Classifications

• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
  • F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
  • F01B11/00—Reciprocating-piston machines or engines without rotary main shaft, e.g. of free-piston type
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
  • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
  • F02B71/00—Free-piston engines; Engines without rotary main shaft

Definitions

• the present invention relates to multi-tandem free piston machines, comprising several pairs of parallel engine cylinders, each cylinder containing two opposite free engine pistons, integral with compressor pistons.
• the invention more particularly relates to a multi-tandem machine with free pistons comprising a frame, an internal mobile assembly comprising a central cross member transverse to an axis of the frame, guided in translation so as to be able to move with an alternating movement the along said axis, carrying, on each side, four internal driving pistons displaceable along the driving cylinders arranged at the apices of a rectangle and two compressor pistons sliding in internal compressor cylinders whose axes pass outside said rectangle, an external mobile assembly comprising two external crosspieces connected by at least one tie rod, each carrying four external engine pistons displaceable in four of said engine cylinders and two compressor pistons sliding in external compressor cylinders, and means for synchronizing the reciprocating movement of the two crews.
• the invention aims to provide a multi-tandem machine whose frame has a very high rigidity, ensuring satisfactory guidance of the crews while allowing easy disassembly of the cylinders, and in particular of the cylinders which have a large axial dimension.
• the invention provides a machine in which the frame comprises a base, an upper base and two frames connecting the base and the base, arranged symmetrically with respect to a median plane of the frame and on which the external compressor cylinders are fixed. by their face facing the median plane, the opposite faces of said external compressor cylinders can be connected by plates.
• the invention finds a particularly important application in energy production installations including a free piston machine, a turbine with gas which receives the exhaust gases from the engine cylinders and a compressor which supplies the compressor cylinders with air at a pressure higher than atmospheric pressure, by means of a conventional cooler.
• each frame can be designed to constitute, with the base, the box spring and a casing which it contains and which delimits a space containing the corresponding external cross-member, a supply manifold for the corresponding external compressor cylinders.
• the sleepers must be provided with guide means.
• a first solution consists in providing them with sliding bearings on fixed guide tubes.
• FIG. 1 is an elevational view of the left part of the machine
• FIG. 2 is a block diagram showing the arrangement of the axes of the driving cylinders and the compression cylinders of the machine of Figure 1, seen at the end,
• the machine shown in FIG. 1 comprises a frame, an internal mobile assembly and an external mobile assembly, as well as fixed gas circulation pipes.
• the frame comprises a base 1.0 and an upper base 11 substantially of the same length, connected by an internal monobloc structure 12 and two frames 13, symmetrically arranged with respect to the median plane III. This constitution, supplemented by cruciform structures 14, gives the frame very great rigidity.
• the frame carries, by means which will be described later, four driving cylinders, two of which, 15a and 15b, appear in FIG. 1, on each side of the median plane III.
• the axes of the four cylinders 15a, 15b, 15c and 15d are arranged at the corners of a rectangle 16 which, in the illustrated embodiment, is arranged with its large side vertically.
• Two internal double-acting compressor cylinders 17a and 17b are mounted one on each side of the central monobloc structure 12. According to the invention, the axes of these cylinders 17a and 17b intersect the small median 1B of the rectangle 16.
• At each frame 13 are fixed two compressor cylinders 18a and 18b also double acting.
• the axes of the cylinders 18a and 18b intersect the large median 19 of the rectangle 16, outside of the latter.
• the internal mobile assembly comprises a central cross member 20 (FIG. 3) which, due to the forces to which it is subjected, will generally be machined in a single forged part.
• the cross member 20 is fixed to an axial guide tube 21, carried by bearings (not shown) spaced from each other by a distance at least equal to three times the diameter of the tube, and fixed to the frame.
• the cross member has two opposite horizontal arms attached to the rods 29 of the pistons of the internal compressor cylinders 17a and 17b. Two protrusions of the cross are attached to the rods of the pistons of the internal engine cylinders 15a, 15b, 15c and 15c.
• the need for lubrication of the parts in relative movement leads to the appearance of an oil mist in the area near the cross member 20.
• the central monobloc structure makes it possible to avoid projections and dispersions. important lubricant.
• this central structure is constituted by a cage 22, inside which is placed a casing 23 enveloping the cross member and of sufficient axial dimensions to allow the movement thereof.
• the casing 23 is obviously provided with seals for the passage of the rods 29 connecting the cross-member to the pistons.
• This casing or the cage can carry the bearings of the guide tube 21.
• the external mobile assembly has a symmetrical constitution with respect to the median plane III. It comprises two external crosspieces 24 (FIG. 4), the span of which can be made much smaller than that of the central crosspiece 20, which offers several advantages. On the one hand, there is a tendency to balance the masses of internal and external crews inherently. On the other hand, the stresses undergone by the external crosspieces are significantly reduced, particularly during the driving phase, when forces of opposite signs are transmitted by the rods of the external driving pistons 25a, 25b, 25c and 25d and the tie rods 26a and 26b of connection between the crosspieces 24, placed in line with the rods of the pistons of the compressor cylinders 18a and 18b. This arrangement of the tie rods allows them to pass outside the central cross member 20.
• the cross members 24, like the cross member 20, are enclosed in a casing 27 provided with sliding seals allowing passage to the Distons rods and the tie rods. They are provided with guide tubes 26 sliding in bearings not shown. These bearings can be carried by the casing 27 or by a cage 30 which surrounds it and reinforces the frame carrying the compressors.
• This device comprises two toothed wheels 31 ( Figures 4 and 5) placed in the median horizontal plane of the machine. Each wheel 31 meshes with two racks 32 and 33.
• the racks 32 are fixed to the central cross member 20 while the racks 33 are fixed to one of the external cross members 24.
• the two wheels 31 are placed on the same side of the median vertical plane of the machine not to constitute with the tie rods 26 a hyperstatic system and they are mounted on bearings having an elasticity making it possible to absorb shocks.
• the fixing of the different cylinders is carried out by means which limit overhangs.
• the external compressor cylinders 18a and 18b are fixed by their internal face, adjacent to the cross-member. This face is fixed by bolts which can also serve to retain the valve-holder plates, on the corresponding frame 13.
• This frame, the depth of which is close to the thickness of the cross-member 24, is itself fixed between base 10 and box spring 11. It is reduced in the middle by a cruciform structure which will be described later.
• the rigidity of the assembly can be increased by connecting the bottoms of the cylinders 18a and 18b by a plate 34 ( Figure 1).
• the fixing of the internal compressor cylinders 17a and 17b poses a problem which is not found in the case of the external compressor cylinders 18a and 18b. Indeed, it is necessary that the access to the injectors of the engines is possible and that one can disassemble the engine cylinders without important preliminary work and preferably in block. This result is achieved thanks to the presence of the internal monobloc structure 12.
• the compressor cylinders 17a and 17b are fixed by flanges on lateral parts of the cage 22, provided for this purpose in very thick sheet metal (40 mm for example).
• the compressor cylinders can have a true symmetry of revolution with regard to the cooling water circuits and the envelope of compressed air which they discharge, which is very favorable for the reduction of thermal stresses. .
• the driving cylinders 15a to 15d are each placed in one of the dihedrons of the cruciform structure 14. They can be introduced by simple translation and rotation in the horizontal plane. They are thus introduced into their belly panties, previously attached to the monobloc structure.
• the driving cylinders 15a to 15d are each placed in one of the dihedrons of the cruciform structure 14. They can be introduced by simple translation and rotation in the horizontal plane. They are thus introduced into their belly panties, previously attached to the monobloc structure.
• a cradle facilitating fixing.
• casings 23 and 27 make it possible to collect the lubricating oil for the bearings, therefore to reduce losses and contamination by the oil.
• the oil is collected in the bottom of the casings 23 and 27 and it is evacuated by automatic bleeders before being mixed again with the excess oil from the engine cylinders.
• Such as the oil outlets 35 and 36 appear in Figures 3 and 4.
• FIG. 3 shows the pipes 37 for supplying treated water for cooling the pistons and 38 for returning water.
• supply and return pipes 41 for cooling water from the external engine pistons are also, in FIG. 4, supply and return pipes 41 for cooling water from the external engine pistons.
• the constitution which has just been described lends itself perfectly to the implementation of a double cycle with supercharging by turbo-blowers, for example according to the scheme described in French patent application No. 78 22 168.
• This arrangement uses the fact that the compressed air directly directed to the expansion gas turbine, added to the air necessary for driving a turbo-blower, can constitute approximately half of the flow rate supplied by the compressors.
• All the compressor cylinders suck in air from the boxes formed by the cage 22 and the frames 13, boxes supplied with air by a turbo-blower not shown.
• the collectors 43 are provided with refrigerants 45 (FIG. 1) and flow into sweep collectors 46 which in turn supply all the engine cylinders 15a-d.
• the MP compressor cylinders placed to the right of the median plane, supply a medium pressure manifold (not shown in the figure). A fraction of the air admitted to this manifold MP is sent to an air turbine driving the turbo-blower. The rest of the air is mixed with the exhaust gases coming from the engine cylinders 15a-d and feeds a gas turbine coupled to the load, constituted for example by an alternator.

