GB471946A - Improvements in or relating to aircraft - Google Patents

Improvements in or relating to aircraft

Info

Publication number
GB471946A
GB471946A GB11578/36A GB1157836A GB471946A GB 471946 A GB471946 A GB 471946A GB 11578/36 A GB11578/36 A GB 11578/36A GB 1157836 A GB1157836 A GB 1157836A GB 471946 A GB471946 A GB 471946A
Authority
GB
United Kingdom
Prior art keywords
wing
wings
planes
fuselage
aeroplane
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB11578/36A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
MAURICE HENRI DELANNE
Original Assignee
MAURICE HENRI DELANNE
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by MAURICE HENRI DELANNE filed Critical MAURICE HENRI DELANNE
Publication of GB471946A publication Critical patent/GB471946A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/08—Aircraft not otherwise provided for having multiple wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

471,946. Tandem - wing aeroplane. DELANNE, M. H. April 23, 1936, No. 11578. Convention date, July 4, 1935. [Class 4] An aeroplane having staggered wings 1, 2 includes stabilizing planes 7 mounted on and normal to the rear plane 2 ; the planes 7 are disposed parallel to the axis of the fuselage and carry adjustable control surfaces 9. The fuselage is habitable throughout its length and is provided with a rear cabin and gunner's cockpit. Ailerons 6 are provided on the wings. The wings may be connected by elements 8 and the planes may be disposed in the slipstream from the propellers. Landing gear as described in Specification 471,944 may be provided. The invention may be applied to seaplanes and an additional forward wing may be provided. The rear wing may be above or below the front wing and the cabin may be detachable for parachute descent.
GB11578/36A 1935-07-04 1936-04-23 Improvements in or relating to aircraft Expired GB471946A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR471946X 1935-07-04

Publications (1)

Publication Number Publication Date
GB471946A true GB471946A (en) 1937-09-14

Family

ID=8902647

Family Applications (1)

Application Number Title Priority Date Filing Date
GB11578/36A Expired GB471946A (en) 1935-07-04 1936-04-23 Improvements in or relating to aircraft

Country Status (1)

Country Link
GB (1) GB471946A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2576294A (en) * 1948-06-26 1951-11-27 Alexander D Geraci Airplane sustentation and control surface arrangement
WO2016005954A1 (en) * 2014-07-11 2016-01-14 On-Air Consulting & Solutions S.R.L. Remotely piloted aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2576294A (en) * 1948-06-26 1951-11-27 Alexander D Geraci Airplane sustentation and control surface arrangement
WO2016005954A1 (en) * 2014-07-11 2016-01-14 On-Air Consulting & Solutions S.R.L. Remotely piloted aircraft

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