GB262489A - Improvements in or relating to flying machines - Google Patents

Improvements in or relating to flying machines

Info

Publication number
GB262489A
GB262489A GB20197/25A GB2019725A GB262489A GB 262489 A GB262489 A GB 262489A GB 20197/25 A GB20197/25 A GB 20197/25A GB 2019725 A GB2019725 A GB 2019725A GB 262489 A GB262489 A GB 262489A
Authority
GB
United Kingdom
Prior art keywords
rudders
thrust
propellers
steering
fixed
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
GB20197/25A
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 GB20197/25A priority Critical patent/GB262489A/en
Publication of GB262489A publication Critical patent/GB262489A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Motorcycle And Bicycle Frame (AREA)

Abstract

262,489. Sihorshy, I. I. Aug. 11, 1925. Planes, arrangement of; steering.-Aircraft having engines and propellers on opposite sides of the centre line are provided with fixed or movable surfaces in the slip streams from the propellers, each surface being so inclined or shaped, or both as normally to counteract the moment of the thrust of the corresponding propeller or. the machine, thereby compensating for any asymmetrical thrust. Fig. 1 shows two rudders 15, 16 arranged in the slip streams from the propelling units 9, 10, each rudder having its convex portion towards the fuselage, and also inclined, to give a lateral thrust towards the tail of the machine. For steering purposes, the rudders are connected together by a cord 18 and are operated by two pedals 21, 22. Instead of the rudders 15, 16 inclined symmetrical surfaces, or cambered surfaces set parallel to the line of flight may be used, or, as shown in Fig. 6, rudders 30 may be mounted behind fixed inclined surfaces 31. Fig. 7 shows another modification in which fixed surfaces 34, both cambered and inclined, are used to com pensate for asymmetrical thrust, a separate rudder 35 being provided for steering. Such surfaces may be provided also where propellers are disposed above and below the centre line.
GB20197/25A 1925-08-11 1925-08-11 Improvements in or relating to flying machines Expired GB262489A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB20197/25A GB262489A (en) 1925-08-11 1925-08-11 Improvements in or relating to flying machines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB20197/25A GB262489A (en) 1925-08-11 1925-08-11 Improvements in or relating to flying machines

Publications (1)

Publication Number Publication Date
GB262489A true GB262489A (en) 1926-12-13

Family

ID=10142009

Family Applications (1)

Application Number Title Priority Date Filing Date
GB20197/25A Expired GB262489A (en) 1925-08-11 1925-08-11 Improvements in or relating to flying machines

Country Status (1)

Country Link
GB (1) GB262489A (en)

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