Inertial acceleration aircraft

Aeronautics and astronautics – Aircraft – heavier-than-air – Airplane and helicopter sustained

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

244 34A, 244 1711, B64C 2700, B64C 3906

Patent

active

058396900

ABSTRACT:
An aircraft structured particularly, as a whole to improve its capacity for accelerating by the means of transforming stored motion of mass into translocational motion of the aircraft; the aircraft is structured particularly, as a whole, to improve its capacities for storing motion of mass and for transforming stored motion of mass into translocational motion of itself; motion preferrably in stored as orbital motion of the aircraft's parts; the stored orbital motion preferrably is transformed by aerodynamic action into translocational motion of the aircraft; the means for storing orbital motion preferrably consists of a rotor, within the periphery of which are situated the aircraft's sustaining, propelling, motion transformation, fuel containment, and landing means; situated within said appended to a generally nonrotating fuselage are, respectively, a pilot area and a means for controlling the source of translocational flight; the preferred motion transforming means comprises a plurality of rotor blades, each of which has a longitudinal axis aligned generally with a radius of the rotor axis and of which is tiltable about a longitudinal axis, and effects the transformation with an appropriate rate collective alteration of the blade lateral axes from coincident with the blade orbital planer to the perpendiculars thereto, which alternation aerodynamically transforms the rotation of the rotor into axial motion thereof; the spin axes of the spinning mechanisms of the propulsion means parallel the rotor axis; appended to each propulsion means is a thrust redirecting means which enables the former to propel the rotor both rotationally and axially.

REFERENCES:
patent: 828867 (1906-08-01), Stoltenberg
patent: 2328786 (1943-09-01), Crowder
patent: 2479125 (1949-08-01), Leonard
patent: 2633922 (1953-04-01), Svenson
patent: 2807428 (1957-09-01), Wibault
patent: 2823875 (1958-02-01), Peterson
patent: 2866608 (1958-12-01), Leonard
patent: 2874920 (1959-02-01), Mallinckrodt
patent: 2918229 (1959-12-01), Lippisch
patent: 2941600 (1960-06-01), Koning et al.
patent: 3251421 (1966-05-01), Bracey
patent: 3356315 (1967-12-01), Kolodziej
patent: 3514053 (1970-05-01), McGuinness
patent: 3838835 (1974-10-01), Kling
patent: 3946970 (1976-03-01), Blankenship
patent: 4195800 (1980-04-01), Wallace
patent: 4433819 (1984-02-01), Carrington

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Inertial acceleration aircraft does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Inertial acceleration aircraft, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Inertial acceleration aircraft will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1695438

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.