1–10 von 35 Ergebnissen
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    GEARED TURBOFAN GAS TURBINE ENGINE ARCHITECTURE

    Freier Zugriff
    KUPRATIS DANIEL BERNARD / SCHWARZ FREDERICK M | Europäisches Patentamt | 2015

    Gas turbine engine with fan variable area nozzle for low fan pressure ratio

    Freier Zugriff
    KOHLENBERG GREGORY A / ZAMORA SEAN P / SCHWARZ FREDERICK M | Europäisches Patentamt | 2018

      Gas turbine engine with fan variable area nozzle for low fan pressure ratio

      Freier Zugriff
      KOHLENBERG GREGORY A / ZAMORA SEAN P / SCHWARZ FREDERICK M | Europäisches Patentamt | 2016

    Hybrid compressor bleed air for aircraft use

    Freier Zugriff
    SCHWARZ FREDERICK M / PIXTON STEPHEN G | Europäisches Patentamt | 2019

      HYBRID COMPRESSOR BLEED AIR FOR AIRCRAFT USE

      Freier Zugriff
      SCHWARZ FREDERICK M / PIXTON STEPHEN G | Europäisches Patentamt | 2016

    GEARED TURBOFAN GAS TURBINE ENGINE ARCHITECTURE

    Freier Zugriff
    HOUSTON DAVID P / KUPRATIS DANIEL BERNARD / SCHWARZ FREDERICK M | Europäisches Patentamt | 2017

      GEARED TURBOFAN GAS TURBINE ENGINE ARCHITECTURE

      Freier Zugriff
      HOUSTON DAVID P / KUPRATIS DANIEL BERNARD / SCHWARZ FREDERICK M | Europäisches Patentamt | 2016

    COMPRESSOR AREA SPLITS FOR GEARED TURBOFAN

    Freier Zugriff
    SCHWARZ FREDERICK M / SPIESMAN PAUL H | Europäisches Patentamt | 2016

    Geared turbofan engine with low pressure environmental control system for aircraft

    Freier Zugriff
    SCHWARZ FREDERICK M / SUCIU GABRIEL L | Europäisches Patentamt | 2020

      GEARED TURBOFAN ENGINE WITH LOW PRESSURE ENVIRONMENTAL CONTROL SYSTEM FOR AIRCRAFT

      Freier Zugriff
      SCHWARZ FREDERICK M / SUCIU GABRIEL L | Europäisches Patentamt | 2016

    NON-CONTACT SEAL ASSEMBLY FOR ROTATIONAL EQUIPMENT WITH LINKAGE BETWEEN ADJACENT ROTORS

    Freier Zugriff
    SCHWARZ FREDERICK M / ACKERMANN WILLIAM K | Europäisches Patentamt | 2017

      Non-contact seal assembly for rotational equipment with linkage between adjacent rotors

      Freier Zugriff
      SCHWARZ FREDERICK M / ACKERMANN WILLIAM K | Europäisches Patentamt | 2020

    ENGINE BLEED SYSTEM WITH MOTORIZED COMPRESSOR

    Freier Zugriff
    SCHWARZ FREDERICK M | Europäisches Patentamt | 2017

    MULTI-ENGINE COORDINATION DURING GAS TURBINE ENGINE MOTORING

    Freier Zugriff
    CHOWDHURY SUBHRADEEP / BOSTWICK DAVID M / GELWAN DAVID et al. | Europäisches Patentamt | 2018

      MULTI-ENGINE COORDINATION DURING GAS TURBINE ENGINE MOTORING

      Freier Zugriff
      CHOWDHURY SUBHRADEEP / BOSTWICK DAVID M / GELWAN DAVID et al. | Europäisches Patentamt | 2021

      Multi-engine coordination during gas turbine engine motoring

      Freier Zugriff
      CHOWDHURY SUBHRADEEP / BOSTWICK DAVID M / GELWAN DAVID et al. | Europäisches Patentamt | 2023

      Multi-engine coordination during gas turbine engine motoring

      Freier Zugriff
      CHOWDHURY SUBHRADEEP / BOSTWICK DAVID M / GELWAN DAVID et al. | Europäisches Patentamt | 2021

    HIGH COMPRESSOR BUILD CLEARANCE REDUCTION

    Freier Zugriff
    VIRTUE JR JOHN P / SAFTLER RISHON / SCHWARZ FREDERICK M | Europäisches Patentamt | 2018

      High compressor build clearance reduction

      Freier Zugriff
      VIRTUE JR JOHN P / SAFTLER RISHON / SCHWARZ FREDERICK M | Europäisches Patentamt | 2019