US868039A - Steering-gear for winged flying-machines or air-ships. - Google Patents

Steering-gear for winged flying-machines or air-ships. Download PDF

Info

Publication number
US868039A
US868039A US36610407A US1907366104A US868039A US 868039 A US868039 A US 868039A US 36610407 A US36610407 A US 36610407A US 1907366104 A US1907366104 A US 1907366104A US 868039 A US868039 A US 868039A
Authority
US
United States
Prior art keywords
air
ring
slats
steering
ships
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 - Lifetime
Application number
US36610407A
Inventor
Julius Uherkovich De Uherkocz
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 US36610407A priority Critical patent/US868039A/en
Application granted granted Critical
Publication of US868039A publication Critical patent/US868039A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers

Definitions

  • My invention relates more particularly to an adjustable steering gear for guiding a flying machine or airship when in flight in the air or sustained in the air, and is especially adapted to what are commonly known as winged flying machines sustained by pairs of flapping or moving wings.
  • My invention is described as attached to a novel ribbed body frame to which are attached two wings having hinged connection with the body and which are vibrated up and down by means of revolving disks, wrist-pins and operated slotted levers connected with the wings.
  • my novel steering gear, an extended fan-shaped projection which aids in sustaining the equilibrium of the body in the air.
  • My invention consists of 'a frame with a circular and pivoted connection with the body and to which frame are attached ribs forming a light but rigid support for the covering of the frame. Also there are attached to the ribs a system of flexible blades which combined invention aids in assisting the equilibrium of the body when in the air and forms a guiding fan or steering gear for guiding-the flight or'position of the body.
  • Figure 1 is the longitudinal section of a flying ma- See application Serial No. 366,103-filed chine showing my steering mechanism applied and taken .on line 1.
  • Fig. 3 is a detailed crosssection taken on line 2. '2. of Fig. 3.
  • Fig. 3 is a sectional plan-view taken on line 3. 3. of Fig. 1.
  • Fig. 4 is a cross-section taken on line 4. 4. of Fig. 1. i
  • the invention consists of a iramedstructure as shown in Figs. 1, 3 and 4.
  • My invention is attached to the rear of the body portion A. of a flying machine as shown in Figs. 1, 2 and 3. 1n the portion A. I have the frame Work consisting of framed ribs 1. 2, 3, 4 and 5 as shown in Figs. 1 and 4 and ribs 7,8 and 9 as shown in Fig. 4.
  • the rear of the body portion is preferably constructed in circular form, butl elect to attach and operate my invention in connection with any form of body of a flying following which the guiding fan is turned laterally.
  • My steering gear is constructed for the purpose of being operated in two distinct planes, horizontal and vertical as shown in Figs. Land 4.
  • the circular frame or ring D. and mounted on the outer surface of this circular frame are a series of cogs, e, e, e, etc., as shown in Figs. 1, 3 and 4.
  • To this rim D. are also attached projecting roller supports, f, g, h, 1', etc., as shown in Figs. 1, 3 and 4.
  • roller supports On these roller supports are mounted the curved rollers 10, 11, 12 and 13 which. when the circular frame is in place, run on the rail or. track 0.
  • the supports 14 and 15 which support the crank-shaft 16.
  • A1; theend. ofthe crank-shaft 16 I mount the cog-wheel 1:7.
  • the crank-shaft 16 is turned. by the handle 18 as shown in Fig. 1.
  • the cogwheel 17 is geared with a series of cogs, E.', on the circular band or rib D.
  • the rim D. is turned.
  • I mount a circular frame I which is pivotally mounted on the axis K., as shown in Fig. 4. Attached to this pivotally.
  • the worm 4l turned by the crank 42.
  • the worm 41 is geared the worm wheel 43, revolving on the shaft 44, as shown in Fig. l.
  • On this same shaft is mounted the sprocluzt-wheel 45.
  • the sprocket chain between the sprocket wheel 45, and the pivotal ring support for the base of the rudder may be loose, or this chain may be made flexible in certain portions.
  • the supporting shaft 44, for the sprocket wheel may be arranged to tilt with the movements of the rudder, or the sprocket wheel may be mounted to oscillate on the supporting shaft.
  • a steeringgear for air ships comprising; a supporting ring rotatahly supported on the ship. rudder carried by said ring, means for rotating the ring and means for tilting the rudder.
  • a steering gear comprising a supporting ring mounted to rotate, a tilting, ring in said rotatable ring, and a rudder carried by said tilting ring.
  • a steering gear for air ships comprising a supporting ring mounted to i'ot ile. a tilting rim; in said rotatable ring. a rudder carried by the tilting ring. means for tilting the rudder, and means for rotating the supporting ringv 4.
  • a rudder comprising an outer supporting ring mounted to rotate. an inner ring pivotally mounted in the outer supporting ring. means for tilting the inner ring and means for rotating the outer ringv slats secured to the inner ring and extending in divergent lines in'the shape of a fan tail, and a covering to the slats.
  • a rudder comprising a ring. slats having their ends secured to said ring. the slats arranged in diverging relation but converging to a. common plane, strengthening strips secured across the slats. brace wires, connected hetween the slats. a covering to-the ring or base portion of the rudder. and blades each having their one edge secured to one of the slats and overlapping the next adjacent slatv
  • I have aliixed my signature in presence of two witnesses.

