GB286516A - Improvements in aeroplane flying machines - Google Patents

Improvements in aeroplane flying machines

Info

Publication number
GB286516A
GB286516A GB1347627A GB1347627A GB286516A GB 286516 A GB286516 A GB 286516A GB 1347627 A GB1347627 A GB 1347627A GB 1347627 A GB1347627 A GB 1347627A GB 286516 A GB286516 A GB 286516A
Authority
GB
United Kingdom
Prior art keywords
wings
edges
central
shows
rearward
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
GB1347627A
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.)
JOHANN ANTON SANDERS
Original Assignee
JOHANN ANTON SANDERS
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 JOHANN ANTON SANDERS filed Critical JOHANN ANTON SANDERS
Priority to GB1347627A priority Critical patent/GB286516A/en
Publication of GB286516A publication Critical patent/GB286516A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B64C3/14—Aerofoil profile

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

286,516. Sanders, J. A. May 19, 1927. Plßnes, construction of; steering and balancing. -An aeroplane has the main dimensions of its wrings in the direction of flight, the leading edges converging forwardly at an acute angle to one another and being bent upwards or constructed of an increased thickness or both. Fig. 1 shows in full and dotted lines several alternative plan 'forms of the wings, the upper surface being con. tinuous with the upper surface of the fuselage. Other alternatives are referred to in which the front edge of the combined wings has a central rearward indentation and the rear edge a rearward central projection. Fig. 7<A> shows the arrangement of two elevators 5 and two ailerons 4 in the rear edges of the wings. When a thin wing is used the central portions may be set at a dihedral angle and the edges at a greater dihedral angle.
GB1347627A 1927-05-19 1927-05-19 Improvements in aeroplane flying machines Expired GB286516A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1347627A GB286516A (en) 1927-05-19 1927-05-19 Improvements in aeroplane flying machines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1347627A GB286516A (en) 1927-05-19 1927-05-19 Improvements in aeroplane flying machines

Publications (1)

Publication Number Publication Date
GB286516A true GB286516A (en) 1928-03-08

Family

ID=10023650

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1347627A Expired GB286516A (en) 1927-05-19 1927-05-19 Improvements in aeroplane flying machines

Country Status (1)

Country Link
GB (1) GB286516A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2575185A (en) * 1950-02-24 1951-11-13 Republic Aviat Corp Airfoil

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2575185A (en) * 1950-02-24 1951-11-13 Republic Aviat Corp Airfoil

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