EP0334905B1 - Pneumatic motor with jet-propulsion disk - Google Patents

Pneumatic motor with jet-propulsion disk Download PDF

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Publication number
EP0334905B1
EP0334905B1 EP19880905874 EP88905874A EP0334905B1 EP 0334905 B1 EP0334905 B1 EP 0334905B1 EP 19880905874 EP19880905874 EP 19880905874 EP 88905874 A EP88905874 A EP 88905874A EP 0334905 B1 EP0334905 B1 EP 0334905B1
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Prior art keywords
motor
impeller
shaft
vent
contrived
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EP19880905874
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German (de)
French (fr)
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EP0334905A1 (en
Inventor
Georges Sagnial
Jacques Chauquet
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CHAUQUET, JACQUES
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Individual
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/32Non-positive-displacement machines or engines, e.g. steam turbines with pressure velocity transformation exclusively in rotor, e.g. the rotor rotating under the influence of jets issuing from the rotor, e.g. Heron turbines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D15/00Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/06Adaptations for driving, or combinations with, hand-held tools or the like control thereof
    • F01D15/065Adaptations for driving, or combinations with, hand-held tools or the like control thereof with pressure-velocity transformation exclusively in rotor

Definitions

  • the problem which the invention proposes to solve is to produce a motor capable of working at very high speed and finding multiple applications in particular for tools requiring cutting speeds requiring rotational speeds of the order of several tens of thousands. revolutions per minute.
  • a pneumatic motor of the type of those consisting, in known manner, of a rotating shaft mounted on bearings and driven in rotation under the effect of at least one jet of air exiting from at least one orifice, or exhaust outlet, formed radially at any angle on at least one propellant disc secured to the axis of the engine, the air jet being injected at said axis, the propellant disc being arranged with a bore central for its mounting on the axis and comprising, on one of its sides, a recess constituting a chamber for receiving the air jet, in the form of a fluid under pressure and high flow rate, said air jet being injected by means of a groove formed on the axis, said chamber being in communication with one or more exhaust ducts formed in the thickness of the disc and one end of which opens out from
  • the receiving chamber is cylindrical, the exhaust duct or ducts are formed throughout the thickness of the disc while flanges close the disc and the exhaust duct or ducts laterally.
  • the flanges are attached and glued to the lateral faces of the disc and to the axis of the engine, the propellant disc (s) also being glued to the axis.
  • the propellant disc is mounted in an exhaust cage having a cylindrical sleeve and extending on one side with a wall forming a bottom mounted in a fixed position on the bearings; an exhaust grille being attached and fixed to the outer or inner periphery of said sleeve.
  • the engine finds a particularly advantageous application for deburring and grinding turbines.
  • the pneumatic motor consists of a rotating shaft (1) at very high speed mounted on two bearings (2) and driven in rotation under the effect of at least one jet of air exiting under pressure and high flow leaving at least one orifice or exhaust outlet formed radially at any angle on at least one propellant disc (3) integral with the axis of the engine, said orifice opening onto the outside diameter of said propellant disc.
  • the pneumatic motor comprises one or more cages for receiving one or more propulsion discs driven in rotation by at least one injection of a pressurized fluid, liquid or gaseous.
  • the engine comprises a propellant disc (3) arranged with a central bore (3.1) for mounting on the axis of the engine.
  • the disc comprises on one of its sides a recess (3.2) constituting a chamber for receiving the pressurized fluid.
  • one or more exhaust ducts (4) originating at their end (4.1) while being in communication with the receiving chamber, and projecting through their other end (4.2) by constituting a reactive conduit over all or part of the width of the propellant disc and on the outer periphery thereof by projecting the fluid into the inner chamber of the cage exhaust.
  • the shape and profile of the exhaust and reactant duct (s) are produced in the most suitable manner for guiding and orienting the fluid, and for practical implementation.
  • the propellant disc is mounted and fixed on the axis by any appropriate means and in particular by gluing.
  • On either side of the propellant disk are disposed front and rear flanges (5-6), intended to laterally seal the disk receiving chamber and the fluid exhaust duct or ducts while leaving the reactive duct free.
  • These flanges made of any suitable material, of desired thickness, are attached and fixed to the side faces of the disc and advantageously by gluing. They are also fixed by gluing by their internal bore (5.1-6.1) on the axis of the motor.
  • the assembly thus formed is rotatably mounted in the exhaust cage (7).
  • This is in the form of a cylindrical sleeve with a bottom wall (7.1) mounted in a fixed position on the bearings (2).
  • An exhaust grid (8) is attached and fixed to the external or internal periphery of the sleeve part of the receiving cage of the propellant disc.
  • This grid is arranged in its central part with an opening for the introduction of a fluid injection nozzle (9) mounted at the end of a fluid supply pipe.
  • the axis of the nozzle is opposite the end of the motor axis.
  • the end of the latter is conical and partially engages in said nozzle to avoid loss of the fluid.
  • To guide and introduce the fluid into the receiving chamber of the propellant disc there is provided on the axis a groove (10) constituting the fluid injection conduit.
  • the operation of the air motor should be specified.
  • the user sends a pressurized fluid through the injection nozzle which penetrates via the injection duct produced on the axis of the engine into the receiving chamber of the propellant disc.
  • the fluid is then evacuated by the exhaust duct (s) arranged radially on the propellant disc.
  • the latter is then rotated by driving the axis of the motor with which it is associated.
  • the fluid is projected onto the internal periphery of the exhaust cage, then it is discharged through the openings or vents of the exhaust grille.
  • such an engine rotates at a speed which can be regulated by the intensity of projection of the fluid in order to reliably reach speeds between 25,000 and 150,000 revolutions / minute.
  • the pneumatic motor can comprise several propulsion discs mounted on the shaft giving it multiple possibilities of torque. Via the injection pipe produced on the engine axis, all the reception chambers produced on each disc will be at the same pressure as will the exhaust pipes.
  • the exhaust duct is extended to form the reactive duct, the latter being produced in the form of a hole, a slot, a keyway-like groove, of cross section suitable for the desired engine torque. .
  • the pneumatic motor according to the invention finds numerous applications.
  • this engine is particularly advantageous for deburring and grinding turbines, or engraving or drilling.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Hybrid Electric Vehicles (AREA)
  • Finish Polishing, Edge Sharpening, And Grinding By Specific Grinding Devices (AREA)

