GB348946A - Improvements in or relating to flying machines - Google Patents

Improvements in or relating to flying machines

Info

Publication number
GB348946A
GB348946A GB20469/30A GB2046930A GB348946A GB 348946 A GB348946 A GB 348946A GB 20469/30 A GB20469/30 A GB 20469/30A GB 2046930 A GB2046930 A GB 2046930A GB 348946 A GB348946 A GB 348946A
Authority
GB
United Kingdom
Prior art keywords
hinged
portions
fuselage
pillars
wings
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
GB20469/30A
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
Priority to GB20469/30A priority Critical patent/GB348946A/en
Publication of GB348946A publication Critical patent/GB348946A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C33/00Ornithopters

Landscapes

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

Abstract

348,946. Glider and ornithopter. SIECK, H. A. F., 24, Princes Avenue, Liverpool. July 5, 1930, No. 20469. [Class 4.] A machine is provided with hinged wing portions pivoted to fixed inner portions projecting from the fuselage, and with means for flapping the hinged portions when required. The hinged portions may be locked in a fixed position for gliding. Two wing portions 8 having a negative incidence at the tips and a positive incidence at the roots are hinged to the ends of stub surfaces 5 braced to the fuselage by struts 6. The portions 8 are hinged at 15 to pairs of convergent rods 14 pivoted to collars 14a on the ends of an axle 16 carrying landing wheels, floats or skis. The axle 16 is carried by pillars 19 passing through roller guides in the fuselage and provided with stops 21, 22 and cushioning springs 25. The pillars 19 can be reciprocated by a treadle hinged to one of them and arranged adjacent to a fixed platform in the fuselage so that the pilot can throw his weight on to one or the other. A clamping device acting on the other pillar 19 may fix the wings in position for gliding. The hinge line of the wings is arranged below the surface so that the edges of the portions 8 abut against the edges of the stub surfaces should the connections to the undercarriage fail. Alternatively a fixed landing carriage may be provided and the rods 14 connected to a separate transverse rod. Additional planes or wings may be secured to the tops of the pillars 19 or to the axle 16 or to both.
GB20469/30A 1930-07-05 1930-07-05 Improvements in or relating to flying machines Expired GB348946A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB20469/30A GB348946A (en) 1930-07-05 1930-07-05 Improvements in or relating to flying machines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB20469/30A GB348946A (en) 1930-07-05 1930-07-05 Improvements in or relating to flying machines

Publications (1)

Publication Number Publication Date
GB348946A true GB348946A (en) 1931-05-21

Family

ID=10146442

Family Applications (1)

Application Number Title Priority Date Filing Date
GB20469/30A Expired GB348946A (en) 1930-07-05 1930-07-05 Improvements in or relating to flying machines

Country Status (1)

Country Link
GB (1) GB348946A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4139171A (en) * 1976-07-16 1979-02-13 Harris Jeremy M Articulated wing ornithopter
CN103482064A (en) * 2013-09-18 2014-01-01 南京航空航天大学 Bionic flapping wing air vehicle
CN104443381A (en) * 2014-12-15 2015-03-25 佛山市神风航空科技有限公司 Small air vehicle with four oscillation wings
CN104494826A (en) * 2014-12-15 2015-04-08 佛山市神风航空科技有限公司 Single-engine rotary horizontal flapping wing air vehicle
CN112977817A (en) * 2021-04-26 2021-06-18 吉林大学 Flapping wing aircraft
US20220153403A1 (en) * 2019-03-20 2022-05-19 The Royal Veterinary College Winged aircraft

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4139171A (en) * 1976-07-16 1979-02-13 Harris Jeremy M Articulated wing ornithopter
CN103482064A (en) * 2013-09-18 2014-01-01 南京航空航天大学 Bionic flapping wing air vehicle
CN104443381A (en) * 2014-12-15 2015-03-25 佛山市神风航空科技有限公司 Small air vehicle with four oscillation wings
CN104494826A (en) * 2014-12-15 2015-04-08 佛山市神风航空科技有限公司 Single-engine rotary horizontal flapping wing air vehicle
CN104494826B (en) * 2014-12-15 2016-06-15 佛山市神风航空科技有限公司 A kind of single-shot rotary flat claps class flapping wing aircraft
US20220153403A1 (en) * 2019-03-20 2022-05-19 The Royal Veterinary College Winged aircraft
CN112977817A (en) * 2021-04-26 2021-06-18 吉林大学 Flapping wing aircraft

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