← Back to Patent Explorer
US3285537A Expired / Lapsed US ⏱️ 0.0 years remaining

Vertical take off and landing aircraft

Assignee: De Havilland Aircraft of Canada Ltd
•
Filing: 1966-03-22
•
Granted: 1966-11-15
•
Expires: 1986-03-22
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

No abstract record available.

Inventors

  • 👤 Whittley Donald Charles

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-02 02:54
CPC Classifications
B; B64; B64C; B64C29/00; B64C29/0008; B64C29/0041; B64C29/005

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 113 words
A VERTICAL TAKE OFF AND LANDING AIRCRAFT COMPRISING: A FUSELAGE; WING STRUCTURE ADAPTED TO SUSTAIN SAID FUSELAGE IN FLIGHT AT A FORWARD CRUISING SPEED; A FIRST JET ENGINE AND A REARWARDLY EXTENDING JET TUBE IN SAID FUSELAGE ADAPTED TO PROPEL SAID AIRCRAFT AT CRUISING SPEED; AT LEAST ONE OTHER JET ENGINE IN SAID FUSELAGE; TWO SIDE PLENUMS EXTENDING LONGITUDINALLY IN THE LOWER FORWARD REGIONS AT LEAST OF SAID FUSELAGE AND EACH HAVING A LONGITUDINAL SLOT FOR THE TANGENTIALLY DOWNWARD ESCAPE OF GASES THEREFROM OVER UNDER SURFACES OF SAID FUSELAGE; MEANS CONNECTING SAID OTHER ENGINE TO SAID PLENUMS AND RETRACTABLE SHROUD FLAP MEANS FOR EACH PLENUM DEFINING WHEN CLOSED THEREWITH SUBSTANTIALLY CONVENTIONAL FUSELAGE CONTOURS
Claim 2
Dependent Claim 113 words
A VERTICAL TAKE OFF AND LANDING AIRCRAFT COMPRISING: A FUSELAGE; WING STRUCTURE ADAPTED TO SUSTAIN SAID FUSELAGE IN FLIGHT AT A FORWARD CRUISING SPEED; A FIRST JET ENGINE AND A REARWARDLY EXTENDING JET TUBE IN SAID FUSELAGE ADAPTED TO PROPEL SAID AIRCRAFT AT CRUISING SPEED; AT LEAST ONE OTHER JET ENGINE IN SAID FUSELAGE; TWO SIDE PLENUMS EXTENDING LONGITUDINALLY IN THE LOWER FORWARD REGIONS AT LEAST OF SAID FUSELAGE AND EACH HAVING A LONGITUDINAL SLOT FOR THE TANGENTIALLY DOWNWARD ESCAPE OF GASES THEREFROM OVER UNDER SURFACES OF SAID FUSELAGE; MEANS CONNECTING SAID OTHER ENGINE TO SAID PLENUMS AND RETRACTABLE SHROUD FLAP MEANS FOR EACH PLENUM DEFINING WHEN CLOSED THEREWITH SUBSTANTIALLY CONVENTIONAL FUSELAGE CONTOURS

References Cited (Backward Citations)

US3124322A Cited
US2918233A Cited
US3148848A Cited
US3117643A Cited
US3073548A Cited
US3053482A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1969-11-14 1970-05-16 1970-11-15 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1973-11-14 1974-05-16 1974-11-15 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1977-11-14 1978-05-16 1978-11-15 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag