GB191125040A - Improvements in or relating to Flying Machines. - Google Patents

Improvements in or relating to Flying Machines.

Info

Publication number
GB191125040A
GB191125040A GB191125040DA GB191125040A GB 191125040 A GB191125040 A GB 191125040A GB 191125040D A GB191125040D A GB 191125040DA GB 191125040 A GB191125040 A GB 191125040A
Authority
GB
United Kingdom
Prior art keywords
shaft
rudder
wings
rods
planes
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
Inventor
Josef Barcz
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
Application granted granted Critical
Publication of GB191125040A publication Critical patent/GB191125040A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/42Adjusting about chordwise axes

Abstract

25,040. Bßrcz, J. Nov. 10. Aerial machines without aerostats; planes, arrangement and construction of; propelling; cars.-A flying-machine comprises supporting- planes 2 hinged to the longitudinal sides of a frame 1, flapping-wings 4 hinged to the frames 2, a car 27 supported from a pivot 30 and by chains 28 passing over pulleys 26, and a rudder 20 mounted on a telescopic shaft 13, 14. The planes 2 may be adjusted by means of bands 3, and, during transport on the ground, may be folded down at the sides of the machine. The wings 4 are provided with flaps 6, which are hinged along one edge and closed in at the sides, and are guided on bolts 7, Fig. 4, fitted with springs 8 which ensure the closing of the flaps at the commencement of the down-stroke. The wings are further fitted with hinged portions 9 which are turned somewhat under the wings during the down-stroke, as shown by dotted lines in Fig. 4, by means of crossed rods 10 connected at one end to levers 11 secured to the parts 9, and at the other end to arms 12 fixed to the machine. The wings 4 are reciprocated by eccentric rods 33, which are fitted with blocks 34 sliding in guides 35, and are connected to rods 36 which operate cranks 37 secured to a shaft 38. The wing shafts 40 are connected to the shaft 38 by universal joints 41, to allow for the adjustment of the planes 2. Steering and balancing.-The rudder 20 may be adjusted bodily longitudinally of the machine, and also about an axis in the line of flight and a transverse axis. The rudder is mounted on a shaft 13 which is adjustably held in a hollow shaft 14 by set-screws 15. The shaft 14 is adjusted about its own axis, so as to turn the rudder for steering laterally, by means of a gear-wheel 16 engaging a sector 17 operated by a lever 19. The rudder is adjusted for elevating by means of a lever 21, telescopic rods 22, arms 23, and rods 24. Aerial machines adapted to travel also on land; framework; tanks and like containers, arrangement of.-During transport on land, the car 27 is fixed against pivotal movement by a nut on the pivot 30, and a wheel 31 is operated from a hand-wheel 32, for steering. The framework is composed of tubes which serve as reservoirs for the liquid fuel of the motor.
GB191125040D 1911-11-10 1911-11-10 Improvements in or relating to Flying Machines. Expired GB191125040A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191125040T 1911-11-10

Publications (1)

Publication Number Publication Date
GB191125040A true GB191125040A (en) 1912-08-08

Family

ID=32568314

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191125040D Expired GB191125040A (en) 1911-11-10 1911-11-10 Improvements in or relating to Flying Machines.

Country Status (1)

Country Link
GB (1) GB191125040A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9259984B2 (en) 2008-07-28 2016-02-16 Fleck Future Concepts Gmbh Combined air, water and road vehicle

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9259984B2 (en) 2008-07-28 2016-02-16 Fleck Future Concepts Gmbh Combined air, water and road vehicle

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