US1097150A - Rotary combustion-engine for aerial machines. - Google Patents

Rotary combustion-engine for aerial machines. Download PDF

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Publication number
US1097150A
US1097150A US71424612A US1912714246A US1097150A US 1097150 A US1097150 A US 1097150A US 71424612 A US71424612 A US 71424612A US 1912714246 A US1912714246 A US 1912714246A US 1097150 A US1097150 A US 1097150A
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cylinders
shaft
engine
pistons
casing
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US71424612A
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Louis Vallez
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/26Engines with cylinder axes coaxial with, or parallel or inclined to, main-shaft axis; Engines with cylinder axes arranged substantially tangentially to a circle centred on main-shaft axis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01BMACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B3/00Reciprocating-piston machines or engines with cylinder axes coaxial with, or parallel or inclined to, main shaft axis
    • F01B3/04Reciprocating-piston machines or engines with cylinder axes coaxial with, or parallel or inclined to, main shaft axis the piston motion being transmitted by curved surfaces
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/18Mechanical movements
    • Y10T74/18056Rotary to or from reciprocating or oscillating
    • Y10T74/18296Cam and slide
    • Y10T74/18304Axial cam
    • Y10T74/18312Grooved

Definitions

  • This invention relates to combustion engines and it has special reference to such engines as are revolving about a fixed shaft.
  • the object of the invention is to provide an engine of the rotary type that shall be lighter and more compact in construction and specially adapted for use in connection with aerial machines by doing away with the crank shaft and by so arranging the cylinders parallel with their axis that the centrifugal force shall be reduced by reducing to its minimum the diameter of the revolving masses.
  • Figure 1 is a general view half in longitudinal section and half in outside view of the engine.
  • Fig. 2 is an end view thereof.
  • This engine is an engine working on the are performed during a rotation of the cylinders about the fix'ed shaft 2 which is held stationary only in the bearing 21, shown at the right of Fig. 1.
  • a drum 3 is fixed on the 1101- low stationary shaft 2 and has a groove 4 cut so as to describe two uninterrupted curves.
  • a roller 5 provided on a carriage 6 rigidly connected with the two pistons 7 and 8. It will thus be easily understood that when the cylinders 1 are rotated about the fixed shaft 2 the roller 5 running in the groove will reciprocate both pistons.
  • the curve of the groove is a double one, the four strokes of the pistons required for completing the cycle will be performed during a single rotation of the cylinders about their shaft.
  • rollers 10 running on the inner periphery of the drum casing 9 which is closed on each side by the hollow shafts carrying plates 11 and 12 on which are" fixed the cylinders which are provided at their outer ends with the distributing devices.
  • the mixture is conducted to the inlet valves through the hollow shaft 2 and through channels 13.
  • the plates 11 and 12 carrying the cylinders are both loosely mounted on the stationary shaft 2 on which they freely rotate.
  • the power is transmitted through the prolongation of the plate 12, which for that purpose is extended through the bearing 21.
  • the inlet valves 17 and outlet valves 18 are controlledby an oscillating lever 16 the one end of which is connected to a pusher 20 which receives its motion from a cam 19 fixed on the side of the drum 3, that is at a place where it is well oiled. There is only one cam for each group of cylinders.
  • the outlet ducts open into a circular collecting channel rotating with the cylinders for the purpose of damping all noise resulting from the escape and acting as a centrifugal aspirator for producing a partial vacuum in the cylinders during the time of escape whereby the volume of the working mixture drawn in is increased, the piston having no resistance to overcome and being on the contrary attracted toward the bottom ofthe cylinder, thus reducing to a minimum the quantity of burnt gases remaining in the explosion chambers.

