Patent Assignment
Reel/Frame 024864/0016
Security Agreement
Recorded: 2010-08-20
Received: 2010-08-20
Pages: 24
Assignor
HEXCEL CORPORATION
Executed: 2010-07-09
Assignee
BANK OF AMERICA, N.A.
101 SOUTH TRYON STREET, NC1-002-15-36, CHARLOTTE, NC, 28255, UNITED STATES
Covered Properties
(45)
Method for Making Composite Material with Blend of Thermoplastic Particles
Application:
12/792,338 →
Helicopter Blade Mandrel
Application:
12/787,439 →
Carbon Fibers Having Improved Strength and Modulus and an Associated Method and Apparatus for Preparing Same
Application:
12/783,069 →
Composite Material For Structural Applications
Application:
12/764,636 →
Method for Molding Composite Structures
Application:
12/726,677 →
Corrosion Resistant Honeycomb
Application:
12/714,565 →
Thermoplastic-Toughened Cyanate Ester Resin Composites with Low Heat Release Properties
Application:
12/713,534 →
Composite Materials with Improved Burn Properties
Application:
12/569,817 →
Method of Molding Complex Composite Parts Using Pre-Plied Multi-Directional Continuous Fiber Laminate
Application:
12/561,492 →
Aerospace Articles Made from Quasi-Isotropic Chopped Prepreg
Application:
12/508,777 →
Epoxy Resin and 4,4'-Diaminobenzanilide Powder
Application:
12/468,926 →
Method for Molding Composite Structures
Application:
12/400,017 →
Prepreg With Integrated Multi-Dimensional Gas Venting Network
Application:
12/358,302 →
Epoxy Resins with Improved Burn Properties
Application:
12/287,202 →
Acoustic Septum Cap Honeycomb
Application:
12/151,886 →
Helicopter Blade Mandrel with Roller Assembly
Application:
12/011,344 →
Composite Materials with Blend of Thermoplastic Particles
Application:
11/787,701 →
Pre-Impregnated Composite Materials with Improved Performance
Application:
11/787,700 →
Acoustic Septum Cap Honeycomb
Application:
11/726,451 →
Carbon Fibers Having Improved Strength and Modulus and an Associated Method and Apparatus for Preparing Same
Application:
11/562,867 →
Aerospace Articles Made from Quasi-Isotropic Chopped Prepreg
Application:
11/476,965 →
Corrosion Resistant Honeycomb
Application:
11/476,964 →
Aircraft Floor and Interior Panels Using Edge Coated Honeycomb
Application:
11/471,078 →
Rubber-Modified Edge Coating for Honeycomb Used in Panels with Composite Face Sheets
Application:
11/432,780 →
Pressurized Molding of Composite Parts
Application:
11/331,511 →
Bismaleimide Prepreg Systems
Application:
11/300,135 →
Edge Coating for Honeycomb Used in Panels with Composite Face Sheets
Application:
11/295,829 →
Aircraft Floor Panels Using Edge Coated Honeycomb
Application:
11/228,601 →
Machinable Composite Mold
Application:
11/180,831 →
Resin compositions with high thermoplatic loading
Application:
11/168,971 →
Acoustic Septum Cap Honeycomb
Application:
11/099,337 →
Optimized Layout for Multi-Bit Memory Banks Each with Two Data Latches and Two Arithmetic Circuits
Application:
10/503,619 →
Interlock Double Weave Fabric and Methods of Making and Using the Same
Application:
10/979,574 →
Edge Coating for Honeycomb Used in Panels with Composite Face Sheets
Application:
10/932,510 →
Method for Making Amine-Terminated Polyarylene Polyethers
Application:
10/740,095 →
Heat-Settable Resins
Application:
10/672,006 →
Friction Lining for Wet Running
Application:
10/149,638 →
Room Temperature Stable Epoxy Prepregs
Application:
10/243,077 →
Energy Absorbing Composite Tube
Application:
10/159,653 →
Chromate-Free Coating for Metal Honeycomb
Application:
10/062,827 →
Stretch Breaking of Fibers
Application:
10/022,129 →
Forming Process for Cellulose Paper Based Honeycomb Structures
Application:
09/970,740 →
Low Smoke Producing Resin for Use in Honeycomb Sandwich Panels
Application:
09/930,071 →
Core-Crush Resistant Fabric and Prepreg for Fiber Reinforced Composite Sandwich Structures
Application:
09/876,310 →
Self-Adhesive Prepreg Face Sheet for Sandwich Panels
Application:
09/795,177 →