US1047266A - Turbine-driven helicopter. - Google Patents

Turbine-driven helicopter. Download PDF

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Publication number
US1047266A
US1047266A US54348510A US1910543485A US1047266A US 1047266 A US1047266 A US 1047266A US 54348510 A US54348510 A US 54348510A US 1910543485 A US1910543485 A US 1910543485A US 1047266 A US1047266 A US 1047266A
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turbine
steam
propeller
screen
shaft
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US54348510A
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Gustav Mees
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C23/00Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/005Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds

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  • the subject of the present invention is a' flaring mouth. 'lVheels a, b are driven by the two blade rims 0 and d of a steam turbine likewise rotating. in opposite directions, the upper rim 0 of which is rigidly connected to the lower propeller wheel 6.
  • the propeller wheel I) mounted on a thrust journal is of the turbine shaft '10 rotates thus with the upper steam blade rim 0 fixed thereto in the one direction; the tur-. bine shaft itself with the steam blade rim d tkeyed to its lower part and the propeller wheel a, keyed to its upper end. so as to face the contracted neck of screen S, rotates, however, in'the other direction.
  • the lower end of the turbine shaft is constructed as a steam inlet pipe, and it is supported by means of a thrust journal in a suitable bearing fixed to a star-shaped frame or spider n, it, carried by screen S.
  • Theprinciple for the operation of the ar-' y rangement remains the same whether I employ pure steam or a mixture of combustiblev gas and. superheated steam obtained from a suitably constructed working gas generator.
  • a mixture of combustible gas and compressed air may be used for driving the turbine as well.
  • the driving of the propeller can be effectedinstead of by a steam or gas turbine by any other suitable engine.
  • a rotary petrol engine' may be used therefor, the cylinders of which, connected in a suitable manner with one of the propeller wheels would have to rotate in the one direction, while the crank shaft, connected with the other propeller wheel, would have to rotatein the other direction.
  • the ideal driving machine for the propeller is, however, undoubtedly the steam or the gas turbine.
  • a turbine driven helicopter comprising an apertured screen, an axially extending rotatable shaft, a first turbine-like propeller wheel fast on said shaft, a second turbinelike propeller wheel rotatable around the shaft, means for rotatingthe wheels in opposite directions, a spider carried by the screen, and a thrust bearing interposed be tween said spider and shaft.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Description

G. MEES.
TURBINE DRIVEN HELICOPTER.
APPLIOATION FILED FEB. 12, 1910.
1,047,266, Patented Dec. 17,1912.
Sleam UNITED STATES PATENT OFFICE.
GUSTAV MEES, OF CHARLOTTENBURG, GERMANY.
TURBINE-DRIVEN HELICOPTER.
Specification of Letters Patent.
Application filed February 12, 1910; Serial No. 543,485.
Patented Dec.17, 1912.
To all whom, it may concern:
Be it known that I, GUSTAV MEEs, a citizen of Germany, residing at Charlottenburg, Germany, have invented new and useful Improvements in Turbine-Driven Helicopters, of which the following is 'a specification.
The subject of the present invention is a' flaring mouth. 'lVheels a, b are driven by the two blade rims 0 and d of a steam turbine likewise rotating. in opposite directions, the upper rim 0 of which is rigidly connected to the lower propeller wheel 6.
The propeller wheel I) mounted on a thrust journal is of the turbine shaft '10 rotates thus with the upper steam blade rim 0 fixed thereto in the one direction; the tur-. bine shaft itself with the steam blade rim d tkeyed to its lower part and the propeller wheel a, keyed to its upper end. so as to face the contracted neck of screen S, rotates, however, in'the other direction. The lower end of the turbine shaft is constructed as a steam inlet pipe, and it is supported by means of a thrust journal in a suitable bearing fixed to a star-shaped frame or spider n, it, carried by screen S.
The necessary rigidity of the entire screen-construction is insured by the tension wires '5, i, the steam inlet pipe R serving as a support.
The air drawn in and forced downward by means of the upper propeller wheel a, which has a fan-section, is thrown with great force .at the parabolically curved plane or mouth of the supporting screen S by the lower wheel 6 whloh rotates at a very highperipheral velocity; in like manner also the exhaust steam from the steam turbine is thrown at the screen. The vertical component of the'air and steam pressure so produced, assisted by the rarefaction of the air, above the screen, enables the entire apparatus with the car attached to rise.
Owing to the opposite rotations of the two propeller wheels and of the steam blade rims, the reactionary moment of torsionis neutralized in a well known manner. This moment would otherwise cause the whole apparatus with the car to move in circles.
. It is assumed that the necessary steam for operating the turbine is obtained from a tubular boiler, preferably heated with liquid fuelplaced in the car. ,This steam is conducted to the turbine by means of a hose. The boiler can, however, obviously be fixed just as well on the supporting apparatus shown in the drawing.
Theprinciple for the operation of the ar-' y rangement remains the same whether I employ pure steam or a mixture of combustiblev gas and. superheated steam obtained from a suitably constructed working gas generator. A mixture of combustible gas and compressed air may be used for driving the turbine as well.
The driving of the propeller can be effectedinstead of by a steam or gas turbine by any other suitable engine. For example a rotary petrol engine'may be used therefor, the cylinders of which, connected in a suitable manner with one of the propeller wheels would have to rotate in the one direction, while the crank shaft, connected with the other propeller wheel, would have to rotatein the other direction. The ideal driving machine for the propeller is, however, undoubtedly the steam or the gas turbine.
I claim:
A turbine driven helicopter comprising an apertured screen, an axially extending rotatable shaft, a first turbine-like propeller wheel fast on said shaft, a second turbinelike propeller wheel rotatable around the shaft, means for rotatingthe wheels in opposite directions, a spider carried by the screen, and a thrust bearing interposed be tween said spider and shaft.
GUSTAV MEES. Witnesses:
HENRY HASPER, WOLDEMAR HAUPT.
US54348510A 1910-02-12 1910-02-12 Turbine-driven helicopter. Expired - Lifetime US1047266A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2997254A (en) * 1959-10-30 1961-08-22 Thomas P Mulgrave Gyro stabilized vertical rising vehicle
US3050275A (en) * 1959-05-28 1962-08-21 United Aircraft Corp Steam driven helicopter rotor head

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3050275A (en) * 1959-05-28 1962-08-21 United Aircraft Corp Steam driven helicopter rotor head
US2997254A (en) * 1959-10-30 1961-08-22 Thomas P Mulgrave Gyro stabilized vertical rising vehicle

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