Description

L. VALLEZ. ROTARY COMBUSTION ENGINE FOR AERIAL MACHINES.
APPLICATION FILED AUG. 9, 1912.
Patented Ma 19, 1914.
four stroke cycle in which the four strokes pours VALLEZ, or LILLE, FRANCE.
ROTARY COMBUSTION-ENGIN FOR AERIAL MACHIN ES.
Specification of Letters Patent.
Application filed August 9, 1912. Serial No. 714,246.
To all whom it may concern:
Be it known that I, Louis VALLEZ, engineer, residing at Lille, Rue du Palais Ribour, Nord, France, have invented a new and useful Rotary Combustion-Engine for Aerial Machines, which is fully set forth in the following specification.
This invention relates to combustion engines and it has special reference to such engines as are revolving about a fixed shaft.
'The object of the invention is to provide an engine of the rotary type that shall be lighter and more compact in construction and specially adapted for use in connection with aerial machines by doing away with the crank shaft and by so arranging the cylinders parallel with their axis that the centrifugal force shall be reduced by reducing to its minimum the diameter of the revolving masses.
In the annexed drawings: Figure 1 -is a general view half in longitudinal section and half in outside view of the engine. Fig. 2 is an end view thereof.
This engine is an engine working on the are performed during a rotation of the cylinders about the fix'ed shaft 2 which is held stationary only in the bearing 21, shown at the right of Fig. 1. With this object in view a drum 3 is fixed on the 1101- low stationary shaft 2 and has a groove 4 cut so as to describe two uninterrupted curves. Within such groove runs a roller 5 provided on a carriage 6 rigidly connected with the two pistons 7 and 8. It will thus be easily understood that when the cylinders 1 are rotated about the fixed shaft 2 the roller 5 running in the groove will reciprocate both pistons. Now, as the curve of the groove is a double one, the four strokes of the pistons required for completing the cycle will be performed during a single rotation of the cylinders about their shaft.
, In order to reduce friction and to prevent deformation of the carriage 6 by the action of centrifugal force, the latter is provided with rollers 10 running on the inner periphery of the drum casing 9 which is closed on each side by the hollow shafts carrying plates 11 and 12 on which are" fixed the cylinders which are provided at their outer ends with the distributing devices.
The mixture is conducted to the inlet valves through the hollow shaft 2 and through channels 13. The plates 11 and 12 carrying the cylinders are both loosely mounted on the stationary shaft 2 on which they freely rotate. The power is transmitted through the prolongation of the plate 12, which for that purpose is extended through the bearing 21.
The inlet valves 17 and outlet valves 18 are controlledby an oscillating lever 16 the one end of which is connected to a pusher 20 which receives its motion from a cam 19 fixed on the side of the drum 3, that is at a place where it is well oiled. There is only one cam for each group of cylinders.
The outlet ducts open into a circular collecting channel rotating with the cylinders for the purpose of damping all noise resulting from the escape and acting as a centrifugal aspirator for producing a partial vacuum in the cylinders during the time of escape whereby the volume of the working mixture drawn in is increased, the piston having no resistance to overcome and being on the contrary attracted toward the bottom ofthe cylinder, thus reducing to a minimum the quantity of burnt gases remaining in the explosion chambers.
Having thus described and ascertained the nature of my invention and in what manner it is to be performed, what I claim is:
1. In an engine of the character described, the combination of a fixed shaft, oppositely disposed cylinders rotatable about said shaft, pistons for said cylinders, means mounted between said cylinders for operating said pistons, a casing surrounding said means, and members closing the ends of said casing and carrying means for transmitting power to a given source.
2. In an engine of the character described, the combination of a fixed shaft, cylinders rotatable about said shaft, piston for said cylinders, means including a drum for operating said pistons, inlet and exhaust valves for said cylinders, and means carried by said drum for operating said valves.
3. In an engine of the character described, the combination of a fixed shaft, a plurality f cylinders rotatable about said shaft, pistons in said. cylinders, piston rods for said pistons, a drum casing, rollers carried by said piston rods and engaging the inner surface of said casing, a drum inclosed by said casing, connections between said drum and pistonrods whereby said cylinders are ro- Patented May 19, 1914.
tated and said pistons reciprocated, inlet and exhaust valves for said c linders, and means carried by said drum for operating said valves.
4. In an engine of the character described, the combination of a fixed shaft, a plurality sf oppositely disposed cylinders rotatable about said shaft, pistons in said cylinders, piston rods connecting the pistons of opposite cylinders, a drum casing, rollers carried by said piston rods andengaging the inner surface of said drum casing, a drum inclosed by said drum casing, connections between said piston rods and said drum whereby said cylinders are rotated and said pistons reciprocated, inlet and exhaust valves for said cylinders, and cams carried by said drum for operating said valves.
5. In an engine of the character described, the combination of a fixed shaft, a plurality of oppositely disposed cylinders rotatable about said shaft, istons for said cylinders, means fixed to said shaft for rotating said cylinders and reciprocating said pistons, a casing surrounding said means and mounted between said oppositely disposed cylinders,
and plates for closing the ends of said cas-- ing, said plates having openings for receiving the 1nner ends of said cylinders.
(3. In an engine of the character described,
the combination of a fixed shaft, a plurality of oppositely disposed cylinders rotatable about said shaft, pistons for said cylinders, means for rotating said cylinders and reciprocating said pistons, a casing surrounding said means and mounted between said oppositely disposed cylinders, and rotatable plates closing the ends of said casing, said plates having openings receiving the inner ends of said cylinders.
7 In an engine of the character described,
the combination of a fixed shaft, a plurality of cylinders rotatable about said shaft, pistons for said cylinders, means for rotating said cylinders and reciprocating said pistons, a casing surrounding said means, and rotatable members closing the ends of said casing and having sleeves extending from said members and surrounding said shaft for transmitting power to a given source.
8. In an engine of the character described,
the combination of a fixed shaft, bearings for said shaft, a plurality of c linders rotatable about said shaft, pistons or said cylinders, means fixed to said shaft for rotating said cylinders and reciprocating said pistons, a casing surroundin said means, and plates closing the ends 0 said casing and having sleeves extending from said plates and surrounding said shaft, one of said sleeves being journaled in one of said bearings and adapted to transmit power to a given source. 7 9. In an engine of the character described, the combination of a fixed shaft, bearings for said shaft, a plurality of cylinders rotatable about said shaft, pistons for said cylinders, means fixed to said shaft for rotating said cylinders and reciprocating said pistons, a case surrounding said means, and plates closing the ends of said casing, one of said plates having a sleeve extending therefrom and surrounding said shaft, said sleeve being journaled in one of said bearings and adapted to transmit power to a given source. In testimony whereof I have signed this specification in the presence of two subscribing witnesses.
LOUIS VALLEZ. Witnesses:
H. C. CoxE,
GABRIEL BELLIARD.
US71424612A 1912-08-09 1912-08-09 Rotary combustion-engine for aerial machines. Expired - Lifetime US1097150A (en)

