IP Library Assignment 030891/0135
Patent Assignment
Reel/Frame 030891/0135

Assignment of Assignor's Interest

Recorded: 2013-07-28 Pages: 29
Assignor
BELL HELICOPTER TEXTRON INC.
Executed: 2013-02-15
Assignee
TEXTRON INNOVATIONS INC.
40 WESTMINSTER STREET, PROVIDENCE, RHODE ISLAND, 02903
Covered Properties (84)
Short Beam Shear Test Fixture
Patent: 8,950,270 →
Application: 13/347,488 →
Publication: US 2012/0222491
Tilt Rotor Aircraft with Fixed Engine Arrangement
Patent: 8,602,347 →
Application: 13/357,981 →
Publication: US 2012/0199699
System and Method of Harvesting Power with a Rotor Hub Damper
Patent: 9,260,185 →
Application: 13/358,046 →
Publication: US 2013/0189098
Window Mounted Raft System
Patent: 9,238,508 →
Application: 13/359,584 →
Publication: US 2012/0193474
Optimized Core for a Structural Assembly
Patent: 9,096,316 →
Application: 13/363,794 →
Publication: US 2013/0195672
System and Method of Actuating a Swashplate for Main Rotor Control
Patent: 9,156,547 →
Application: 13/370,130 →
Publication: US 2013/0209252
Flight Control Laws for Constant Vector Flat Turns
Patent: 8,332,082 →
Application: 13/391,522 →
Publication: US 2012/0253558
Rotor Hub for Use with High-Inertia Blades
Patent: 8,444,382 →
Application: 13/391,708 →
Publication: US 2013/0004311
Hub Assembly with Centrifugal and Radial Bearings
Patent: 9,156,544 →
Application: 13/400,837 →
Publication: US 2013/0216382
Coaxial Counter-Rotating Rotor System
Patent: 9,169,012 →
Application: 13/401,110 →
Publication: US 2013/0214087
Compact Rotorcraft Dual-Element Spherical Elastomeric Centrifugal-Force Bearing Assembly
Patent: 8,926,281 →
Application: 13/401,203 →
Publication: US 2013/0216384
System and Method of Manufacturing a Composite Structure in a Closed Cavity Mold
Patent: 9,381,679 →
Application: 13/404,111 →
Publication: US 2013/0221580
Dual Frequency Damper for an Aircraft
Patent: 8,622,375 →
Application: 13/421,991 →
Publication: US 2013/0241124
Rotor Blade De-Icing System
Patent: 9,056,684 →
Application: 13/422,599 →
Publication: US 2012/0256053
Gearbox with Passive Lubrication System
Patent: 9,458,923 →
Application: 13/426,789 →
Publication: US 2012/0247874
Self Pumping and Priming Adhesive Joint System
Patent: 9,382,933 →
Application: 13/430,117 →
Publication: US 2012/0251225
Device and Method for Repairing Structural Components
Patent: 8,808,823 →
Application: 13/437,665 →
Publication: US 2012/0189807
Self Tuning Vibration Isolation System
Patent: 8,731,743 →
Application: 13/444,469 →
Publication: US 2013/0274961
Method of Supporting a Structural Box Beam
Patent: 8,632,712 →
Application: 13/447,440 →
Publication: US 2012/0199269
Self Tuning Vibration Absorber
Patent: 9,296,476 →
Application: 13/450,060 →
Publication: US 2013/0282204
Aircraft Rotor with Discrete Flap Hinge
Patent: 9,352,830 →
Application: 13/455,814 →
Publication: US 2013/0287576
Multi-Function Detection Liner for Manufacturing of Composites
Patent: 9,205,605 →
Application: 13/455,855 →
Publication: US 2013/0283920
Hybrid Tape for Robotic Transmission
Patent: 9,457,465 →
Application: 13/460,420 →
Publication: US 2012/0289371
Tooling System and Method for Removing a Damaged or Defective Bushing
Patent: 9,156,149 →
Application: 13/467,118 →
Publication: US 2012/0288338
Takeoff/Landing Touchdown Protection Management System
Patent: 9,354,635 →
Application: 13/488,916 →
Publication: US 2013/0325221
Removable Horizontal Stabilizer for Helicopter
Patent: 8,602,351 →
Application: 13/496,241 →
Publication: US 2012/0168559
Rotor Yoke and Method of Making the Same
Patent: 9,199,731 →
Application: 13/501,594 →
Publication: US 2012/0201683