Landscapes

• Engineering & Computer Science (AREA)
• Mechanical Engineering (AREA)
• General Engineering & Computer Science (AREA)
• Chemical & Material Sciences (AREA)
• Combustion & Propulsion (AREA)
• Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
• Molds, Cores, And Manufacturing Methods Thereof (AREA)
• Casting Devices For Molds (AREA)

Priority Applications (2)

Applications Claiming Priority (2)

Publications (1)

Family

ID=9227056

Family Applications (1)

Country Status (12)

Cited By (2)

Families Citing this family (2)

Citations (4)

Family Cites Families (4)

• 1979
  • 1979-06-25 FR FR7916295A patent/FR2459875A1/fr active Pending
• 1980
  • 1980-06-16 CA CA354,042A patent/CA1132458A/fr not_active Expired
  • 1980-06-18 IT IT22859/80A patent/IT1131350B/it active
  • 1980-06-23 DE DE8080901199T patent/DE3061420D1/de not_active Expired
  • 1980-06-23 US US06/237,128 patent/US4678407A/en not_active Expired - Lifetime
  • 1980-06-23 JP JP50136780A patent/JPS56500724A/ja active Pending
  • 1980-06-23 WO PCT/FR1980/000097 patent/WO1981000019A1/fr not_active Ceased
  • 1980-06-25 BE BE0/201173A patent/BE884002A/fr not_active IP Right Cessation
• 1981
  • 1981-01-12 EP EP80901199A patent/EP0031344B1/fr not_active Expired
  • 1981-02-19 SU SU813247130A patent/SU948297A3/ru active
  • 1981-02-19 NO NO810579A patent/NO153541C/no unknown
  • 1981-02-23 DK DK80181A patent/DK80181A/da not_active Application Discontinuation

Patent Citations (4)

Also Published As

Similar Documents

Legal Events