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Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2417487A (en) * 1944-03-18 1947-03-18 Edwin S Hall Cam engine
US2445902A (en) * 1945-03-26 1948-07-27 Joseph D Bell Engine drive
US3599536A (en) * 1969-08-28 1971-08-17 Mobile Aerial Towers Inc Torque motor
US20020059907A1 (en) * 1999-03-23 2002-05-23 Thomas Charles Russell Homogenous charge compression ignition and barrel engines
US20030079715A1 (en) * 1999-03-23 2003-05-01 Hauser Bret R. Integral air compressor for boost air in barrel engine
US20040035385A1 (en) * 1999-03-23 2004-02-26 Thomas Charles Russell Single-ended barrel engine with double-ended, double roller pistons
US20040094103A1 (en) * 2002-04-30 2004-05-20 Hauser Bret R. Radial valve gear apparatus for barrel engine
US7033525B2 (en) 2001-02-16 2006-04-25 E.I. Dupont De Nemours And Company High conductivity polyaniline compositions and uses therefor
US20080006237A1 (en) * 2006-07-07 2008-01-10 Jeffrey Page Rotary cylindrical power device
US7469662B2 (en) 1999-03-23 2008-12-30 Thomas Engine Company, Llc Homogeneous charge compression ignition engine with combustion phasing
US20100236522A1 (en) * 2006-07-07 2010-09-23 Jeffrey Page Rotary Cylindrical Device With Coupled Pairs of Pistons
WO2011009454A2 (en) * 2009-07-24 2011-01-27 GETAS GESELLSCHAFT FüR THERMODYNAMISCHE ANTRIEBSSYSTEME MBH Axial-piston motor, method for operating an axial piston motor, and method for producing a heat exchanger of an axial-piston motor
US8046299B2 (en) 2003-10-15 2011-10-25 American Express Travel Related Services Company, Inc. Systems, methods, and devices for selling transaction accounts

