IP Library › Assignment 047872/0658
Patent Assignment
Reel/Frame 047872/0658

CONFIRMATORY LICENSE

Recorded: 2018-10-26 Received: 2018-10-26 Pages: 19
Assignor
Assignee
DEPARTMENT OF THE NAVY
47076 LILJENCRANTZ ROAD, BLDG. 435, PATUXENT RIVER, MD, 20670, UNITED STATES
Covered Applications (17)
COOLING PASSAGES FOR GAS TURBINE ENGINE COMPONENT
App. No. 14/949,047
→
GAS TURBINE ENGINE COMPONENT WITH INCREASED COOLING CAPACITY
App. No. 14/923,553
→
AIRFOIL SHOWERHEAD PATTERN APPARATUS AND SYSTEM
App. No. 14/862,422
→
GAS TURBINE ENGINE HIGH LIFT AIRFOIL COOLING IN STAGNATION ZONE
App. No. 14/767,768
→
GAS TURBINE ENGINE COMPONENT HAVING TRANSVERSELY ANGLED IMPINGEMENT RIBS
App. No. 14/759,271
→
GAS TURBINE ENGINE AIRFOIL COOLING PASSAGE CONFIGURATION
App. No. 14/696,627
→
GAS TURBINE ENGINE TURBINE BLADE TIP WITH COATED RECESS
App. No. 14/686,979
→
RIB BUMPER SYSTEM
App. No. 14/670,566
→
BLADES AND BLADE DAMPERS FOR GAS TURBINE ENGINES
App. No. 14/639,490
→
SPLAYED TIP FEATURES FOR GAS TURBINE ENGINE AIRFOIL
App. No. 14/630,814
→
CORE ASSEMBLY INCLUDING STUDDED SPACER
App. No. 14/616,940
→
INTERNAL COOLING CAVITY WITH TRIP STRIPS
App. No. 14/602,035
→
AIRFOIL AND METHOD OF MAKING
App. No. 13/737,200
→
BLADE OUTER AIR SEAL
App. No. 13/597,745
→
GAS TURBINE ENGINE COMPONENT COOLING CIRCUIT
App. No. 13/565,877
→
AIRFOIL COOLING CIRCUITS
App. No. 13/529,143
→
GAS TURBINE ENGINE COMPRESSOR STATOR SEAL
App. No. 13/466,549
→