Mobile Energy Attenuating Seat and Safety Harness for Aircraft
Patent: 8,991,760 →
Application: 13/509,514 →
Publication: US 2012/0223551
Dual-Path Fluid Injection Jet
Patent: 8,869,941 →
Application: 13/509,967 →
Publication: US 2012/0222761
Emergency Subsystem for a Fluid System
Patent: 9,599,212 →
Application: 13/510,234 →
Publication: US 2012/0227820
Apparatus for Improved Vibration Isolation
Patent: 8,888,079 →
Application: 13/511,821 →
Publication: US 2012/0279816
Method of Making Core-Stiffened Structure
Patent: 9,266,313 →
Application: 13/521,367 →
Publication: US 2012/0321835
Apparatus for Attaching a Member to a Core-Stiffened Structure and a Combination Thereof
Patent: 9,175,474 →
Application: 13/521,397 →
Publication: US 2012/0284970
Stall Prevention/Recovery System and Method
Patent: 9,218,002 →
Application: 13/522,993 →
Publication: US 2013/0030607
Variable Stiffness Support
Patent: 8,746,649 →
Application: 13/545,167 →
Publication: US 2013/0001841
Airfoil Shaped Tail Boom
Patent: 8,840,058 →
Application: 13/554,309 →
Publication: US 2012/0280079
System and Method of Augmenting Power in a Rotorcraft
Patent: 8,939,399 →
Application: 13/563,086 →
Publication: US 2014/0034781
Variable Stiffness Liquid Inertia Vibration Eliminator
Patent: 8,684,340 →
Application: 13/576,121 →
Publication: US 2012/0292839
System and Method for Developing Fault Diagnostics and Failure Prognosis of Spline Wear in a Drive System
Patent: 9,354,036 →
Application: 13/576,127 →
Publication: US 2012/0303294
Swashplate-Mounted Permanent Magnet Alternator
Patent: 9,024,505 →
Application: 13/576,575 →
Publication: US 2012/0299428
Method and Apparatus for in-Flight Blade Folding
Patent: 8,998,125 →
Application: 13/576,612 →
Publication: US 2012/0292456
Method and Apparatus for Actively Manipulating Aerodynamic Surfaces
Patent: 8,657,228 →
Application: 13/577,633 →
Publication: US 2012/0305698
Moldable Fly-Away Tool Structure System
Patent: 9,868,233 →
Application: 13/578,059 →
Publication: US 2012/0308768
Composite Rotor Blade Having Weighted Material for Mass Balancing
Patent: 9,487,290 →
Application: 13/578,975 →
Publication: US 2012/0301299
Propulsive Anti-Torque Nozzle System with External Rotating Sleeve for a Rotorcraft
Patent: 8,636,242 →
Application: 13/579,002 →
Publication: US 2012/0318910
Method of Developing Flight Infrastructure in Conjunction with a Sale of an Aircraft
Application: 13/580,341 →
Publication: US 2012/0316979
Anti-Torque Nozzle System with Internal Sleeve Valve for a Rotorcraft
Patent: 8,636,243 →
Application: 13/580,532 →
Publication: US 2012/0318911
Propulsive Anti-Torque Nozzle System with Rotating Thrust Director for a Rotorcraft
Patent: 8,636,244 →
Application: 13/580,577 →
Publication: US 2012/0312916
Method of Making a Composite Article Having an Internal Passageway
Patent: 9,090,042 →
Application: 13/641,290 →
Publication: US 2013/0032286
Power Safety Instrument System
Patent: 9,035,802 →
Application: 13/641,325 →
Publication: US 2013/0120165
Multi-Directional Load Joint System
Patent: 8,985,515 →
Application: 13/641,369 →
Publication: US 2013/0026297
Center Lap Tool Machine for Large Transmission Gears
Patent: 9,079,282 →
Application: 13/641,410 →
Publication: US 2013/0029565
Active Vent and Re-Inflation System for a Crash Attenuation Airbag
Patent: 8,870,115 →
Application: 13/641,426 →
Publication: US 2013/0032665
Helicopter Gearbox Auxiliary Cooling System
Patent: 9,272,777 →
Application: 13/661,269 →
Publication: US 2014/0116654
Passive Cooling of Transmission Using Mast Mounted Heat Pipes
Patent: 8,985,517 →
Application: 13/676,954 →
