GB680482A - Improvements in or relating to power transmission - Google Patents

Improvements in or relating to power transmission

Info

Publication number
GB680482A
GB680482A GB11767/50A GB1176750A GB680482A GB 680482 A GB680482 A GB 680482A GB 11767/50 A GB11767/50 A GB 11767/50A GB 1176750 A GB1176750 A GB 1176750A GB 680482 A GB680482 A GB 680482A
Authority
GB
United Kingdom
Prior art keywords
clutch
coupling
fluid
balk
teeth
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
GB11767/50A
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.)
Raytheon Technologies Corp
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of GB680482A publication Critical patent/GB680482A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H37/00Combinations of mechanical gearings, not provided for in groups F16H1/00 - F16H35/00
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H2700/00Transmission housings and mounting of transmission components therein; Cooling; Lubrication; Flexible suspensions, e.g. floating frames
    • F16H2700/02Transmissions, specially for working vehicles

Abstract

680,482. Synchronized claw clutches; epicyclic gear. UNITED AIRCRAFT CORPORATION. May 11, 1950 [May 21, 1949], No. 11767 / 50. Classes 80 (i) and 80 (ii). [Also in Groups XXVI, XXIX and XXXIII] A toothed clutch 50, 54, between each of a number of parallel engine-shafts 5, 6, of multiple power-plant and freely mounted pinions 11 driving a common wheel 16 on the single-parallel shaft 18, Fig. 2, of a contrarotating aircraft propeller, has a fluid-coupling 60, 96, Fig. 3, which is filled only for synchronising the toothed clutch, and a positive balk 140, 106 for preventing asynchronous engagement. The axially-fixed driven clutch-member 54 forms 'part of the impeller 60 of the fluidcoupling, which is splined to the driven pinion 11, whilst the axially movable clutch-member 50 slides on the input shaft 5 on splines 102, which also carry a ring 98 having external teeth 104 engaging with limited circumferential clearance in axial slots 106 in an extension balk-sleeve of the freely-mounted turbine 96 of the fluid-coupling. With the fluid-coupling filled, as described below, for synchronizing, and transmitting torque with slip, the said torque causes the ring 98 to turn in opposition to centralising springs 146, Fig. 4, until its teeth 104 are at one end of the slots 106, taking with it the sliding clutch-member 50, rightward engaging movement of which is then prevented by butting engagement of balk-teeth 140 on the clutchmember 50 against the ends of the slots 106. Under synchronous conditions, absence of torque on the fluid-coupling causes the springs 146 to centralise the ring-teeth 104 in the slots 106 which latter then permit entry (without circumferential clearance) of the balk-teeth 140, to free the clutch-member 50 for engagement. Control is hydraulic and procedure for clutch engagement, either for driving the running gear-wheel 16 from an engine shaft 5, or for driving the shaft 5 from the running wheel 16 for starting an engine, is to turn a rotary valve 110, Fig. 3, the initial movement of which supplies pressure-oil through a duct 116 to fill the fluid-coupling, which then transmits full-load torque with slip which diminishes (but does not vanish) as synchronism approaches. This torque moves the slots 106 to balk position, as above described, so that when, during further movement of the control-valve 110 through half its extreme range, oil pressure is directed to the left faces of a group of clutch-actuating pistons 68, the latter move the clutch-member 50 axially to the balk position, and then compress clutchloading springs 78. With the engine shaft 5 driving, when the fluid-coupling attains minimum slip, the operator decelerates the engineshaft 5, the consequent initial overrun producing synchronism as the torque on the fluid-coupling vanishes, whereupon the springs 146 release the balk-slots 106 to permit full engagement of the positive clutch-member 50 with the driven teeth 54, under axial spring-load. The controlvalve 110 is then turned to the limit of its stroke, cutting off the supply to the fluid-coupling, which drains through holes 130, the clutchpistons 68 remaining. under pressure. For clutch-disengagement, the valve 110 is turned fully back to its original position to supply pressure-oil to the right faces of the pistons 68 which disengage the clutch through the springs 78 when torque-load is taken off the clutch teeth 50, 54 by the operator decelerating the engineshaft 5. To prevent overheating of the fluid coupling a valve 158, carried on a stem 156 of high thermal expansion coefficient, opens automatically to relieve the coupling above a predetermined temperature. The contra-rotating propeller drive comprises an input sun 24, Fig. 2, fast on the propeller shaft 18; planets 26 on a carrier 28 fast to an outer sleeve 35 carrying one propeller; a ring- gear 32 fast on an inner sleeve 36 carrying the other; and a reaction ring 42 meshing smaller planet-steps 38, to ensure fixed-proportioned opposite rotation of the propellers. Only one of the engines need have a starter, the others being started from it through their clutches.
GB11767/50A 1949-05-21 1950-05-11 Improvements in or relating to power transmission Expired GB680482A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US680482XA 1949-05-21 1949-05-21

Publications (1)

Publication Number Publication Date
GB680482A true GB680482A (en) 1952-10-08

Family

ID=22080090

Family Applications (1)

Application Number Title Priority Date Filing Date
GB11767/50A Expired GB680482A (en) 1949-05-21 1950-05-11 Improvements in or relating to power transmission

Country Status (1)

Country Link
GB (1) GB680482A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2156051A (en) * 1984-02-03 1985-10-02 Fluidrive Eng Co Ltd Fluid couplings

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2156051A (en) * 1984-02-03 1985-10-02 Fluidrive Eng Co Ltd Fluid couplings

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