GB2394523A - Drive assembly having an elongate member - Google Patents

Drive assembly having an elongate member Download PDF

Info

Publication number
GB2394523A
GB2394523A GB0224717A GB0224717A GB2394523A GB 2394523 A GB2394523 A GB 2394523A GB 0224717 A GB0224717 A GB 0224717A GB 0224717 A GB0224717 A GB 0224717A GB 2394523 A GB2394523 A GB 2394523A
Authority
GB
United Kingdom
Prior art keywords
drive assembly
drive
assembly according
engagement
article
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.)
Withdrawn
Application number
GB0224717A
Other versions
GB0224717D0 (en
Inventor
Paul Kevin Quirk
Omar Ali-Adib
Nandan Armon
Mark Alan Will
Conor Coady
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB0224717A priority Critical patent/GB2394523A/en
Publication of GB0224717D0 publication Critical patent/GB0224717D0/en
Publication of GB2394523A publication Critical patent/GB2394523A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/34Turning or inching gear
    • F01D25/36Turning or inching gear using electric motors
    • 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
    • F16C1/00Flexible shafts; Mechanical means for transmitting movement in a flexible sheathing
    • F16C1/02Flexible shafts; Mechanical means for transmitting movement in a flexible sheathing for conveying rotary movements
    • F16C1/06Flexible shafts; Mechanical means for transmitting movement in a flexible sheathing for conveying rotary movements with guiding sheathing, tube or box
    • 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
    • F16C2360/00Engines or pumps
    • F16C2360/23Gas turbine engines

Abstract

A drive assembly 30 comprises drive means 31 for providing a driving force, and engagement mechanism 34 for further driving an article, preferably the compressor 14 of a gas turbine 10. The assembly 30 further includes an elongate member 35 extending between the drive means 31 and the engagement mechanism 34, and transmission means 36 extending along the elongate member 35 to transmit the driving force from the drive means 31 to the engagement mechanism 34. The engagement mechanism 34 is preferably a belt 42 which in use drives the compressor, through friction, to allow the inspection of the compressor blades. The drive means 31 may be a motor. The elongate member may be flexible.