Publication: US 2014/0116652
Constant-Velocity Drive System for Gimbaled Rotor Hubs
Patent: 8,590,833 →
Application: 13/677,146 →
Publication: US 2013/0156580
Blade-Pitch Control System with Indexing Swashplate
Patent: 9,365,288 →
Application: 13/678,272 →
Publication: US 2014/0133980
Laptop Based Rapid Control Laws Development
Application: 13/685,758 →
Publication: US 2014/0148977
Vacuum Assisted Conformal Shape Setting Device
Patent: 9,930,728 →
Application: 13/695,762 →
Publication: US 2013/0043232
Single Stage Debulk and Cure of a Prepreg Material
Application: 13/696,944 →
Publication: US 2013/0056131
Flight Control Laws for Vertical Flight Path
Patent: 9,304,516 →
Application: 13/696,963 →
Publication: US 2013/0060406
High Efficiency External Airbag for Crash Attenuation
Patent: 9,487,301 →
Application: 13/696,970 →
Publication: US 2013/0062465
Temperature Adaptive Fluid Damping System
Patent: 9,188,190 →
Application: 13/697,029 →
Publication: US 2013/0048127
Reconfigurable Rotor Blade
Patent: 8,876,036 →
Application: 13/698,702 →
Publication: US 2013/0062456
Constant Area Vent for External Crash Attenuation Airbag
Patent: 9,045,222 →
Application: 13/699,758 →
Publication: US 2013/0068883
Pylon Mounting System with Vibration Isolation
Patent: 8,840,062 →
Application: 13/699,769 →
Publication: US 2013/0105621
System and Method for Measuring Wrinkle Depth in a Composite Structure
Application: 13/699,777 →
Publication: US 2013/0088222
Blade-Pitch Control System with Feedback Swashplate
Patent: 9,169,735 →
Application: 13/699,785 →
Publication: US 2013/0136596
Elastomeric Signal Transmission and Motion Amplification
Patent: 9,175,673 →
Application: 13/699,838 →
Publication: US 2013/0216399
System and Method for Detecting Objects in a Fluid System
Patent: 9,255,834 →
Application: 13/699,861 →
Publication: US 2013/0160549
Hydrodynamic Ram Mitigating Fuel Cell Structure
Patent: 8,919,376 →
Application: 13/699,937 →
Publication: US 2013/0206265
Pilot Cyclic Control Margin Display
Patent: 9,216,816 →
Application: 13/699,974 →
Publication: US 2013/0134255
Aft-Loading Aircraft with Twin T-Tail Assembly
Patent: 9,162,748 →
Application: 13/699,998 →
Publication: US 2013/0153708
Skid Landing Gear System
Patent: 8,919,694 →
Application: 13/700,020 →
Publication: US 2013/0112810
Flight Control Laws for Automatic Hover Hold
Patent: 9,162,752 →
Application: 13/703,640 →
Publication: US 2013/0138270
Humidity Control for Abrasive Blasting Systems
Patent: 9,168,635 →
Application: 13/703,644 →
Publication: US 2013/0143470
Dual Series Damper System
Patent: 9,481,455 →
Application: 13/703,650 →
Publication: US 2013/0084183
Airfoil Shaped Tail Boom
Patent: 8,814,078 →
Application: 13/703,667 →
Publication: US 2013/0087653
Adaptive Twist System for a Rotor Blade
Patent: 8,662,843 →
Application: 13/703,766 →
Publication: US 2013/0089422
Self-Aligning Inlet Plenum System for Rotorcraft
Patent: 8,998,130 →
Application: 13/703,785 →
Publication: US 2013/0087663
Flight Control Laws for Full Envelope Banked Turns
Patent: 9,098,090 →
Application: 13/703,800 →
Publication: US 2013/0090788
Method and Apparatus for Actively Manipulating Aerodynamic Surfaces
Patent: 8,657,229 →
Application: 13/703,813 →
Publication: US 2013/0082136
Embedded Conductor Honeycomb Core and Sandwich Panel Incorporating Same
Patent: 9,114,591 →
Application: 13/724,257 →
Publication: US 2013/0122245
Automated Diagnostic Inspection of Mechanical Controls
Patent: 9,227,738 →
Application: 13/731,974 →
Publication: US 2014/0188332
Related Assignments (22)
Other recorded transfers of the patents in this record — the chain of ownership.
