGENT
To: GOLDMAN SACHS BANK USA, AS SUCCESSOR COLLATERAL AGENT
Reel/Frame 065132/0644 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 20, 2023
From: CREDIT SUISSE AG, CAYMAN ISLANDS BRANCH, AS PREDECESSOR COLLATERAL AGENT
To: GOLDMAN SACHS BANK USA, AS SUCCESSOR COLLATERAL AGENT
Reel/Frame 064961/0671 →
RELEASE OF SECURITY INTEREST Recorded Apr 19, 2023
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE
To: TA AEROSPACE CO.; TRANSDIGM, INC.; TRANSDIGM GROUP INCORPORATED; ACME AEROSPACE, INC.; ADAMS RITE AEROSPACE, INC.; AEROCONTROLEX GROUP, INC.; AEROSONIC CORPORATION; AIRBORNE HOLDINGS, INC.; AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; AMSAFE COMMERCIAL PRODUCTS INC.; AMSAFE, INC.; ARKWIN INDUSTRIES, INC.; AVIONIC INSTRUMENTS LLC; AVIONICS SPECIALTIES, INC.; AVTECH TYEE, INC.; BEAM'S INDUSTRIES; BREEZE EASTERN CORPORATION; BRUCE AEROSPACE, INC.; CEF INDUSTRIES, INC.; CHAMPION AEROSPACE LLC; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; ELECTROMECH TECHNOLOGIES LLC; HARCO LABORATORIES, INC.; HARCO LLC; HARTWELL CORPORATION; MARATHONNORCO AEROSPACE, INC.; PEXCO AEROSPACE, INC.; PNEUDRAULICS, INC.; SCHNELLER LLC; SEMCO INSTRUMENTS, INC.; SHIELD RESTRAINT SYSTEMS, INC.; TACTAIR FLUID CONTROLS INC.; TEAC AEROSPACE TECHNOLOGIES, INC.; TELAIR INTERNATIONAL LLC; TRANSCOIL LLC; WESTERN SKY INDUSTRIES, LLC; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; ARMTEC COUNTERMEASURES CO.; ARMTEC DEFENSE PRODUCTS COMPANY; LEACH INTERNATIONAL CORPORATION; NMC GROUP INC.; MASON ELECTRIC CO.; KORRY ELECTRONICS CO.; PALOMAR PRODUCTS, INC.; CHELTON, INC. (N/K/A CHELTON AVIONICS, INC.); SIMPLEX MANUFACTURING CO.; APICAL INDUSTRIES, INC.
Reel/Frame 063363/0753 →
SECURITY INTEREST Recorded Feb 27, 2023
From: TRANSDIGM INC.; TRANSDIGM GROUP INCORPORATED; 17111 WATERVIEW PKWY LLC; ACME AEROSPACE, INC.; ADAMS RITE AEROSPACE, INC.; AEROCONTROLEX GROUP, INC.; AEROSONIC LLC; AIRBORNE ACQUISITION, INC.; AIRBORNE GLOBAL, INC.; AIRBORNE HOLDINGS, INC.; AIRBORNE SYSTEMS NA INC.; AIRBORNE SYSTEMS NORTH AMERICA INC.; AIRBORNE SYSTEMS NORTH AMERICA OF CA INC.; AMSAFE GLOBAL HOLDINGS, INC.; AMSAFE, INC.; ANGUS ELECTRONICS CO.; APICAL INDUSTRIES, INC.; ARKWIN INDUSTRIES, INC.; ARMTEC COUNTERMEASURES CO.; ARMTEC COUNTERMEASURES TNO CO.; ARMTEC DEFENSE PRODUCTS CO.; AUXITROL WESTON USA, INC.; AVIATION TECHNOLOGIES, INC.; AVIONIC INSTRUMENTS LLC; AVIONICS SPECIALTIES, INC.; AVTECHTYEE, INC.; BETA