GB299274A - Improvements in or relating to planes for aircraft - Google Patents

Improvements in or relating to planes for aircraft

Info

Publication number
GB299274A
GB299274A GB1368928A GB1368928A GB299274A GB 299274 A GB299274 A GB 299274A GB 1368928 A GB1368928 A GB 1368928A GB 1368928 A GB1368928 A GB 1368928A GB 299274 A GB299274 A GB 299274A
Authority
GB
United Kingdom
Prior art keywords
gear
shaft
drums
plane
secured
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
GB1368928A
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 GB1368928A priority Critical patent/GB299274A/en
Publication of GB299274A publication Critical patent/GB299274A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/14Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/14Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B64C9/18Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)

Abstract

299,274. Fowler, H. D. May 9, 1928. Planes, construction of; steering and balancing.-An aircraft plane comprises a cambered main portion, a trailing portion of smaller cross-section and an auxiliary surface adapted to be housed beneath the trailing portion and to be projected rearwardly and downwardly to vary the area and camber of the plane. Mechanism is provided for projecting and retracting end sections of the auxiliary surface in opposite directions when required to facilitate control. The main portion of the plane has front and rear spars 16, 17 connected by pressure ribs 18 and prevented from tilting by bracing 23. The under surface of the trailing portion is offset from the main under surface to accommodate auxiliary planes 28 carried by trolleys 29 running on curved rails 24 secured by brackets 25 to the rear spar 17. The rails 24 project through slots in the trailing portion. The trolleys are moved by endless cables 34 passed around pulleys 34 on the rails 24 and secured to drums on a vertical shaft 37 moved by a handle 33 in the central section of the plane. The cables leading to the two outer sections are secured to drums 36<a>, 36<b>, on a shaft 37a and sleeve 49, Fig. 11, and that from the central section is secured to a drum 36 on a sleeve 47 surrounding the shaft 37<a> and suspended from a bearing 48. The sleeve 49 has a gear 50 in mesh with a gear 71 on a shaft 69 which has a gear 68 meshing with a gear 67 on a third shaft 65. The gear 67 is in mesh also with a gear 63 splined to the shaft 37a when the parts are in the position shown. Movement of the handle 38 when the parts are in this position causes opposite rotations of the two drums 36<a>, 36<b> while the drum 36 remains stationary. By moving a lever 55, cams 54 on shafts 52, 56 cause a plate 60 to be raised to move the gear 63 out of mesh with the gear 67, and by raising the sleeve 49 and shaft 37<a> cause all three drums to be clutched together. Movement of the handle 38 under these circumstances causes all three drums to be moved together to vary the camber and area of the plane as a whole.
GB1368928A 1928-05-09 1928-05-09 Improvements in or relating to planes for aircraft Expired GB299274A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1368928A GB299274A (en) 1928-05-09 1928-05-09 Improvements in or relating to planes for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1368928A GB299274A (en) 1928-05-09 1928-05-09 Improvements in or relating to planes for aircraft

Publications (1)

Publication Number Publication Date
GB299274A true GB299274A (en) 1928-10-25

Family

ID=10027609

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1368928A Expired GB299274A (en) 1928-05-09 1928-05-09 Improvements in or relating to planes for aircraft

Country Status (1)

Country Link
GB (1) GB299274A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0414531A2 (en) * 1989-08-23 1991-02-27 British Aerospace Public Limited Company Self locking end stops for aircraft control surfaces

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0414531A2 (en) * 1989-08-23 1991-02-27 British Aerospace Public Limited Company Self locking end stops for aircraft control surfaces
EP0414531A3 (en) * 1989-08-23 1991-04-10 British Aerospace Plc Self locking end stops for aircraft control surfaces

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