GB191000210A - Improvements in Flying-machines. - Google Patents

Improvements in Flying-machines.

Info

Publication number
GB191000210A
GB191000210A GB191000210DA GB191000210A GB 191000210 A GB191000210 A GB 191000210A GB 191000210D A GB191000210D A GB 191000210DA GB 191000210 A GB191000210 A GB 191000210A
Authority
GB
United Kingdom
Prior art keywords
planes
machine
steering
propellers
wheel
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
Fritz Huth
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 GB191000210A publication Critical patent/GB191000210A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

210. Huth, F. Jan. 5, 1909, [Convention date]. Aerial machines without aerostats adapted to travel also on land; planes, arrangement and construction of; propelling; steering.- An aerial machine is provided with annular supporting-planes constructed of overlapping frames of various shapes. Fig. 2 shows a triplane machine in plan and elevation, the fabric of the planes being stretched between the frames a, b. The upper plane may be over the others, or staggered as shown. The propellers are placed in the central space, and may be driven by separate motors, the propellers being connected together. The central propeller may serve as the fly-wheel of the motor. The motor may be connected to the ground wheels. Flapping wings may be used with the machine. The portions vr, vl hr, hl of the bearing-planes are movable for steering and maintaining stability. The parts may be connected to the correspondingly-marked parts shown in Fig. 4 On lifting the hand-wheel H, the bevel wheels are equally turned, and the front and rear planes are equally and oppositely turned, causing a change of altitude of the machine. Rotation of the wheel H causes the planes to be raised at one side and lowered at the other side of the machine, and also causes rotation of the vertical rudder, or of specially - provided planes, through ropes sl, sr, thus counteracting the increased resistance on one side of the machine. By this means, lateral stability is recovered. Lateral steering is effected by turning the whole steering- gear about the pillar g. Another form of steering-gear is shown in Fig. 5. By raising or lowering the shaft, the plane is symmetrically adjusted, and, by rotating the wheel H, the plane is warped, and the vertical rudder is moved through wires sl, sr. By moving the shaft in a slot f, the vertical rudder is operated without appreciably affecting the main planes. The steering-members are automatically maintained in position for straight flight, or the normal position is indicated. The relative inclination of the propeller axes and the planes may be varied to suit the speed of travel of the machine. The Specification in the original form, as open to inspection under Section 91 (3) (a), comprises also the following subject-matter: Intermeshing propellers, as shown in Fig. 4<a> (Cancelled), rotate oppositely in a casing indicated by the dotted !ines, whereby the lifting effect is increased. This is also effected by moving the propeller blades farther from their centre of rotation during the downward movement, as shown in Fig. 5<a> (Cancelled). The rod to which the blades f, f<1> are fixed slides transversely under the influence of the crank l, pivoted at m and engaging the rod at k. If the displacement takes place at one side only, the machine turns. The propellers may further be driven through eccentrics in order to accelerate the downward movement. Where several motors are used, the propellers are connected together, suitable clutches or free-wheel gears being provided. This subject-matter does not appear in the Specification as accepted,
GB191000210D 1909-01-05 1910-01-04 Improvements in Flying-machines. Expired GB191000210A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE191000210X 1909-01-05

Publications (1)

Publication Number Publication Date
GB191000210A true GB191000210A (en) 1910-09-29

Family

ID=32405554

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191000210D Expired GB191000210A (en) 1909-01-05 1910-01-04 Improvements in Flying-machines.

Country Status (1)

Country Link
GB (1) GB191000210A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005092704A1 (en) * 2004-03-29 2005-10-06 Kimura, Yumiko Aircraft having a ring-shaped wing structure

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005092704A1 (en) * 2004-03-29 2005-10-06 Kimura, Yumiko Aircraft having a ring-shaped wing structure

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