GB464476A - Improvements in rotary engines - Google Patents

Improvements in rotary engines

Info

Publication number
GB464476A
GB464476A GB28618/35A GB2861835A GB464476A GB 464476 A GB464476 A GB 464476A GB 28618/35 A GB28618/35 A GB 28618/35A GB 2861835 A GB2861835 A GB 2861835A GB 464476 A GB464476 A GB 464476A
Authority
GB
United Kingdom
Prior art keywords
rotors
compressor
inlet
pressure
rotor
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB28618/35A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Milo AB
Original Assignee
Milo AB
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Milo AB filed Critical Milo AB
Publication of GB464476A publication Critical patent/GB464476A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00Rotary-piston machines or engines
    • F01C1/08Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing
    • F01C1/082Details specially related to intermeshing engagement type machines or engines
    • F01C1/084Toothed wheels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00Rotary-piston machines or engines
    • F01C1/08Rotary-piston machines or engines of intermeshing engagement type, i.e. with engagement of co- operating members similar to that of toothed gearing
    • F01C1/082Details specially related to intermeshing engagement type machines or engines
    • F01C1/088Elements in the toothed wheels or the carter for relieving the pressure of fluid imprisoned in the zones of engagement

Abstract

464,476. Meshing-screw engines. AKTIEBOLAGET MILO. Oct. 16, 1935, No. 28618. Convention date, Feb. 12. [A Specification was laid open to inspection under Sect. 91 of the Acts, April 17, 1936.] [Class 110 (ii)] The engine or compressor has rotors 410, 412, geared externally by gears 442, 444, so that the helical threads on the rotor do not make contact with one another. The pressure side a of a convex thread has a smaller radius of curvature than the curve b on the suction side (in the case of a compressor). Roller bearings 416, 418, take up the radial pressure, and ball bearings 424 the axial pressure. Internal cooling of the rotors is secured by means of holllow shafts provided with concentric internal tubes 446, 448, respectively. Cooling liquid is introduced by nozzles 450 into the interior tubes, and returns outside these tubes into the spaces 460. Inlet and outlet ports 462, 464, for the compressor, are provided. Radial bores 466, 470, prevent suction of lubricant into the compressor casing, and penetration of compressed medium into the bearings at the H.P. end, respectively. The top circle 474 of the smaller rotor, and the root circle of the greater rotor, coincide with the pitch circle. The constructions of a thread T and a recess R are described, to secure efficient meshing of the rotors. The rotors may be made shorter than the pitch of the threads, and the inlet and outlet ports extended to embrace parts of the end plates. Fig. 5 shows a view of the pressure end with a plate 502 provided to limit the edge of the delivery port. The bounding line of the axial port is described in the Specification, and is developed to fit the shapes of the threads and recesses of the rotors. Similarly the inlet port may be extended to embrace part of the end plate in the L.P. end. To prevent fluid being trapped by a tooth in a recess R, a small passage may be provided, which leads to the delivery port. In Fig. 1 the portion of the rotors located to the left of lines 510, 514, 512, is completely enclosed by the casing, while that to the right is in communication with the inlet 462.
GB28618/35A 1935-02-12 1935-10-16 Improvements in rotary engines Expired GB464476A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE464476X 1935-02-12

Publications (1)

Publication Number Publication Date
GB464476A true GB464476A (en) 1937-04-16

Family

ID=20310251

Family Applications (1)

Application Number Title Priority Date Filing Date
GB28618/35A Expired GB464476A (en) 1935-02-12 1935-10-16 Improvements in rotary engines

Country Status (1)

Country Link
GB (1) GB464476A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2474653A (en) * 1945-04-26 1949-06-28 Jarvis C Marble Helical gear compressor or motor
US4493623A (en) * 1983-02-22 1985-01-15 Chandler Evans Inc. Oil lubricated main drive shaft for fuel pump
US11365735B2 (en) * 2017-10-25 2022-06-21 Carrier Corporation Internal discharge gas passage for compressor

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2474653A (en) * 1945-04-26 1949-06-28 Jarvis C Marble Helical gear compressor or motor
US4493623A (en) * 1983-02-22 1985-01-15 Chandler Evans Inc. Oil lubricated main drive shaft for fuel pump
US11365735B2 (en) * 2017-10-25 2022-06-21 Carrier Corporation Internal discharge gas passage for compressor

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