THIS DOCUMENT HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE 5-YEAR REVIEW POLICY. NOTES: (a) INCLUDING THE MAX ENGINE SHAFT ECCENTRICITY AND MISALIGNMENT SPECIFIED HEREIN, AND UNDER THE CONDITIONS OF MAXIMUM PROPELLER DESIGN LOADING, THE FORCES EXERTED BY THE PROPELLER SPLINES ON THE ENGINE DRIVE SPLINES SHALL NOT EXCEED A SIDE LOAD OF 6000 POUNDS, A FORE AND AFT THRUST OF 1500 POUNDS, AND A MOMENT OF L. FOR NORMAL CONTINUOUS OPERATION THE FORCES SHALL NOT EXCEED 45% OF THESE SPECIFIED DESIGN VALUES. (b) MAX BOLT DEPTH J INDICATES AMOUNT OF MIN REMOVAL SPACE TO BE ALLOWED IN PROP MFR PARTS FOR THE ATTACHMENT BOLT. PROP MFR SHALL REFER TO ENG MFR INSTALLATION DWG WHICH SHALL SHOW MAX AND MIN REQUIRED DEPTH OF INSTALLED BOLT. (c) PROP MFR SHALL REFER TO ENG MFR ENGINE INSTALLATION DWG WHICH SHALL SHOW MAX DEPTH TO FIRST FULL UNINTERRUPTED THD AND MIN DEPTH TO LAST FULL UNINTERRUPTED THD AVAILABLE FOR BOLT ENGAGEMENT. (d) MAX END PLAY .050 (THIS LIMIT IS INCLUDED IN THE TOLERANCE)


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    PROPELLER ATTACHMENT-NOSE MOUNTED


    Erscheinungsdatum :

    2006-07-27



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    PROPELLER ATTACHMENT - NOSE MOUNTED

    SAE Technical Papers | 2013


    PROPELLER ATTACHMENT--NOSE MOUNTED

    SAE Technical Papers | 1953


    Aerodynamic Interaction and Analysis of Nose-Mounted Propeller Aircraft

    Anand, Apurva / MV, Shesha Sai / V, Chandrasekaran et al. | AIAA | 2023


    Aerodynamic Interaction and Analysis of Nose-Mounted Propeller Aircraft

    Anand, Apurva / Sai, M. V. Shesha / Chandrasekaran, V. et al. | TIBKAT | 2023


    PROPELLER ATTACHMENT DEVICE AND PROPELLER ATTACHMENT METHOD

    MAKII TATSUO | Europäisches Patentamt | 2021

    Freier Zugriff