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PROPULSIVE WING, LLC

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Company Details

Name: PROPULSIVE WING, LLC
Jurisdiction: New York
Legal type: DOMESTIC LIMITED LIABILITY COMPANY
Status: Active
Date of registration: 30 Dec 2005 (19 years ago)
Entity Number: 3298940
ZIP code: 13066
County: Onondaga
Place of Formation: New York
Address: 105 CHURCHILL LANE, FAYETTEVILLE, NY, United States, 13066

DOS Process Agent

Name Role Address
C/O JOSEPH KUMMER DOS Process Agent 105 CHURCHILL LANE, FAYETTEVILLE, NY, United States, 13066

Agent

Name Role Address
JOSEPH KUMMER Agent 105 CHURCHILL LANE, FAYETTEVILLE, NY, 13066

Filings

Filing Number Date Filed Type Effective Date
140303002167 2014-03-03 BIENNIAL STATEMENT 2013-12-01
120113003054 2012-01-13 BIENNIAL STATEMENT 2011-12-01
100128002562 2010-01-28 BIENNIAL STATEMENT 2009-12-01
071203002448 2007-12-03 BIENNIAL STATEMENT 2007-12-01
060303000910 2006-03-03 AFFIDAVIT OF PUBLICATION 2006-03-03

USAspending Awards / Contracts

Procurement Instrument Identifier:
NNX11CD95P
Award Or Idv Flag:
AWARD
Award Type:
PO
Action Obligation:
0.00
Base And Exercised Options Value:
0.00
Base And All Options Value:
0.00
Awarding Agency Name:
National Aeronautics and Space Administration
Performance Start Date:
2011-07-21
Description:
THE CHALLENGES OF THE NEXT CENTURY OF AVIATION WILL REQUIRE INNOVATIVE AND REVOLUTIONARY CONCEPTS TO MEET AIR TRANSPORTATION DEMANDS. ONE NASA VISION FOR FUTURE TRANSPORT-SIZED AIRCRAFT INCLUDES THE BLENDED-WING-BODY (BWB) PLATFORM WITH EMBEDDED, DISTRIBUTED PROPULSION AS A MEANS FOR INCREASED EFFICIENCY AND REDUCED NOISE. IN CRUISE, EMBEDDED PROPULSION BENEFITS FROM BOUNDARY LAYER INGESTION AND WAKE FILLING, RESULTING IN HIGH PROPULSIVE EFFICIENCY. HOWEVER, SEVERAL CHALLENGES EXIST, INCLUDING INLET NOZZLE DESIGN, PROPULSOR DESIGN FOR INGESTION OF HIGHLY NON-UNIFORM INFLOW, AND PROPULSOR/AIRFRAME SUPPORT STRUCTURE OPTIMIZATION. THIS WORK PROPOSES A HYBRID TURBOELECTRIC PROPULSION SYSTEM INCORPORATING SMALL EMBEDDED, DISTRIBUTED CROSS-FLOW FANS (CFF) FOR BOUNDARY LAYER CONTROL AND WAKE FILLING, AND MUCH LARGER AXIAL FANS FOR PRIMARY THRUST. BRINGING TOGETHER THE BEST QUALITIES OF BOTH AXIAL AND CFF PROPULSION, A SUBSTANTIAL IMPROVEMENT IN OVERALL VEHICLE EFFICIENCY IS POSSIBLE. CFD AND ANALYTICAL ANALYSES WILL BE USED TO INVESTIGATE THE FLOW FIELD AND RANGE OF APPLICATION FOR SUCH A SYSTEM. COMPARISONS WILL BE MADE WITH PUBLISHED BASELINE DESIGNS WITH RESPECT TO POWER REQUIREMENTS, COMPONENT WEIGHTS, SUPPORT STRUCTURE, AND OTHER KEY PARAMETERS.
Naics Code:
541712: RESEARCH AND DEVELOPMENT IN THE PHYSICAL, ENGINEERING, AND LIFE SCIENCES (EXCEPT BIOTECHNOLOGY)
Product Or Service Code:
AR11: R&D-AERO & SPACE TECH-B RES

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Date of last update: 29 Mar 2025

Sources: New York Secretary of State