Abstract

A pneumatic motor with jet-propulsion disk comprises a rotating shaft (1) mounted on bearings to which a rotary movement is imparted by a high-speed jet of compressed air issuing from at least one part (4) or exhaust outlet arranged radially at any desired angle on at least one propulsion disk (3) integral with the shaft of the motor, said part opening on the outer diameter of the propulsion disk into an exhaust chamber.

Description

On connaît différents types de moteurs pneumatiques. On peut citer par exemple le brevet US 3748054 ou l'entraînement d'un disque propulsif s'effectue par l'injection d'un jet d'air au niveau de la périphérie du disque. On peut citer également le brevet FR 2 202 529 où l'injection du fluide en vue de l'entraînement d'un disque propulsif s'effectue au niveau de son axe d'entraînement. Dans ce brevet, le disque utilise une chambre spéciale pour créer l'évacuation de l'air sous l'effet de la force centrifuge.Different types of pneumatic motors are known. Mention may be made, for example, of patent US Pat. No. 3,748,054, where the drive of a propellant disc is effected by injecting an air jet at the periphery of the disc. Mention may also be made of patent FR 2 202 529 where the injection of the fluid with a view to driving a propellant disc is carried out at its drive axis. In this patent, the disc uses a special chamber to create the evacuation of air under the effect of centrifugal force.

Le problème que se propose de résoudre l'invention est de réaliser un moteur susceptible de travailler à très grande vitesse et trouvant de multiples applications notamment pour les outils exigant des vitesses de coupe nécessitant des vitesse de rotation de l'ordre de plusieurs dizaines de milliers de tours par minute.The problem which the invention proposes to solve is to produce a motor capable of working at very high speed and finding multiple applications in particular for tools requiring cutting speeds requiring rotational speeds of the order of several tens of thousands. revolutions per minute.

