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The Award database is continually updated throughout the year. As a result, data for FY19 is not expected to be complete until April, 2020.

  1. Compliant Brush Shroud Casing Development for Aircraft Engine Compressors

    SBC: ADVANCED COMPONENTS & MATERIALS, INC.            Topic: N/A

    The proposed Phase II program will optimize the design and manufacturing process of a compliant brush shroud casing. Recent tests at Wright Laboratories with staged brush seals have demonstrated significantly increased blade to shroud rub tolerance of acompliant casing. Phase I of the program is expected to demonstrate the feasibility of two innovative brush shroud designs with lower cost and we ...

    SBIR Phase I 2001 Department of DefenseAir Force
  2. Compliant Brush Shroud Casing Development for Aircraft Engine Compressors

    SBC: ADVANCED COMPONENTS & MATERIALS, INC.            Topic: N/A

    The proposed Phase II program will optimize the design and manufacturing process of a compliant brush shroud casing. Recent tests at Wright Laboratories with staged brush seals have demonstrated significantly increased blade to shroud rub tolerance of acompliant casing. Phase I of the program is expected to demonstrate the feasibility of two innovative brush shroud designs with lower cost and we ...

    SBIR Phase II 2001 Department of DefenseAir Force
  3. Advanced Materials and Cooling Schemes for Rocket Engine Combustion Chambers

    SBC: SIERRA ENGINEERING, INC.            Topic: N/A

    We will produce and test a flight-type transpiration cooled combustion chamber for high performance, reusable, liquid rocket engines utilizing a novel uniform pore material. The Sierra Engineering design produces a durable, low cost, flight-weighttranspiration cooled liner with integral fluid distribution and structural support hardware. The design will be based upon the rigorous analysis proced ...

    SBIR Phase I 2001 Department of DefenseAir Force
  4. Advanced Materials and Cooling Schemes for Rocket Engine Combustion Chambers

    SBC: SIERRA ENGINEERING, INC.            Topic: N/A

    We will produce and test a flight-type transpiration cooled combustion chamber for high performance, reusable, liquid rocket engines utilizing a novel uniform pore material. The Sierra Engineering design produces a durable, low cost, flight-weighttranspiration cooled liner with integral fluid distribution and structural support hardware. The design will be based upon the rigorous analysis proced ...

    SBIR Phase II 2001 Department of DefenseAir Force

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