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Description

No. 868,039 PATENTED 001?. 15, 1907.
J. U. DE UHERKOGZ. STEERING GEAR FOR WINGED FLYING MAGHINE$ 0R AIR SHIPS.
APPLIOATION FILED APB..3, 1907.
2 SHEETS-SHEET 1 AITORNEY PATENTED OCT. 15, 1907. 'J. U. DE UHERKOGZ. STEERING GEAR FOR WINGED FLYING MACHINES 0R AIR SHIPS.
APPLICATION FILED APR. 3. 1907.
-' 2 HEETS-SHBET 2.
ATTORNEY UNITED sures PATENT OFFICE.
STEERING-GEAR FOR WINGED FLYING-MACHINES OR AIR-SHIPS.
Specification of Letters Patent.
Patented Oct. 15, 1907.
' Application filed A ril 3, 1907. Serial No. 366,104.
To all whom it may concern:
Be it known that I, J umus Unaaxovron on Unan- Kocz, residing at Binghamton, in the county of Broome and State of New York, a subject of Hungary, have invented certain new and useful Improvement in- Steering-Gear for Winged Flying-Machines or Air-Ships, of which the following is a specification.
My invention relates more particularly to an adjustable steering gear for guiding a flying machine or airship when in flight in the air or sustained in the air, and is especially adapted to what are commonly known as winged flying machines sustained by pairs of flapping or moving wings.
My invention is described as attached to a novel ribbed body frame to which are attached two wings having hinged connection with the body and which are vibrated up and down by means of revolving disks, wrist-pins and operated slotted levers connected with the wings. A 'prili3, 1907. To the rigid framed body in the rear and attached thereto by circular and hinged connections is my novel steering gear, an extended fan-shaped projection which aids in sustaining the equilibrium of the body in the air.
My invention-consists of 'a frame with a circular and pivoted connection with the body and to which frame are attached ribs forming a light but rigid support for the covering of the frame. Also there are attached to the ribs a system of flexible blades which combined invention aids in assisting the equilibrium of the body when in the air and forms a guiding fan or steering gear for guiding-the flight or'position of the body. It is operated by a combination of axes operating in concentric c ircles one within the other and thus enabling my fan-shaped steering gear to take positions vertically or to be gradually changed from one degree of curve to another; to be raised up or down; to be revolved and the fan-blades placed at different angles and thus by these changed positions to enable the body 'in flight to move up or down; to the right or. to the left means of an adjustable shaft connected with the propelling power within the body, or any other form of motive power.
l elect to use in the operation of this flying machine and my steering gear, any form of motive power or v mechanical device for furnishiiig-such power as is best suited for the purpose aimed at.
With this and other objects in view the invention comprises certain novel constructions, combinations and arrangementiof parts as is hereinafter particularly described. 1 Figure 1 is the longitudinal section of a flying ma- See application Serial No. 366,103-filed chine showing my steering mechanism applied and taken .on line 1. 1. of Fig. 3. Fig.2 is a detailed crosssection taken on line 2. '2. of Fig. 3. Fig. 3 is a sectional plan-view taken on line 3. 3. of Fig. 1. Fig. 4 is a cross-section taken on line 4. 4. of Fig. 1. i
invention consists of a iramedstructure as shown in Figs. 1, 3 and 4. Y I My invention is attached to the rear of the body portion A. of a flying machine as shown in Figs. 1, 2 and 3. 1n the portion A. I have the frame Work consisting of framed ribs 1. 2, 3, 4 and 5 as shown in Figs. 1 and 4 and ribs 7,8 and 9 as shown in Fig. 4. The rear of the body portion is preferably constructed in circular form, butl elect to attach and operate my invention in connection with any form of body of a flying following which the guiding fan is turned laterally.
My steering gear is constructed for the purpose of being operated in two distinct planes, horizontal and vertical as shown in Figs. Land 4. To accomplish this I construct the circular frame or ring D., and mounted on the outer surface of this circular frame are a series of cogs, e, e, e, etc., as shown in Figs. 1, 3 and 4. To this rim D., are also attached projecting roller supports, f, g, h, 1', etc., as shown in Figs. 1, 3 and 4. On these roller supports are mounted the curved rollers 10, 11, 12 and 13 which. when the circular frame is in place, run on the rail or. track 0. I
To further operate my invention, within thebody portion I mount the supports 14 and 15 which support the crank-shaft 16. A1; theend. ofthe crank-shaft 16 I mount the cog-wheel 1:7. The crank-shaft 16 is turned. by the handle 18 as shown in Fig. 1. The cogwheel 17 is geared with a series of cogs, E.', on the circular band or rib D. Thus by the turning of the cogwheel 17, the rim D., is turned. Within the rim D., I mount a circular frame I which is pivotally mounted on the axis K., as shown in Fig. 4. Attached to this pivotally. mounted ring or band J and extending to- Ward the rear are fastened theflseries of slats 21 to 26 etc asshown in Figs. 3 and 4. These slats following the contour of the band to which they are fastened, extend in a curved line as shown in' Figs. 3 and 4 but all converge into a fiat surface or a horiiontal line at the point I, as shown in Figs. 1 and 3. They at the same time diverge while approaching this horizontal line and surface, as shown in Fig. 3. i