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2417487A (en) * 1944-03-18 1947-03-18 Edwin S Hall Cam engine
US2445902A (en) * 1945-03-26 1948-07-27 Joseph D Bell Engine drive
US3599536A (en) * 1969-08-28 1971-08-17 Mobile Aerial Towers Inc Torque motor
US20020059907A1 (en) * 1999-03-23 2002-05-23 Thomas Charles Russell Homogenous charge compression ignition and barrel engines
US20030079715A1 (en) * 1999-03-23 2003-05-01 Hauser Bret R. Integral air compressor for boost air in barrel engine
US6662775B2 (en) 1999-03-23 2003-12-16 Thomas Engine Company, Llc Integral air compressor for boost air in barrel engine
US20040035385A1 (en) * 1999-03-23 2004-02-26 Thomas Charles Russell Single-ended barrel engine with double-ended, double roller pistons
US6698394B2 (en) 1999-03-23 2004-03-02 Thomas Engine Company Homogenous charge compression ignition and barrel engines
US7469662B2 (en) 1999-03-23 2008-12-30 Thomas Engine Company, Llc Homogeneous charge compression ignition engine with combustion phasing
US20040163619A1 (en) * 1999-03-23 2004-08-26 Thomas Engine Company Homogenous charge compression ignition and barrel engines
US6986342B2 (en) 1999-03-23 2006-01-17 Thomas Engine Copany Homogenous charge compression ignition and barrel engines
US7033525B2 (en) 2001-02-16 2006-04-25 E.I. Dupont De Nemours And Company High conductivity polyaniline compositions and uses therefor
US6899065B2 (en) 2002-04-30 2005-05-31 Thomas Engine Company Radial-valve gear apparatus for barrel engine
US20040094103A1 (en) * 2002-04-30 2004-05-20 Hauser Bret R. Radial valve gear apparatus for barrel engine
US8046299B2 (en) 2003-10-15 2011-10-25 American Express Travel Related Services Company, Inc. Systems, methods, and devices for selling transaction accounts
US20080006237A1 (en) * 2006-07-07 2008-01-10 Jeffrey Page Rotary cylindrical power device
US7721685B2 (en) * 2006-07-07 2010-05-25 Jeffrey Page Rotary cylindrical power device
US20100236522A1 (en) * 2006-07-07 2010-09-23 Jeffrey Page Rotary Cylindrical Device With Coupled Pairs of Pistons
WO2011009454A2 (en) * 2009-07-24 2011-01-27 GETAS GESELLSCHAFT FüR THERMODYNAMISCHE ANTRIEBSSYSTEME MBH Axial-piston motor, method for operating an axial piston motor, and method for producing a heat exchanger of an axial-piston motor
WO2011009454A3 (en) * 2009-07-24 2011-04-14 GETAS GESELLSCHAFT FüR THERMODYNAMISCHE ANTRIEBSSYSTEME MBH Axial-piston motor, method for operating an axial piston motor, and method for producing a heat exchanger of an axial-piston motor
CN102686848A (en) * 2009-07-24 2012-09-19 热力驱动系统有限责任公司 Axial-piston motor, method for operating an axial piston motor, and method for producing a heat exchanger of an axial-piston motor
CN102686848B (en) * 2009-07-24 2015-11-25 热力驱动系统有限责任公司 Axial piston motor
US9376913B2 (en) 2009-07-24 2016-06-28 Getas Gesellschaft Fuer Thermodynamische Antriebssysteme Mbh Axial-piston engine with a compressor stage, and with an engine-oil circuit and a pressure-oil circuit as well as method for operation of such an axial-piston engine

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