Un autre problème que se propose de résoudre l'invention est de concevoir un moteur pnematique de fabrication simple, de montage rapide, peu couteux, de poids et d'encombrement faibles évitant toute pièce de liaison et de fixation, tout en garantissant une grande fiabilité de fonctionnement.
Pour résoudre ce problème, il a été conçu et mis au point un moteur pneumatique du type de ceux constitué, de manière connue, d'un arbre tournant monté sur paliers et entraîné en rotation sous l'effet d'au moins un jet d'air sortant d'au moins un orifice, ou bouche d'échappement, ménagé radialement à un angle quelconque sur au moins un disque propulseur solidaire de l'axe du moteur, le jet d'air étant injecté au niveau dudit axe, le disque propulseur étant agencé avec un alésage central pour son montage sur l'axe et comprenant, sur l'un de ses côtés, un chambrage constituant une chambre de réception du jet d'air, sous forme d'un fluide sous pression et débit élevé, ledit jet d'air étant injecté au moyen d'une gorge formée sur l'axe, ladite chambre étant en communication avec un ou plusieurs conduits d'échappement formés dans l'épaisseur du disque et dont une extrémité débouche de sa périphérie extérieure, en constituant un conduit réactif.
Another problem which the invention proposes to solve is to design a pneumatic motor of simple manufacture, quick assembly, inexpensive, of low weight and size avoiding any connecting and fixing part, while guaranteeing high reliability. Operating.
To solve this problem, it has been designed and developed a pneumatic motor of the type of those consisting, in known manner, of a rotating shaft mounted on bearings and driven in rotation under the effect of at least one jet of air exiting from at least one orifice, or exhaust outlet, formed radially at any angle on at least one propellant disc secured to the axis of the engine, the air jet being injected at said axis, the propellant disc being arranged with a bore central for its mounting on the axis and comprising, on one of its sides, a recess constituting a chamber for receiving the air jet, in the form of a fluid under pressure and high flow rate, said air jet being injected by means of a groove formed on the axis, said chamber being in communication with one or more exhaust ducts formed in the thickness of the disc and one end of which opens out from its outer periphery, constituting a reactive duct.

Selon l'invention, la chambre de réception est cylindrique, le ou les conduits d'échappement sont formés dans la totalité de l'épaisseur du disque tandis que des flasques obturent latéralement le disque et le ou les conduits d'échappement.According to the invention, the receiving chamber is cylindrical, the exhaust duct or ducts are formed throughout the thickness of the disc while flanges close the disc and the exhaust duct or ducts laterally.

Les flasques sont rapportés et collés sur les faces latérales du disque et sur l'axe du moteur, le ou les disques propulseurs étant également collés sur l'axe.The flanges are attached and glued to the lateral faces of the disc and to the axis of the engine, the propellant disc (s) also being glued to the axis.

Le disque propulseur est monté dans une cage d'échappement présentant un manchon cylindrique et se prolongeant sur un côté avec une paroi formant fond montée à position fixe sur les paliers ; une grille d'échappement étant rapportée et fixée sur la périphérie extérieure ou intérieure dudit manchon.The propellant disc is mounted in an exhaust cage having a cylindrical sleeve and extending on one side with a wall forming a bottom mounted in a fixed position on the bearings; an exhaust grille being attached and fixed to the outer or inner periphery of said sleeve.

Selon une autre caractéristique, le moteur trouve une application particulièrement avantageuse pour les turbines d'ébavurage et de meulage.According to another characteristic, the engine finds a particularly advantageous application for deburring and grinding turbines.

Ces caractéristiques et d'autres encore ressortiront bien de la suite de la description.These characteristics and others will become apparent from the following description.

Pour fixer l'objet de l'invention d'une manière non limitative illustrée aux figures des dessins où :

  • La figure 1 est une vue en coupe longitudinale du moteur pneumatique selon l'invention.
  • La figure 2 est une vue à grande échelle et en perspective du disque propulseur du moteur, illustrant notamment la chambre de réception du fluide.
  • La figure 3 est une vue de face du disque propulseur.
  • La figure 4 est une vue de côté selon la ligne A-A de la figure 3.
To fix the subject of the invention in a nonlimiting manner illustrated in the figures of the drawings where:
  • Figure 1 is a longitudinal sectional view of the pneumatic motor according to the invention.
  • FIG. 2 is a large-scale perspective view of the propellant disk of the engine, in particular illustrating the fluid reception chamber.
  • Figure 3 is a front view of the propellant disc.
  • FIG. 4 is a side view along the line AA in FIG. 3.

Afin de rendre plus concret l'objet de l'invention, on le décrit maintenant d'une manière non limitative aux figures des dessins.In order to make the object of the invention more concrete, it is now described in a nonlimiting manner in the figures of the drawings.