Assignment of Assignor's Interest Jan 30, 2012
From: WILLIAMS, DAVID L.
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 027620/0280 →
Assignment of Assignor's Interest Feb 2, 2012
From: ISAAC, MARK L.; ELLIOTT, DAVID A.; ROSS, BRENT C.
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 027640/0417 →
Assignment of Assignor's Interest Feb 14, 2012
From: LAFON, BRIAN D.; CAPWELL, ROBERT G.
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 027701/0137 →
Assignment of Assignor's Interest Mar 1, 2012
From: WIINIKKA, MARK; STAMPS, FRANK B.; SOTTIAUX, DANIEL P.; DAILEY, ZACH
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 027793/0108 →
Assignment of Assignor's Interest Mar 1, 2012
From: STAMPS, FRANK B.; BRYAN, MARSHALL W.; THOMPSON, TERRY K.; BRAZIEL, ORION
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 027793/0118 →
Assignment of Assignor's Interest Mar 17, 2012
From: BISHOP, STEPHEN K.; GREENBERG, ROBERT J.; HENRY, FORREST W.
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 027882/0024 →
Assignment of Assignor's Interest Mar 17, 2012
From: CORRIGAN, JOHN; STAMPS, FRANK B.
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 027882/0022 →
Assignment of Assignor's Interest Mar 17, 2012
From: BOSWORTH, JEFFREY; YUCE, MITHAT; STAMPS, FRANK B.; SMITH, MICHAEL R.
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 027882/0037 →
Assignment of Assignor's Interest Mar 19, 2012
From: MCCOLLOUGH, JAMES M.; AUBERT, ROGER
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 027884/0069 →
Assignment of Assignor's Interest Mar 23, 2012
From: POSTER, SCOTT D.; ELLIOTT, DAVID A.; COPE, GARY A.
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 027916/0308 →
Assignment of Assignor's Interest Mar 27, 2012
From: CHRISTENSEN, KEVIN THOMAS; SHUE, SHYHPYNG JACK; CAUDILL, TROY SHELDON
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 027940/0515 →
Assignment of Assignor's Interest Apr 12, 2012
From: SOTTIAUX, DANIEL P.; STAMPS, FRANK B.
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 028038/0904 →
Assignment of Assignor's Interest Apr 18, 2012
From: DICKMAN, COREY J.; FENNY, CARLOS A.; SCHULTZ, DAVID P.
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 028068/0932 →
Assignment of Assignor's Interest May 21, 2012
From: STAMPS, FRANK B.; TISDALE, PATRICK R.; YUCE, MITHAT
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 028244/0009 →
Assignment of Assignor's Interest Jun 15, 2012
From: COVINGTON, CHARLES ERIC; YUCE, MITHAT; POPELKA, DAVID A.; STAMPS, FRANK B.
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 028388/0033 →
Assignment of Assignor's Interest Sep 9, 2012
From: LEE, WEI-YUEH; OLDROYD, PAUL
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 028922/0167 →
Assignment of Assignor's Interest Oct 31, 2012
From: BELL HELICOPTER TEXTRON INC.
To: TEXTRON INNOVATIONS INC.
Reel/Frame 029220/0745 →
Assignment of Assignor's Interest Jan 29, 2013
From: WHITWORTH, DENVER; FRENCH, BRIAN; CRIBB, VANCE, III
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 029715/0782 →
Assignment of Assignor's Interest Jan 10, 2014
From: STAMPS, FRANK B.; TISDALE, PATRICK R.; YUCE, MITHAT
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 031943/0279 →
Assignment of Assignor's Interest Dec 16, 2014
From: BELL HELICOPTER TEXTRON INC.
To: TEXTRON INNOVATIONS INC.
Reel/Frame 034521/0296 →
Assignment of Assignor's Interest Dec 16, 2014
From: MCCULLOUGH, RON
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 034521/0036 →
Corrective Assignment to Correct the the Original Assignment Previously Recorded at Reel: 030891 Frame: 0135. Assignor(S) Hereby Confirms the Assignment. Jul 16, 2021
From: BELL HELICOPTER TEXTRON INC.
To: TEXTRON INNOVATIONS INC.
Reel/Frame 056893/0946 →