Design Of The Low Vibration Turboprop Powerplant Suspension System for The DASH 7 Aircraft

830755

02/01/1983

Event
Business Aircraft Meeting and Exposition
Authors Abstract
Content
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.
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DOI
https://doi.org/10.4271/830755
Pages
16
Citation
Hrycko, G., "Design Of The Low Vibration Turboprop Powerplant Suspension System for The DASH 7 Aircraft," SAE Technical Paper 830755, 1983, https://doi.org/10.4271/830755.
Additional Details
Publisher
Published
Feb 1, 1983
Product Code
830755
Content Type
Technical Paper
Language
English