Le moteur pneumatique est constitué d'un arbre tournant (1) à très grande vitesse monté sur deux paliers (2) et entrainés en rotation sous l'effet d'au moins un jet d'air sortant sous pression et débit élevé sortant d'au moins un orifice ou bouche d'échappement ménagé radialement à un angle quelconque sur au moins un disque propulseur (3) solidaire de l'axe du moteur, ledit orifice débouchant sur le diamètre extérieur dudit disque propulseur.The pneumatic motor consists of a rotating shaft (1) at very high speed mounted on two bearings (2) and driven in rotation under the effect of at least one jet of air exiting under pressure and high flow leaving at least one orifice or exhaust outlet formed radially at any angle on at least one propellant disc (3) integral with the axis of the engine, said orifice opening onto the outside diameter of said propellant disc.

Plus précisémment, le moteur pneumatique comporte une ou plusieurs cages de réception d'un ou plusieurs disques propulseurs entrainés en rotation par au moins une injection d'un fluide sous pression, liquide ou gazeux.More precisely, the pneumatic motor comprises one or more cages for receiving one or more propulsion discs driven in rotation by at least one injection of a pressurized fluid, liquid or gaseous.

En se référant aux dessins, le moteur comprend un disque propulseur (3) agencé avec un alésage central (3.1) pour son montage sur l'axe du moteur.Referring to the drawings, the engine comprises a propellant disc (3) arranged with a central bore (3.1) for mounting on the axis of the engine.

Le disque comprend sur l'un de ses côtés un chambrage (3.2) constituant une chambre de réception du fluide sous pression.The disc comprises on one of its sides a recess (3.2) constituting a chamber for receiving the pressurized fluid.

Sur la périphérie du disque propulseur et dans son épaisseur sont réalisés un ou plusieurs conduits d'échappement (4) prenant naissance à leur extrémité (4.1) en étant en communication avec la chambre de réception, et débordant par leur autre etrémité (4.2) en constituant un conduit réactif sur tout ou partie de la largeur du disque propulseur et sur la périphérie extérieure de celui-ci en projetant le fluide dans la chambre intérieure de la cage d'echappement.On the periphery of the propellant disc and in its thickness are made one or more exhaust ducts (4) originating at their end (4.1) while being in communication with the receiving chamber, and projecting through their other end (4.2) by constituting a reactive conduit over all or part of the width of the propellant disc and on the outer periphery thereof by projecting the fluid into the inner chamber of the cage exhaust.

La forme et le profil du ou des conduits d'échappement et réactif sont réalisés de la manière la plus appropriée pour le guidage et l'orientation du fluide, et la réalisation pratique.The shape and profile of the exhaust and reactant duct (s) are produced in the most suitable manner for guiding and orienting the fluid, and for practical implementation.

Le disque propulseur est monté et fixé sur l'axe par tous moyens appropriés et en particulier par collage. De part et d'autre du disque propulseur sont disposés des flasques avant et arrière (5-6), destinés à étancher latéralement la chambre de réception du disque et le ou les conduits d'échappement du fluide tout en laissant libre le conduit réactif. Ces flasques réalisés en tous matériaux appropriés, d'épaisseur désirée, sont rapportés et fixes sur les faces latérales du disque et avantageusement par collage. Ils sont également fixés par collage par leur alésage intérieur (5.1-6.1) sur l'axe du moteur.The propellant disc is mounted and fixed on the axis by any appropriate means and in particular by gluing. On either side of the propellant disk are disposed front and rear flanges (5-6), intended to laterally seal the disk receiving chamber and the fluid exhaust duct or ducts while leaving the reactive duct free. These flanges made of any suitable material, of desired thickness, are attached and fixed to the side faces of the disc and advantageously by gluing. They are also fixed by gluing by their internal bore (5.1-6.1) on the axis of the motor.

