Abstract:
A radial-piston machine has a rotor formed with a plurality of cylinders, wherein pistons are reciprocable. Each such piston is formed on its radially outer end with a reception seat and a pivotable portion of a respective piston shoe is engageable on the seat. The piston shoes ride on an eccentric cam in a housing of the machine. Each such piston shoe may move radially into and out of engagement with the respective piston. A pair of end members axially flank the piston shoes to prevent their escape in axial direction. The former requirement to connect the piston shoes pivotably to the pistons is eliminated by the application of seal- and support-faces in the rotor, a stroke guide face on the cam, outer faces and end faces on the piston shoes and innermost faces on provided end members, whereby the piston shoes are retained between the mentioned faces, but permitted to otherwise free movement between the pistons, rotor, end members, and the cam. A certain fastening of the piston shoe to the piston may, however, be provided, if so desired.
Abstract:
An aircraft has a plurality of pairs of disc-type wings behind each other kept by holding structures on the body of the craft. Each pair has one disc-type wing on the right and one disc type wing on the left of the body, symmetrically arranged relative to the body. The discs have propeller blades which can be retracted into the discs and be extended from the discs. The discs are also provided with windows wherein adjustable covers are located which can close and open the windows.For forward flight the discs are slightly inclined to act as wings which carry the craft. For vertical take off and landing the propeller blades are extended from the discs while the discs are revolved for action of the propeller blades as lift providers for the craft. An analysis which is given in this specification shows that a considerable benefit is obtained at equal installation of power if at least two pairs of propeller revolving discs are provided on the aircraft.
Abstract:
In a radial piston pump, motor, transmission the deep diving or entering piston shoe is utilized and swingably borne in the pivot-bed of the radially reciprocating piston. Since deep diving piston shoes have large piston strokes, the shoes pivot in the pistons in large angles. Thereby a considerable force - portion of the load on the piston is transferred to the wall between the piston and the cylinder, whereby heretofore short pistons occasionally produced welding and sticking between the cylinder wall and the piston wall. The piston therefore receives radially extending portions, which may extend beyond the medial portion of the piston shoe and may even enter into the ring groove of the piston stroke actuator ring. Thereby a very long guidance of the piston on cylinder wall portions is obtained, which makes the application of effective pressure balancing pockets at correct location between piston wall and cylinder wall possible. An extended piston guide and friction - less travel of the piston in the cylinder without wearing or sticking is assured.
Abstract:
A cylinder in a fluid handling device in which high pressures and temperature vary in a periodic cycle. An outer chamber surrounding the cylinder in which a pressurized fluid is used to equalize the pressure inside and outside the cylinder wall to prevent breaking under high internal pressures. The pressurized fluid is also transferred from the outer chamber for use in the cylinder of the fluid handling device.
Abstract:
In an axial piston motor or pump the cylinder barrel is mounted on a medial shaft which has a shoulder which axially, bears against the front end of the rotor barrel. The rear end of the medial shaft is radially borne in a housing portion. The front portion of the medial shaft is provided with a bearing member of an axial thrust bearing for support on a respective axial thrust bearing member in the housing. On the rear end of the rotary barrel an axially selfthrusting control body is provided to seal the flow of fluid to and from the cylinders of the rotary barrel. The control body presses against the rotary barrel, the rotary barrel presses against the shoulder of the medial shaft and the thrust bearing member of the shaft bears on the thrust bearing member of the housing. As a result thereof the cylinders in the rotary barrel can be straight through bores. The manufacturing of the rotor barrel is thereby simplified and the flow acceleration losses of former bag bore type cylinders are prevented.
Abstract:
A control pintle carries a rotor which rotates around the pintle. The rotor has chambers which can take in and expel fluid. Passages of a reduced cross-sectional area carry the fluid to or from the control pintle and to or from the chambers. The control pintle has control parts and fluid lines, as well as certain recesses. Rotor and control pintle are insofar known from the former art. The invention provides unloading recesses in specific relation to the passages and chambers to make the rotor float around the control pintle concentrically or eccentrically in a desired extent. Supply slots are added to assist the build-up of hydrodynamic pressure fields to act in co-operation with the hydrostatic forces. Details are shown, how such supply means become provided or supply be secured.
Abstract:
A rotor having airfoil section shaped blades is set into a fluid stream. Over a connection or transmission means a propeller is connected to the rotor. The fluid stream whereinto the rotor is set gives airflow energy to the rotor and revolves the rotor. The propeller is driven by the rotor over the connection or transmission means. Since the propeller is revolved by the rotor in the fluid stream, the propeller provides a thrust. The thrust may be used to lift a weight or to drive a member. A suitable application of the arrangement is, for example, to transform a multibladed helicopter into a gliding craft which descends under a gliding angle towards the surface of the earth when the helicopter has a complete engine failure. Auto-rotation accidents can thereby be prevented. The device is also applicable to drive a vehicle or to lift a weight. Variable means can be applied to obtain variable thrusts in flying craft to improve their efficiencies or change from one flight system to another flight system. In other embodiments several novel concepts for air-borne craft are provided which include emergency landing devices, retractable and extendable or relation varifying devices for wings or propellers.
Abstract:
In a radial piston pump, motor, transmission the deep diving or entering piston shoe is utilized and swingably borne in the pivot-bed of the radially reciprocating piston. Since deep diving piston shoes have large piston strokes, the shoes pivot in the pistons in large angles. Thereby a considerable force-portion of the load on the piston is transfered to the wall between the piston and the cylinder, whereby heretofore short pistons occasionally produced welding and sticking between the cylinder wall and the piston wall. The piston therefore receives radially extending portions, which may extend beyond the medial portion of the piston shoe and may even enter into the ring groove of the piston stroke actuator ring. Thereby a very long guidance of the piston on cylinder wall portions is obtained, which makes the application of effective pressure balancing pockets at correct location between piston wall and cylinder wall possible. An extended piston guide and friction-less travel of the piston in the cylinder without wearing or sticking is assured.
Abstract:
In a fluid pump or motor improvements are provided to the piston shoes therein to permit a higher pressure in the respective device. Other improvements are done to the hydrostatic bearings in radial piston or radial chamber type fluid motors and pumps. A further arrangement is, that plural pistons are applied to permit the use of two different fluids in the respective device. This leads also to the application of disc springs and their modification in a pump or motor to make the pumping of non-viscous fluids like water possible at very high pressure. Motors are provided with arrangements to permit them to drive and to carry simultaneously or to have hollow shafts, whereby improved and novel machines and vehicles are obtained.
Abstract:
A cylindrical piston has a part-cylindrical outcut, which is slotted radially and contains a swingable pivot-member of at least part-cylindrical configuration borne in the outcut and pivoting therein under load. The mentioned outcut is formed partially around an axis which is normal to the longitudinal axis of the mentioned piston and extending through the longitudinal axis of the piston. A plurality of preferably part-annullarily formed grooves for the reception of pressure fluid are provided preferably in said pivot-member in order to lubricate bearing portions of said member between two adjacent grooves or recesses to assure a high pressure lubrication from both ends of the respective bearing portion. Efficiency and lifetime of said bearing portion is thereby increased and so is the bearing capability.