. At the point L between the slats of the upper half of the circular .bandll,- and those of the lower half of the circle J. I insert the cross-slat M. These converging slats, 22 to 25 etc.,- are thus securely fastened to this cross-slat M. as shown in Figs. 1, 3 and 4 and tints form the upper half of the circle J., and the slats forming the lower half of the circle J henceforth extend in a nearly parallel line to each other, those in the upper half of the circle being fastened to the upper side of the crossslat l\'l., and those on the lower half of the band J. ,being attached to the lower side of the slat M. These slats extend outward to line 3 in Fig. l, where they are supported by the cross-slat N. Thus I form and construct a fan shaped frame as shown in Fig. 3. From the crosspiece M., and to the respective ends of the extending slat mentioned and along the same and attached to them are extended blades, 30 to 37 as shown in Figs. 2 and 3. These blades are fastened on one side to the extended slats and on the other the blade edge is left unattached. To add to its strength but not to its weight, I stretch across the slats of the frame work, fine cords or wires, 39 as shown in Fig. 3. That portion of th steering gear between the point where the slats are fa: tened to the band or rim J to the point where .there is mounted the cross-slat M., I cover with canvas, cloth or any other suitable or flexible material. the ready manipulation of the steering gear in a vertical direction, I mount. within the body portion a shaft supporter, 40, as shown in Fig. 1. On these I mount the worm 4l, turned by the crank 42. On this worm 41 is geared the worm wheel 43, revolving on the shaft 44, as shown in Fig. l. On this same shaft is mounted the sprocluzt-wheel 45. To the sprocket wheel 45 is attached the sprocket chain 46 which 111 turn is attached by hinged connections to the circular band J., at the points 47 and 48. so that in the operation of the lowering or raising the steering gear. I turn the sprocket wheel which by means of the connecting sprocket chains turns upon the axis K. To revolve the steering gear vertically I turn the crank-shaft 16 which turns the cog-wheel 49, which is geared to the cogs E., on the rim J., and thus it revolves the steering gear in a Vertical plane either way. Thus by two gearings I can For either raise or lower, the steering gear or turn it vertically or horizontally.
In order to permit simultaneous rotary movement of the fan-tail rudder as Well as up and down tilting motion, the sprocket chain between the sprocket wheel 45, and the pivotal ring support for the base of the rudder, may be loose, or this chain may be made flexible in certain portions. Also the supporting shaft 44, for the sprocket wheel may be arranged to tilt with the movements of the rudder, or the sprocket wheel may be mounted to oscillate on the supporting shaft.
Having thus fully described my invention what. 1 claim as new and for which I desire Letters Patent is :1. follows:
1. A steeringgear for air ships comprising; a supporting ring rotatahly supported on the ship. rudder carried by said ring, means for rotating the ring and means for tilting the rudder.
2. A steering gear comprising a supporting ring mounted to rotate, a tilting, ring in said rotatable ring, and a rudder carried by said tilting ring.
.l. A steering gear for air ships comprising a supporting ring mounted to i'ot ile. a tilting rim; in said rotatable ring. a rudder carried by the tilting ring. means for tilting the rudder, and means for rotating the supporting ringv 4. A rudder comprising an outer supporting ring mounted to rotate. an inner ring pivotally mounted in the outer supporting ring. means for tilting the inner ring and means for rotating the outer ringv slats secured to the inner ring and extending in divergent lines in'the shape of a fan tail, and a covering to the slats.
5. A rudder comprising a ring. slats having their ends secured to said ring. the slats arranged in diverging relation but converging to a. common plane, strengthening strips secured across the slats. brace wires, connected hetween the slats. a covering to-the ring or base portion of the rudder. and blades each having their one edge secured to one of the slats and overlapping the next adjacent slatv In testimony whereof I have aliixed my signature, in presence of two witnesses.
JULIUS I'IIICRROVItIl 1 1 lllllGltKt'HZ.
Witnesses:
US36610407A 1907-04-03 1907-04-03 Steering-gear for winged flying-machines or air-ships. Expired - Lifetime US868039A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US36610407A US868039A (en) 1907-04-03 1907-04-03 Steering-gear for winged flying-machines or air-ships.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US36610407A US868039A (en) 1907-04-03 1907-04-03 Steering-gear for winged flying-machines or air-ships.

