Tandem-engine aircraft propulsion module
OwnerCarl J. Hermachinventor
Life of this patent
Estimating the term…
Abstract
Tandem-engine aircraft propulsion module attachable to an aircraft fuselage and/or to the aircraft wings directly. This propulsion module contains fore-and-aft in-line engines and an intermediate fuel compartment. A subhousing of this module has engine instrumentation and controls placed for overhead introduction into an underlying aircraft fuselage cabin when the module is secured on top thereof. Propulsion modules of this invention are readily removable and replaceable for ease of inspection and maintenance, and if like-sized are mutually interchangeable. These modules are inherently economical and enable cost-effective fuselage and dry-wing construction. They also enhance flight safety, not only in comparison with single-engine aircraft but also especially as compared with off-axial twin-engine aircraft.
Claims4
Tandem-engine propulsion module, comprising
- a housing with only two engines, respectively fore-and-aft in the housing, a fuel compartment centered fore-and-aft in the housing, and engine instruments and controls;
- adapted to be installed as the only propulsion means for a fixed-wing aircraft having fuselage means extending fore-and-aft, including a forward cabin portion for a flight crew, with the engine instruments and controls accessible to the flight crew.
Powered dry-wing aircraft,
- comprising, in combination,
- boatlike fuselage means extending fore and aft along and about a substantially horizontal centerline;
- wing means extending substantially horizontally and laterally outboard relative to the fuselage means, and secured thereto;
- outboard stabilization means depending from the wing means and flanking the fuselage means;
- and
- a tandem-engine propulsion module in part contiguous with and detachably secured to at least one of the foregoing means,
- the propulsion module being adapted to rotate a tractor propeller and a pusher propeller located respectively forward and aft of the leading and trailing edges of the wing means.
Method of powering a fixed-wing aircraft provided with enclosed fuselage means extending fore-and-aft including a crew cabin and having single-wing means extending outboard therefrom in opposite lateral directions,
- comprising the steps of
- providing a propulsion module detachably attachable to the fuselage means proximate to inboard portions of the wing means and adapted to carry forward and aft engine means;
- providing an engine fuel compartment in the propulsion module, centering the engine fuel compartment in plan laterally relative to the fuselage means and fore-and-aft relative to the wing means;
- and
- detachably attaching the propulsion module in substantial contiguity to an upper portion of the fuselage means.
Dependencies are inferred from the claim text.