L'ensemble ainsi constitué est monté à rotation dans la cage d'échappement (7). Celle-ci se présente sous la forme d'un manchon cylindrique avec une paroi formant fond (7.1) monté à position fixe sur les paliers (2). Une grille d'échappement (8) est rapportée et fixée sur la périphérie extérieure ou interne de la partie manchon de la cage de réception du disque propulseur. Cette grille est aménagée dans sa partie centrale avec une ouverture pour l'introduction d'une buse d'injection de fluide (9) montée en bout d'un tuyau d'alimentation du fluide. L'axe de la buse est en regard de l'extrémité de l'axe moteur. L'extrémité de ce dernier est conique et s'engage partiellement dans ladite buse pour éviter une déperdition du fluide. Pour assurer le guidage et l'introduction du fluide dans la chambre de réception du disque propulseur, il est prévu sur l'axe une gorge (10) constituant le conduit d'injection du fluide.The assembly thus formed is rotatably mounted in the exhaust cage (7). This is in the form of a cylindrical sleeve with a bottom wall (7.1) mounted in a fixed position on the bearings (2). An exhaust grid (8) is attached and fixed to the external or internal periphery of the sleeve part of the receiving cage of the propellant disc. This grid is arranged in its central part with an opening for the introduction of a fluid injection nozzle (9) mounted at the end of a fluid supply pipe. The axis of the nozzle is opposite the end of the motor axis. The end of the latter is conical and partially engages in said nozzle to avoid loss of the fluid. To guide and introduce the fluid into the receiving chamber of the propellant disc, there is provided on the axis a groove (10) constituting the fluid injection conduit.

Il est en outre prévu à l'arrière du moteur pneumatique ainsi conçu un nez ou bague d'arrêt (11) venant en appui sur les paliers.There is also provided at the rear of the pneumatic motor thus designed a nose or stop ring (11) coming to bear on the bearings.

Il convient de préciser le fonctionnement du moteur pneumatique. L'utilisateur envoie un fluide sous pression par la buse d'injection qui pénètre par l'intermédiaire du conduit d'injection réalisé sur l'axe du moteur dans la chambre de réception du disque propulseur.The operation of the air motor should be specified. The user sends a pressurized fluid through the injection nozzle which penetrates via the injection duct produced on the axis of the engine into the receiving chamber of the propellant disc.

Le fluide est alors évacué par le ou les conduits d'échappement disposés radialement sur le disque propulseur. Ce dernier est alors mis en rotation en entrainant l'axe du moteur auquel il est associé. Le fluide est projeté sur la périphérie interne de la cage d'échappement, puis il est évacué par les ouvertures ou évents de la grille d'échappement.The fluid is then evacuated by the exhaust duct (s) arranged radially on the propellant disc. The latter is then rotated by driving the axis of the motor with which it is associated. The fluid is projected onto the internal periphery of the exhaust cage, then it is discharged through the openings or vents of the exhaust grille.

Selon les expérimentations effectuées un tel moteur tourne à une vitesse qui peut être régulée par l'intensité de projection du fluide pour atteindre en toute fiabilité des vitesses entre 25 000 et 150 000 tours/minutes.According to the experiments carried out, such an engine rotates at a speed which can be regulated by the intensity of projection of the fluid in order to reliably reach speeds between 25,000 and 150,000 revolutions / minute.

Sans sortir du cadre de l'invention, le moteur pneumatique peut comprendre plusieurs disques propulseurs montés sur l'arbre lui conférant de multiples possibilités de couple. Par l'intermédiaire du conduit d'injection réalise sur l'axe moteur, toutes les chambres de réception réalisées sur chaque disque seront à la même pression ainsi que les conduits d'échappement.Without departing from the scope of the invention, the pneumatic motor can comprise several propulsion discs mounted on the shaft giving it multiple possibilities of torque. Via the injection pipe produced on the engine axis, all the reception chambers produced on each disc will be at the same pressure as will the exhaust pipes.

Par ailleurs, le conduit d'échappement se prolonge pour former le conduit réactif, celui-ci étant réalisé sous la forme d'un trou, d'une fente, d'une rainure type rainure de clavette, de section appropriée au couple moteur désiré.Furthermore, the exhaust duct is extended to form the reactive duct, the latter being produced in the form of a hole, a slot, a keyway-like groove, of cross section suitable for the desired engine torque. .

Le moteur pneumatique selon l'invention trouve de très nombreuses applications.The pneumatic motor according to the invention finds numerous applications.

En particulier, ce moteur est particulièrement intéressant pour les turbines d'ébavurage et meulage, ou gravure ou perçage.In particular, this engine is particularly advantageous for deburring and grinding turbines, or engraving or drilling.

Les avantages ressortent bien de l'invention. En particulier, on souligne :

  • la simplicité de montage du moteur, évitant l'utilisation de toutes pièces de liaison.
  • la simplicité de fabrication des éléments constitutifs du moteur réduisant son prix de revient.
  • La grande fiabilité de fonctionnement.
The advantages emerge clearly from the invention. In particular, we emphasize:
  • the simplicity of mounting the motor, avoiding the use of any connecting parts.
  • the simplicity of manufacture of the constituent elements of the engine reducing its cost price.
  • High operating reliability.

