CN109555786A - A kind of receipts oil ring anti-rotation location structure - Google Patents

A kind of receipts oil ring anti-rotation location structure Download PDF

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Publication number
CN109555786A
CN109555786A CN201811543792.1A CN201811543792A CN109555786A CN 109555786 A CN109555786 A CN 109555786A CN 201811543792 A CN201811543792 A CN 201811543792A CN 109555786 A CN109555786 A CN 109555786A
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China
Prior art keywords
axis
oil ring
rotation
ring
nut
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Granted
Application number
CN201811543792.1A
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Chinese (zh)
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CN109555786B (en
Inventor
郁丽
迟延飞
胡广阳
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AECC Shenyang Engine Research Institute
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AECC Shenyang Engine Research Institute
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Priority to CN201811543792.1A priority Critical patent/CN109555786B/en
Publication of CN109555786A publication Critical patent/CN109555786A/en
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Publication of CN109555786B publication Critical patent/CN109555786B/en
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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
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/30Parts of ball or roller bearings
    • F16C33/66Special parts or details in view of lubrication
    • 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
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • F16C33/10Construction relative to lubrication
    • 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
    • F16N31/02Oil catchers; Oil wipers

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Rolling Contact Bearings (AREA)

Abstract

This application discloses a kind of receipts oil ring anti-rotation location structures, it includes bearing, axis, the receipts oil ring with comb tooth, sealing ring, cupuliform locking plate and nut, bearing is installed on the outside of axis, oil ring is received to be installed on the inside of axis and position by the end face axial of axis, it receives and sets spaced sealing ring between oil ring and axis, cup type locking plate is axially inserted into the comb tooth one end for receiving oil ring, and cup type locking plate is relatively fixed to limit the rotation for receiving oil ring by nut and axis.The application realizes the purpose of design for receiving oil ring and axis circumferential direction anti-rotation and axially position, axial upper anti-rotation is devised in assembly bearing diameter of axle position rear end and positions the structure of end face, on collar radial thickness without influence, nor affect on the structure of sealing ring minimum axis internal diameter, axis external screw thread and nut cooperate simultaneously, so that the axial nothing of cupuliform locking plate realization receipts oil ring jumps, the design of nut and receipts oil ring anti-rotation, after realizing positioning, avoids sealing element caused by receiving oil ring sealing structure axial jump and radial deflection and touch and rub.

