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Design Of The Low Vibration Turboprop Powerplant Suspension System for The DASH 7 Aircraft The de Havilland Aircraft of Canada, Limited
- Format:
- Conference/Event
- Author/Creator:
- Hrycko, G.O., author.
- Conference Name:
- Business Aircraft Meeting and Exposition (1983-04-12 : Wichita, Kansas, United States)
- Language:
- English
- Physical Description:
- 1 online resource
- Place of Publication:
- Warrendale, PA SAE International 1983
- Summary:
- Larger turboprop aircraft are finding increased acceptance with today's fuel-conscious operators. However, these aircraft must also appeal to the air traveller' who has become accustomed to the vibration free environment of turbojets. This requirement of minimum propeller-induced vibration results in a conflicting constraint for the designer of a flutter free installation.Described in this paper is the two-plane engine mounting scheme used successfully in de Havilland's DASH 7 commuter aircraft. The suspension system meets the design objectives of low transmissibility, adequate whirl flutter margins and minimized landing loads
- Notes:
- Vendor supplied data
- Publisher Number:
- 830755
- Access Restriction:
- Restricted for use by site license
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