GB662147A - Lubricating mechanism for the intermediate or translational bearings of contra-rotating airscrews - Google Patents

Lubricating mechanism for the intermediate or translational bearings of contra-rotating airscrews

Info

Publication number
GB662147A
GB662147A GB52549A GB52549A GB662147A GB 662147 A GB662147 A GB 662147A GB 52549 A GB52549 A GB 52549A GB 52549 A GB52549 A GB 52549A GB 662147 A GB662147 A GB 662147A
Authority
GB
United Kingdom
Prior art keywords
bearing
pumps
valves
airscrews
reservoir
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
GB52549A
Inventor
James Arthur Crowhurst
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.)
HAVILAND AIRCRAFT Co Ltd
De Havilland Aircraft Co Ltd
Original Assignee
HAVILAND AIRCRAFT Co Ltd
De Havilland Aircraft Co Ltd
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 HAVILAND AIRCRAFT Co Ltd, De Havilland Aircraft Co Ltd filed Critical HAVILAND AIRCRAFT Co Ltd
Priority to GB52549A priority Critical patent/GB662147A/en
Publication of GB662147A publication Critical patent/GB662147A/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
    • F16NLUBRICATING
    • F16N7/00Arrangements for supplying oil or unspecified lubricant from a stationary reservoir or the equivalent in or on the machine or member to be lubricated
    • F16N7/38Arrangements for supplying oil or unspecified lubricant from a stationary reservoir or the equivalent in or on the machine or member to be lubricated with a separate pump; Central lubrication systems
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30Blade pitch-changing mechanisms
    • 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
    • F16NLUBRICATING
    • F16N31/00Means for collecting, retaining, or draining-off lubricant in or on machines or apparatus

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Details Of Gearings (AREA)
  • Rolling Contact Bearings (AREA)

Abstract

662,147. Force feed lubricating. DE HAVILLAND AIRCRAFT CO., Ltd. Feb. 7, 1950 [Jan. 7, 1949], No. 525/49. Class 12 (iii). Lubricating mechanism for an intermediate or translational bearing of contra-rotating airscrews comprises oil pumps 8 adapted to be driven continuously by relative rotation of the two airscrews for circulating oil through the bearing 4 and an oil reservoir 7 in communication with the pumps 8 and bearing 4 for supplying oil to the pumps and for receiving oil drained from the bearing, the supply of oil to the bearing being proportional to the speed of rotation of the airscrews. The bearing races are carried by inner and outer parts 5, 6 of a housing, the parts being in driving connection with the adjacent airscrews. The reservoir 7 is contained within the part 6 which also carries the pumps 8, inlet valves 12 and outlet valves 15. The pumps 8 are of the intermeshing gear-wheel type and have shaft connections to multi-start worms 10 in driven connection with a worm wheel 11 carried by the inner part 5 so that the pumps are driven at a speed proportional to the speed of rotation of the airscrews. The inlet and outlet valves 12, 15 are centrifugally opened and spring closed, the arrangement being such that the outlet valves 15 open at a lower speed than the inlet valves 12. One or more breather valves 18 which are also centrifugally opened and spring closed are provided. A removable plug 19 is fitted for topping up the reservoir with lubricant. In operation lubricant passes from the reservoir by way of valves 12 into passageways 13 to the pumps 8 from which it is pumped through passageways 14 to the bearing. From the bearing, lubricant passes through passageways 16 and through valves 15 back to the reservoir 7. In a modification pumps driven by worm and spur gearing deliver lubricant to the bearing from which it is centrifugally returned, the inlet and outlet valves being dispensed with.
GB52549A 1949-01-07 1949-01-07 Lubricating mechanism for the intermediate or translational bearings of contra-rotating airscrews Expired GB662147A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB52549A GB662147A (en) 1949-01-07 1949-01-07 Lubricating mechanism for the intermediate or translational bearings of contra-rotating airscrews

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB52549A GB662147A (en) 1949-01-07 1949-01-07 Lubricating mechanism for the intermediate or translational bearings of contra-rotating airscrews

Publications (1)

Publication Number Publication Date
GB662147A true GB662147A (en) 1951-12-05

Family

ID=9705890

Family Applications (1)

Application Number Title Priority Date Filing Date
GB52549A Expired GB662147A (en) 1949-01-07 1949-01-07 Lubricating mechanism for the intermediate or translational bearings of contra-rotating airscrews

Country Status (1)

Country Link
GB (1) GB662147A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1477721A2 (en) * 2003-05-13 2004-11-17 Pfeiffer Vacuum GmbH Device for lubricating the bearings of a rotating shaft
CN113639029A (en) * 2021-08-16 2021-11-12 上海尚实能源科技有限公司 Turboprop engine reduction box unit body

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1477721A2 (en) * 2003-05-13 2004-11-17 Pfeiffer Vacuum GmbH Device for lubricating the bearings of a rotating shaft
EP1477721A3 (en) * 2003-05-13 2004-12-29 Pfeiffer Vacuum GmbH Device for lubricating the bearings of a rotating shaft
CN113639029A (en) * 2021-08-16 2021-11-12 上海尚实能源科技有限公司 Turboprop engine reduction box unit body

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