Description

A kind of receipts oil ring anti-rotation location structure
Technical field
The application belongs to aero-engine technology field, in particular to a kind of receipts oil ring anti-rotation location structure.
Background technique
Advanced aero engine, bearing fuel system much requires fuel feeding under ring, and supplies under the bearer ring of certain fulcrums Oil circuit footpath must receive oil ring and axis in the structure of axially position and circumferential anti-rotation, by axis internal diameter by receiving oil ring and axle construction It is limited with the structure size of collar radial thickness, meanwhile, for integrating the receipts oil ring of seal structure, the positioning for receiving oil ring is also determined Obturaging gap isostructuralism can design.At present guaranteeing axis internal diameter and under the premise of axis radial thickness, oil ring and axis are being received Anti-rotation location structure is only capable of taking the structure of axial anti-rotation and axial limiting, and receiving oil ring with axis is radially that clearance fit is close at two Seal positioning.
As shown in Figure 1, bearing 11 is mounted on axis 12, receives oil ring 13 and axis 12 takes the knot of axial anti-rotation and axial limiting Structure receives oil ring 3 in axial limiting by the nut 5 with rib 6, and realizes that the circumferential direction for receiving oil ring 3 and axis 2 is anti-by structure of grinding one's teeth Turn.Receive the radial fit gap of oil ring 13 and axis 12, the spacing at two between sealing 14 and comb tooth 17 and right side sealing ring 14 it Between spacing codetermined the deflection in the radial direction of comb tooth 17, when the spacing between comb tooth 17 and right side sealing ring 14 is larger When, the deflection in the radial direction of comb tooth 17 is also larger.
Seal structure is integrated due to receiving oil ring, if dimension chain control is unreasonable when assembly and work operating, will cause to receive Oil ring sealing is interfered with runway, serious for labyrinth gas seals to will lead to comb tooth and runway matrix touches to rub and causes spark or even axis Hold the failures such as chamber kindling.
Summary of the invention
The purpose of the application is any of the above-described to solve the problems, such as there is provided a kind of receipts oil ring anti-rotation location structure.
The technical solution of the application is: a kind of receipts oil ring anti-rotation location structure comprising bearing, axis, the receipts oil with comb tooth Ring, sealing ring, cupuliform locking plate and nut, bearing are installed on the outside of axis, receive oil ring and are installed on the inside of axis and the end by axis Face axially position is received and sets spaced sealing ring between oil ring and axis, and cup type locking plate is axially inserted into the comb tooth one end for receiving oil ring, and Cup type locking plate is relatively fixed to limit the rotation for receiving oil ring by nut and axis.
The oil ring anti-rotation location structure of the application realizes receipts oil ring under axis internal diameter and the limitation of collar radial thickness structure With the purpose of design of axis circumferential direction anti-rotation and axially position, axial upper anti-rotation and positioning are devised in assembly bearing diameter of axle position rear end The structure of end face nor affects on the structure of sealing ring minimum axis internal diameter, while axis external screw thread on collar radial thickness without influence Cooperate with nut, so that cupuliform locking plate realizes receipts oil ring, axially nothing jumps, nut and the design for receiving oil ring anti-rotation, realization position Afterwards, it avoids sealing element caused by receiving oil ring sealing structure axial jump and radial deflection and touches and rub.
Detailed description of the invention
In order to illustrate more clearly of technical solution provided by the present application, attached drawing will be briefly described below.It is aobvious and easy Insight, drawings discussed below are only some embodiments of the present application.
Fig. 1 is the receipts oil ring anti-rotation location structure schematic diagram of the prior art.
Fig. 2 is the receipts oil ring anti-rotation location structure schematic diagram of the application.
Specific embodiment
To keep the purposes, technical schemes and advantages of the application implementation clearer, below in conjunction in the embodiment of the present application Attached drawing, technical solutions in the embodiments of the present application is further described in more detail.
It is illustrated in figure 2 the receipts oil ring anti-rotation location structure sectional view of the application, the receipts oil ring anti-rotation positioning of this application Structure includes bearing 21, axis 22, receives oil ring 23 (with comb tooth 28), sealing ring 24, cupuliform locking plate 25, nut 26.Bearing 21 is pacified Outside loaded on axis 22 receives oil ring 23 and is installed on the inside of axis 22 and by 27 axially position of end face of axis 22, receive oil ring 23 with Spaced sealing ring 24 is set between axis 22, cup type locking plate 25 is axially inserted into 28 one end of comb tooth for receiving oil ring 23, and cup type locking plate 25 is relatively fixed to limit the rotation for receiving oil ring 23 by nut 26 and axis 22.
Wherein, the minimum diameter of axis 22 is ф d1, and the maximum outside diameter of axis 22 is ф d2, axis 22 and 21 fitting area L0 model of bearing The smallest radial ring thickness of axis 22 in enclosing is h1, and the smallest radial ring thickness of axis 22 is that (this is 22 Gewindefreistiche position of axis to h2 Set smallest radial size), above-mentioned size is that structure size is restricted requirement.
The positioning of axis 22 and receipts oil ring 23 and anti-rotation structure are arranged at axis 22 and 21 fitting area L0 of bearing and sealing ring 24 Rear end.
The receipts oil ring anti-rotation location structure of the application uses structure of grinding one's teeth, screw thread and the cup type locking plate of axis 22 and nut 26 Integrated positioning form, axis 22 and receipts oil ring 23 pass through axial structure of grinding one's teeth, while realizing circumferential anti-rotation, end after mounting Face 27 will receive 23 one end axially position of oil ring, receive 23 other end of oil ring by cupuliform retainer ring 25,26 axially position of nut.Receive oil ring 23 Anti-rotation is realized by cup type locking plate 25 with nut 26.
The application's receives oil ring anti-rotation location structure suitable for the rotor under restricted structure and with the axial direction between rotation member The design of anti-rotation axial positioning structure, soluble limit arrowhead are h1 h2.
The oil ring anti-rotation location structure of the application realizes receipts oil ring under axis internal diameter and the limitation of collar radial thickness structure With the purpose of design of axis circumferential direction anti-rotation and axially position, axial upper anti-rotation and positioning are devised in assembly bearing diameter of axle position rear end The structure of end face nor affects on the structure of sealing ring minimum axis internal diameter, while axis external screw thread on collar radial thickness without influence Cooperate with nut, so that cupuliform locking plate realizes receipts oil ring, axially nothing jumps, nut and the design for receiving oil ring anti-rotation, realization position Afterwards, it avoids sealing element caused by receiving oil ring sealing structure axial jump and radial deflection and touches and rub.
The above, the only specific embodiment of the application, but the protection scope of the application is not limited thereto, it is any Within the technical scope of the present application, any changes or substitutions that can be easily thought of by those familiar with the art, all answers Cover within the scope of protection of this application.Therefore, the protection scope of the application should be with the scope of protection of the claims It is quasi-.

