GB749436A - Improvements relating to aircraft - Google Patents

Improvements relating to aircraft

Info

Publication number
GB749436A
GB749436A GB13175/52A GB1317552A GB749436A GB 749436 A GB749436 A GB 749436A GB 13175/52 A GB13175/52 A GB 13175/52A GB 1317552 A GB1317552 A GB 1317552A GB 749436 A GB749436 A GB 749436A
Authority
GB
United Kingdom
Prior art keywords
wings
fuselage
shafts
aircraft
axes
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
GB13175/52A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB749436A publication Critical patent/GB749436A/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
    • B64C39/003—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage
    • B64C39/005—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage about a horizontal transversal axis

Landscapes

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

Abstract

749,436. Rotating wing aircraft. ORAZI, P. May 23, 1952 [May 24, 1951], No. 13175/52. Class 4. An aircraft comprises a fuselage and substantially plane wings mounted on opposite sides of said fuselage for rotation about spanwise axes, said wings having at least one operative configuration wherein said axes are disposed with respect to each other at an angle of less than 180 degrees. In the embodiment shown the wings b are mounted on shafts c<SP>1</SP> mounted at dihedral angles on the fuselage R, the shafts being connected by a universal joint K. In conjunction with or alternative to the provision of dihedral angles, the wings may be arranged in swept-back positions. A differential gear may be used to connect the shafts instead of the joint K whereby a control effect may be achieved by differential rotation of the wings.
GB13175/52A 1951-05-24 1952-05-23 Improvements relating to aircraft Expired GB749436A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US749436XA 1951-05-24 1951-05-24

Publications (1)

Publication Number Publication Date
GB749436A true GB749436A (en) 1956-05-23

Family

ID=22122578

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13175/52A Expired GB749436A (en) 1951-05-24 1952-05-23 Improvements relating to aircraft

Country Status (1)

Country Link
GB (1) GB749436A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009109918A3 (en) * 2008-03-04 2010-03-18 Philip Bogrash Cycloidal rotor with non-circular blade orbit

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009109918A3 (en) * 2008-03-04 2010-03-18 Philip Bogrash Cycloidal rotor with non-circular blade orbit

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