TRANSFORMER TECHNOLOGY LLC; BREEZE-EASTERN LLC; BRIDPORT HOLDINGS, INC.; BRIDPORT-AIR CARRIER, INC.; BRUCE AEROSPACE INC.; CDA INTERCORP LLC; CEF INDUSTRIES, LLC; CENTURY HELICOPTERS, INC.; CHAMPION AEROSPACE LLC; CHELTON AVIONICS HOLDINGS, INC.; CHELTON AVIONICS, INC.; CHELTON DEFENSE PRODUCTS, INC.; CMC ELECTRONICS AURORA LLC; DART AEROSPACE USA, INC.; DART BUYER, INC.; DART HELICOPTER SERVICES, INC.; DART INTERMEDIATE, INC.; DART TOPCO, INC.; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; ELECTROMECH TECHNOLOGIES LLC; ESTERLINE EUROPE COMPANY LLC; ESTERLINE INTERNATIONAL COMPANY; ESTERLINE TECHNOLOGIES CORPORATION; ESTERLINE TECHNOLOGIES SGIP LLC; HARCOSEMCO LLC; HARTWELL CORPORATION; HELI TECH, INC.; HYTEK FINISHES CO.; ILC HOLDINGS, INC.; JANCO CORPORATION; JOHNSON LIVERPOOL LLC; KIRKHILL INC.; KORRY ELECTRONICS CO.; LEACH HOLDING CORPORATION; LEACH INTERNATIONAL CORPORATION; LEACH MEXICO HOLDING LLC; LEACH TECHNOLOGY GROUP, INC.; MARATHONNORCO AEROSPACE, INC.; MASON ELECTRIC CO.; MCKECHNIE AEROSPACE DE, INC.; MCKECHNIE AEROSPACE HOLDINGS, INC.; MCKECHNIE AEROSPACE US LLC; NAT SEATTLE INC.; NMC GROUP, INC.; NORDISK AVIATION PRODUCTS LLC; NORTH HILLS SIGNAL PROCESSING CORP.; NORTH HILLS SIGNAL PROCESSING OVERSEAS LLC; NORWICH AERO PRODUCTS, INC.; OFFSHORE HELICOPTER SUPPORT SERVICES, INC.; PALOMAR PRODUCTS, INC.; PARAVION TECHNOLOGY, INC.; PEXCO AEROSPACE, INC.; PNEUDRAULICS, INC.; POWER DEVICE CORPORATION; SCHNELLER LLC; SEMCO INSTRUMENTS, INC.; SHIELD RESTRAINT SYSTEMS, INC.; SIMPLEX MANUFACTURING CO.; SKANDIA, INC.; SKURKA AEROSPACE INC.; SYMETRICS INDUSTRIES, LLC; TA AEROSPACE CO.; TACTAIR FLUID CONTROLS, INC.; TDG ESL HOLDINGS INC.; TEAC AEROSPACE TECHNOLOGIES, INC.; TELAIR US LLC; TEXAS ROTRONICS, INC.; TRANSICOIL LLC; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; BRIDPORT ERIE AVIATION, INC.; TRANSDIGM UK HOLDINGS PLC
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE
Reel/Frame 063012/0788 →
PATENT SECURITY AGREEMENT Recorded Apr 9, 2020
From: AIRBORNE SYSTEMS NORTH AMERICA OF NJ INC.; ACME AEROSPACE, INC.; ADAMS RITE AEROSPACE, INC.; AEROCONTROLEX GROUP, INC.; AEROSONIC CORPORATION/LLC; AIRBORNE HOLDINGS, INC.; AMSAFE COMMERCIAL PRODUCTS INC.; AMSAFE, INC.; ARKWIN INDUSTRIES, INC.; AVIONIC INSTRUMENTS LLC; AVIONICS SPECIALTIES, INC.; AVTECHTYEE, INC.; BEAM’S INDUSTRIES; BREEZE-EASTERN CORPORATION; BRUCE AEROSPACE, INC.; CEF INDUSTRIES, INC.; CHAMPION AEROSPACE