Publications (1)

Publication Number Publication Date
US868039A true US868039A (en) 1907-10-15

Family

ID=2936487

Family Applications (1)

Application Number Title Priority Date Filing Date
US36610407A Expired - Lifetime US868039A (en) 1907-04-03 1907-04-03 Steering-gear for winged flying-machines or air-ships.

Country Status (1)

Country Link
US (1) US868039A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2687858A (en) * 1952-08-06 1954-08-31 Page Ludolphus Graham Aircraft control

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2687858A (en) * 1952-08-06 1954-08-31 Page Ludolphus Graham Aircraft control

Similar Documents

Publication Publication Date Title
US868039A (en) Steering-gear for winged flying-machines or air-ships.
US1264152A (en) Aeroplane.
US920792A (en) Winged propelling and guiding mechanism for air-ships.
US1378112A (en) Flying-machine
US827017A (en) Wing of flying-machines.
US1123653A (en) Amusement apparatus or aviator-instructor.
US1034120A (en) Flying-machine.
US1129874A (en) Aeroplane.
US356743A (en) Zjvtejytor
US998978A (en) Aerial vessel.
US1308054A (en) Flying-machine
US974846A (en) Autoplane.
US958747A (en) Flying-machine.
US875787A (en) Flying or air car.
US1001849A (en) Flying-machine.
US868038A (en) Mechanism for winged flying-machines or air-ships.
US1145526A (en) Flying-machine.
US1135009A (en) Flying-machine.
US838673A (en) Automobile aerial navigator.
US1079508A (en) Flying-machine.
US998834A (en) Aerial navigating device.
US1927536A (en) Aircraft sustaining system and propulsion
US1009157A (en) Flying-machine.
US1098024A (en) Flying-machine.
US1291686A (en) Airship.