Claims (1)

1. a kind of receipts oil ring anti-rotation location structure, which is characterized in that including bearing (21), axis (22), the receipts oil with comb tooth (28) Ring (23), sealing ring (24), cupuliform locking plate (25) and nut (26), bearing (21) are installed on the outside of axis (22), receive oil ring (23) it is installed on the inside of axis (22) and passes through end face (27) axially position of axis (22), receive and set between oil ring (23) and axis (22) Spaced sealing ring (24), cup type locking plate (25) are axially inserted into comb tooth (28) one end for receiving oil ring (23), and cup type locking plate (25) relatively fixed to limit the rotation for receiving oil ring (23) by nut (26) and axis (22).
CN201811543792.1A 2018-12-17 2018-12-17 Anti-rotation positioning structure of oil receiving ring Active CN109555786B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811543792.1A CN109555786B (en) 2018-12-17 2018-12-17 Anti-rotation positioning structure of oil receiving ring

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811543792.1A CN109555786B (en) 2018-12-17 2018-12-17 Anti-rotation positioning structure of oil receiving ring

Publications (2)

Publication Number Publication Date
CN109555786A true CN109555786A (en) 2019-04-02
CN109555786B CN109555786B (en) 2020-07-07

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811543792.1A Active CN109555786B (en) 2018-12-17 2018-12-17 Anti-rotation positioning structure of oil receiving ring

Country Status (1)

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CN (1) CN109555786B (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201953484U (en) * 2010-12-23 2011-08-31 中国航空工业集团公司沈阳发动机设计研究所 Device for avoiding lubricating oil leaking through adopting labyrinth sealing structure
CN203050804U (en) * 2012-12-27 2013-07-10 中国燃气涡轮研究院 Comb gear ring structure capable of being fast buckled
WO2015022373A1 (en) * 2013-08-14 2015-02-19 Aktiebolaget Skf Bearing arrangement
CN204900542U (en) * 2015-06-04 2015-12-23 中航商用航空发动机有限责任公司 Oil ring is radially received to main shaft bearing and impeller formula for aviation
CN206581990U (en) * 2016-12-30 2017-10-24 中国航发商用航空发动机有限责任公司 The system of obturaging of prewhirling of aero-engine
CN108167336A (en) * 2017-12-27 2018-06-15 中国航发哈尔滨轴承有限公司 One kind is for Aero-engine Bearing and receives oil ring connection structure

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201953484U (en) * 2010-12-23 2011-08-31 中国航空工业集团公司沈阳发动机设计研究所 Device for avoiding lubricating oil leaking through adopting labyrinth sealing structure
CN203050804U (en) * 2012-12-27 2013-07-10 中国燃气涡轮研究院 Comb gear ring structure capable of being fast buckled
WO2015022373A1 (en) * 2013-08-14 2015-02-19 Aktiebolaget Skf Bearing arrangement
CN204900542U (en) * 2015-06-04 2015-12-23 中航商用航空发动机有限责任公司 Oil ring is radially received to main shaft bearing and impeller formula for aviation
CN206581990U (en) * 2016-12-30 2017-10-24 中国航发商用航空发动机有限责任公司 The system of obturaging of prewhirling of aero-engine
CN108167336A (en) * 2017-12-27 2018-06-15 中国航发哈尔滨轴承有限公司 One kind is for Aero-engine Bearing and receives oil ring connection structure

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