Claims (9)

  1. Air motor consisting of a bearing-mounted rotating shaft (1) driven by at least one air jet from at least one orifice or vent contrived radially and at a given angle to at least one impeller (3) integral with the motor shaft, the air jet being injected into said shaft and the impeller (3) featuring a central bore (3.1) for shaft mounting and a recessed channel (3.2) on either side to receive the air jet injected under pressure and at high flow rates through an integral shaft line, said recessed channel communicating with one or more vent slots (4) contrived in the thickness of the impeller (3), with one end of the slot(s) opening onto the circumference of the impeller and constituting a reactive channel, characterized in that the recessed channel is cylindrical and in that the vent slot(s) are contrived in the full thickness of the impeller and in that the shrouds (5) (6) laterally obturate the impeller (3) and the vent slot(s).
  2. Motor as claimed in claim 1, characterized in that the shrouds are glued onto the impeller sides and the motor shaft and in that the impeller(s) are likewise glued onto the shaft.
  3. Motor as claimed in both claims 1 and 2, characterized in that the impeller is mounted within an impeller housing (7) consisting of a cylindrical sleeve extending down one side with a wall acting as a bottom rigidly positioned on the bearings and a loose vent gate (8) being mounted on the outer or inner periphery of said sleeve.
  4. Motor as claimed in claim 3, characterized in that the vent gate (8) is designed to receive the end of an injection nozzle equipping a fluid supply line.
  5. Motor as claimed in any of claims 1, 2, 3 and 4, characterized in that the shaft of said motor features an integral injection fluid line between the recessed impeller channel and the injection nozzle.
  6. Motor as claimed in claim 5, characterized in that the motor shaft end is conical, entering the cavity of the injection nozzle to a substantial depth.
  7. Motor as claimed in any of claims 1, 3, 4, 5 and 6, characterized in that it features a plurality of impeller housings, each equipped with an impeller.
  8. Motor as claimed in any of claims 1, 3, 4, 5 and 6, characterized in that it features a plurality of impellers mounted in the same housing and on the same motor shaft, said shaft being contrived with an injection line carrying a fluid under a single pressure to the various recessed impeller channels.
  9. Use of the motor described in any of claims 1, 3, 4, 5 and 6 and either of claims 7 or 8, in applications such as deburring, grinding, engraving or drilling turbines.
EP19880905874 1987-06-17 1988-06-17 Pneumatic motor with jet-propulsion disk Expired - Lifetime EP0334905B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT88905874T ATE101238T1 (en) 1987-06-17 1988-06-17 AIR MOTOR WITH RETURN PULLEY.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8708890A FR2616845A1 (en) 1987-06-17 1987-06-17 PNEUMATIC MOTOR
FR8708890 1987-06-17

Publications (2)

Publication Number Publication Date
EP0334905A1 EP0334905A1 (en) 1989-10-04
EP0334905B1 true EP0334905B1 (en) 1994-02-02

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EP19880905874 Expired - Lifetime EP0334905B1 (en) 1987-06-17 1988-06-17 Pneumatic motor with jet-propulsion disk

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US (1) US5118250A (en)
EP (1) EP0334905B1 (en)
DE (1) DE3887678T2 (en)
FR (1) FR2616845A1 (en)
WO (1) WO1988010358A1 (en)

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GB2240817A (en) * 1990-02-09 1991-08-14 Vni I Kt I Kompressornogo Mash Reaction-jet turbine
GB9924283D0 (en) * 1999-10-14 1999-12-15 Potential Makes Work Limited Method and apparatus for generating motive power
US8850791B2 (en) * 2007-03-31 2014-10-07 Jinan Metal Haber Metallurgical Technology Development Co., Ltd Flywheel engine
US10634181B2 (en) 2013-03-12 2020-04-28 Case Western Reserve University Asymmetrical-force connector system
WO2014161555A1 (en) * 2013-03-31 2014-10-09 محسن نصر الدين علي يوسف، Electricity generator with jet
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Publication number Publication date
FR2616845B1 (en) 1994-08-19
DE3887678D1 (en) 1994-03-17
FR2616845A1 (en) 1988-12-23
EP0334905A1 (en) 1989-10-04
DE3887678T2 (en) 1994-06-23
US5118250A (en) 1992-06-02
WO1988010358A1 (en) 1988-12-29

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