LLC; DATA DEVICE CORPORATION; DUKES AEROSPACE, INC.; ELECTROMECH TECHNOLOGIES LLC; HARCO LABORATORIES, INCORPORATED; HARCO LLC; HARTWELL CORPORATION; MARATHONNORCO AEROSPACE, INC.; PEXCO AEROSPACE, INC.; PNEUDRAULICS, INC.; SCHNELLER LLC; SEMCO INSTRUMENTS, INC.; SHIELD RESTRAINT SYSTEMS, INC.; TACTAIR FLUID CONTROLS, INC.; TEAC AEROSPACE TECHNOLOGIES, INC.; TELAIR INTERNATIONAL LLC; TRANSDIGM, INC.; TRANSCOIL LLC; WESTERN SKY INDUSTRIES, LLC; WHIPPANY ACTUATION SYSTEMS, LLC; YOUNG & FRANKLIN INC.; ARMTEC COUNTERMEASURES CO.; ARMTEC DEFENSE PRODUCTS COMPANY; ARMTEC DEFENSE PRODUCTS CO.; LEACH INTERNATIONAL CORPORATION; NMC GROUP, INC.; TA AEROSPACE CO.; MASON ELECTRIC COMPANY; KORRY ELECTRONICS CO.; PALOMAR PRODUCTS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS TRUSTEE AND NOTES COLLATERAL AGENT
Reel/Frame 052352/0704 →
SECURITY INTEREST Recorded Apr 3, 2019
From: SOURIAU USA, INC.; LEACH INTERNATIONAL CORPORATION; TA AEROSPACE CO.; ADVANCED INPUT DEVICES, INC.; MASON ELECTRIC CO.; NMC GROUP, INC.; PALOMAR PRODUCTS, INC.; KORRY ELECTRONICS CO.; MEMTRON TECHNOLOGIES CO.; JOSLYN SUNBANK COMPANY, LLC; ARMTEC DEFENSE PRODUCTS CO.; ARMTEC COUNTERMEASURES CO.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 048788/0581 →
SECURITY INTEREST Recorded Apr 3, 2019
From: SOURIAU USA, INC.; LEACH INTERNATIONAL CORPORATION; TA AEROSPACE CO.; ADVANCED INPUT DEVICES, INC.; MASON ELECTRIC CO.; NMC GROUP, INC.; PALOMAR PRODUCTS, INC.; KORRY ELECTRONICS CO.; MEMTRON TECHNOLOGIES CO.; JOSLYN SUNBANK COMPANY, LLC; ARMTEC DEFENSE PRODUCTS CO.; ARMTEC COUNTERMEASURES CO.
To: CREDIT SUISSE AG
Reel/Frame 048788/0719 →
RELEASE OF SECURITY INTEREST Recorded Mar 15, 2019
From: WELLS FARGO BANK, NATIONAL ASSOCIATION
To: ADVANCED INPUT DEVICES, INC.; ARMTEC DEFENSE PRODUCTS CO.; KIRKHILL-TA CO.; KORRY ELECTRONICS CO.; LEACH INTERNATIONAL CORPORATION; MASON ELECTRIC CO.; NMC GROUP,INC.; PACIFIC AEROSPACE & ELECTRONICS, INC.
Reel/Frame 048609/0901 →
SECURITY INTEREST Recorded May 15, 2015
From: ADVANCED INPUT DEVICES, INC.; ARMTEC DEFENSE PRODUCTS CO.; KIRKHILL-TA CO.; KORRY ELECTRONICS CO.; LEACH INTERNATIONAL CORPORATION; MASON ELECTRIC CO.; NMC GROUP, INC.; PACIFIC AEROSPACE & ELECTRONICS, INC.
To: WELLS FARGO BANK, NATIONAL ASSOCIATION
Reel/Frame 035676/0001 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 21, 2011
From: MUTASCIO, ENRICO R.
To: ARMTEC DEFENSE PRODUCTS CO.
Reel/Frame 026470/0294 →