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N&R ENGNERING MGT SUPPORT SVCS

Company Information
Address
6659 PEARL RD STE 201
CLEVELAND, OH 44130-3821
United States


http://www.nrengineering.com

Information

UEI: L3UNFWGGDL84

# of Employees: 6


Ownership Information

HUBZone Owned: No

Socially and Economically Disadvantaged: Yes

Woman Owned: No



Award Charts




Award Listing

  1. Probabilistic/Reliability Software Tool for Ceramic Matrix Composite/Environmental Barrier Coating Interface Modeling

    Amount: $728,911.00

    One potential way to achieve N+3 goals is the introduction of ceramic matrix composite (CMC) materials into turbine engines. The introduction of CMC vanes and/or blades into turbine engines leads to g ...

    SBIRPhase II2020National Aeronautics and Space Administration
  2. Approaches to Facilitate Using HPT SiC/SiC CMC Vanes and Rotor Blades

    Amount: $121,041.00

    The work will evaluate the benefit of cooling compressor discharge air. T3 air, for use in cooling High Pressure Turbine(HPT) first stage vane and blades for future high OPR and high power density air ...

    SBIRPhase I2020National Aeronautics and Space Administration
  3. Probabilistic/Reliability Software Tool for Ceramic Matrix Composite/Environmental Barrier Coating Interface Modeling

    Amount: $124,322.00

    One potential way to achieve N+3 goals is the introduction of ceramic matrix composite (CMC) materials into turbine engines. The introduction of CMC vanes and/or blades into turbine engines lead to ga ...

    SBIRPhase I2019National Aeronautics and Space Administration
  4. Design Concepts for Low Aspect Ratio High Pressure Turbines for High Bypass Ratio Turbofans

    Amount: $741,544.00

    The performance gains and weight reductions from using Ceramic Matrix Composite(CMC) turbine blades in both the High Pressure Turbine(HPT) and Low Pressure Turbine(LPT) will be determined. Shroudin ...

    SBIRPhase II2017National Aeronautics and Space Administration
  5. Hybrid Disk Fabrication by Linear Friction Welding

    Amount: $148,143.00

    The objective of this proposed Phase I effort is to expand upon the earlier successes with LFW as the bonding method between PM and SX alloys. The early work established feasibility of the LFW proces ...

    SBIRPhase I2017Department of Defense Air Force
  6. Fan Duct Heat Exchanger for Turbine Cooling Air

    Amount: $123,954.00

    The proposal is for the design of a fan duct heat exchanger in order to improve aircraft fuel burn. The fan duct heat exchanger decreases the temperature of the 15% to 20% of compressor discharge air ...

    SBIRPhase I2016National Aeronautics and Space Administration
  7. Design Concepts for Low Aspect Ratio High Pressure Turbines for High Bypass Ratio Turbofans

    Amount: $123,837.00

    The proposal is to identify cycle improvements and verify structural feasibility of shrouding a low aspect ratio High Pressure Turbine(HPT) rotor designed to use ceramic blades. When the clearance-to- ...

    SBIRPhase I2016National Aeronautics and Space Administration
  8. Uncertainty Propagation to Modal Parameters and Metrics

    Amount: $748,872.00

    This program implements a Bayesian framework for uncertainty quantification of material parameters needed for life prediction of polymer matrix composite (PMC) bolted joints. Accurate estimations of f ...

    SBIRPhase II2016Department of Defense Air Force
  9. Uncertainty Quantification of Test Derived Model Parameters for Life Prediction of Composite Bolted Joints in an ICME Framework

    Amount: $148,553.00

    ABSTRACT:This program implements a Bayesian framework for uncertainty quantification of material parameters needed for life prediction of polymer matrix composite (PMC) bolted joints. Accurate estimat ...

    SBIRPhase I2015Department of Defense Air Force
  10. Physics-based MDAO tool for CMC blades and vanes conceptual design

    Amount: $122,648.00

    The proposed work will develop a reliability analysis tool consistent with conceptual-level design for ceramic matrix composite (CMC) turbine blades and vanes. The analysis software will comprise a su ...

    SBIRPhase I2015National Aeronautics and Space Administration
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