Description

Drive Assembly This invention relates to drive assemblies. More 5
particularly, but not exclusively, the invention relates to drive assemblies for use with gas turbine engines, for example to drive a rotary component of a gas turbine engine, such as intermediate pressure compressor.
During the servicing of gas turbine engines, it can be 10 necessary to inspect the compressors and turbines. This requires the intermediate compressor to be rotated by hand or by using a rod or a stick to rotate the compressor.
According to one aspect of this invention there is provided a drive assembly comprising drive means for 15 providing a driving force, an engagement mechanism for drivingly engaging an article, an elongate member extending between the drive means and the engagement mechanism, and transmission means extending along the elongate member to transmit the driving means extending along the elongate 20 member to transmit the driving force from the drive means to the engagement mechanism to drive the article.
Preferably the drive means comprises a motor, which may be an electric motor. Control means may be provided to control the drive means. The control means may be provided 25 on the drive means, or may be remote therefrom.
A casing may be provided to hold the drive means therein. The casing is preferably substantially cylindrical. The transmission means may be flexible and may extend 30 through the elongate member. In one embodiment, the transmission means comprises an elongate transmission element such as a cable. The transmission means may include a sleeve provided around the elongate transmission elements. The sleeve may comprise a housing through which 35 the elongate transmission element extends. The sleeve may comprise a cable housing and extend the length of the
elongate transmission element.
The engagement mechanism may comprise a gear assembly and may also include a movable engagement member engageable with the article, wherein the engagement member can be 5 driven by the drive means.
The gear assembly may comprise a worm gear arrangement. The worm gear arrangement may comprise a worm gear to which the transmission means may be connected. The worm gear arrangement may comprise a driving wheel in 10 driving engagement with the worm gear. The wheel is preferably a toothed wheel or a pulley.
The engagement member may be mounted on the wheel. A second wheel may be provided and the engagement member may extend around the driving wheel and the second wheel.
15 The engagement member may be flexible. Preferably, the engagement member comprises a track member which is conveniently endless. The engagement member conveniently has a surface to drive the article by friction engagement therewith. 20 The elongate member may be hollow and preferably comprises a tubular member. The drive means is preferably provided at a first end of the elongate member and the engagement mechanism is preferably provided at a second opposite end of the elongate member.
25 The engagement mechanism may be pivotally attached to the elongate member.
Clamping means may be provided to clamp the drive assembly to an article. The clamping means may comprise a first pair of clamping members to clampingly engage an 30 object, which may be part of the article and may also include a second pair of clamping members to clampingly engage a second part of the article. The first and second pairs of clamping members are preferably arranged opposite each other.
3s The clamping members may be formed of a plastics material, for example, nylon. The clamping members may be
movable to engage an object. Preferably, the clamping members are mounted on the elongate member and may be slidable along the elongate member into engagement with the object. 5 The preferred embodiment of this invention is particularly suitable for use in turning an intermediate compressor of a gas turbine engine, for example during inspection. With the preferred embodiment, the engagement mechanism can be inserted from the front of the engine 10 through the fan and the inlet guide vanes until the engagement member engages the intermediate compressor. The preferred embodiment of the device can be clamped to the inlet guide vanes by the clamping means. Operation of the drive means of the preferred embodiment to drive the 15 engaging member drives the intermediate compressor causing it to turn.
An embodiment of the invention will now be described by way of example only, with reference to the accompanying drawings, in which: 20 Fig. 1 is a schematic sectional side view of a gas turbine engine showing a drive assembly in use; Fig. 2 shows a drive assembly; Fig. 3 is a close up of the region marked III in Fig. 2; and 25 Fig. 4 is a view of a gear assembly used in the engagement mechanism of the drive assembly shown in Fig. 2.
With reference to Fig. 1, a ducted fan gas turbine engine generally indicated at 10 has a principal axis X-X.
The engine 10 comprises, in axial flow series, an air 30 intake 11, a propulsive fan 12, a compressor region 114 comprising an intermediate pressure compressor 14, and a high pressure compressor 16, combustion means 118 comprising a combustion 18, and a turbine region 120 comprising a high pressure turbine 20, an intermediate 35 pressure turbine 22, and a low pressure turbine 24. An exhaust nozzle 26 is provided at the tail of the engine 10.
The gas turbine engine 10 works in the conventional manner so that air entering the intake 11 is accelerated by the fan to produce two air flows: a first air flow into the intermediate pressure compressor 14 and a second air flow 5 which provides propulsive thrust. The intermediate pressure compressor 14 compresses the air flow directed into it before delivering the air to the high pressure compressor 16 where further compression takes place.
The compressed air exhausted from the high pressure 10 compressor 16 is directed into the combustion 18 where it is mixed with fuel and the mixture combusted. The resultant hot combustion products then expand through, and thereby drive the high, intermediate and low pressure turbine 20, 22 and 24 before being exhausted through the IS nozzle 26 to provide additional propulsive thrust. The high, intermediate and low pressure turbines 20, 22 and 24 respectively drive the high and intermediate pressure compressors 16 and 14 and the fan 12 by suitable interconnecting shafts 28.
20 During maintenance and service of the engine 10, it is often necessary to inspect the intermediate pressure compressor 14. For this purpose, a drive assembly 30 is provided to turn the intermediate pressure compressor on its shaft about the axis X-X.
25 Referring to Figs. 2 to 4 of the drawings, there is shown the drive assembly 30, which comprises drive means 31 comprising an electric motor 32 held within a casing 33.
The drive assembly 30 also includes an engagement mechanism 34 and a hollow elongate tubular shaft 35 extending from 30 the drive means 31 to the engagement mechanism 34.
Transmission means in the form of an elongate cable arrangement 36 extends from the motor 32 to the engagement mechanism 34 through the hollow elongate shaft 35. The motor 32 provides a driving force which is transmitted by 35 the cable arrangement 36 to the engagement mechanism 34.
Referring to Fig. 3, there is shown a close-up of the
engagement mechanism 34 which comprises a main body 38 in which is held a gear arrangement 40 (shown in more detail in Fig. 3), and a movable engagement member, in the form of a track member 42 driven by the motor 32.
5 The cable arrangement 36 comprises an inner cable 48 and a guide member which may be in the form of a cable housing 50 through which the inner cable 48 extends.
Referring to Fig. 4, the gear arrangement 40 comprises a worm gear 44 and a pulley or toothed wheel 46 arranged in 10 meshing engagement with the worm gear 44. The worm gear 44 comprises a securing portion 52 and which is mounted on the main body 38, as shown in Fig. 3, and a meshing portion 54 which engages the toothed wheel 46. A neck portion 56 extends between the securing portion 52 and the meshing 15 portion 54. The neck portion 56 is journalled in the main body 38 to allow rotation of the worm gear 44 about its main axis.
In use, spinning of the inner cable 48 about its longitudinal axis by the motor 32 causes corresponding 20 rotary motion of the worm gear 44. The meshing portion 54 of the worm gear 44 is in meshing engagement with the toothed wheel 46. The toothed wheel 46 comprises a main part 57 having thereon teeth 58 for meshing with the meshing portion 54 of the worm gear 44. The toothed wheel 25 46 is rotatably mounted on the main body 38 by pins 47.
The toothed wheel 46 also includes a central axially extending portion 60 which provides a rotary member around which the track member 42 extends.
The track member 42 extends from the toothed wheel 46 30 along the main body 38 to a further rotary member 62 which is rotatably mounted on the main body 38 by pins 63 at the opposite end thereof to the gear arrangement 40. Thus by operating the motor 32, to provide a rotary force to the inner cable about its axis, the meshing portion 54 of the 35 worm gear 44 is caused to rotate to drive the toothed wheel 46, which in turn, drives the track member 42.
As can be seen, the cable arrangement 36 extends from the elongate member 35 via an aperture 64 defined therein.
The elongate member 35 comprises a main portion 65 and an end portion 66 which is provided generally at right angles 5 to the main portion 65. The end portion 60 is pivotally mounted to the main body 38 by a U-shaped mounting arrangement 68 and a pivot pin 70.
The track member 42 is formed of a material that will not damage the blades of the intermediate compressor 14.
lO The track member 42 is in the form of an endless belt, which could be, for example, a timing belt.
The elongate shaft 35 is provided with clamping means 72 for clamping the drive assembly 30 to the variable inlet guide vanes of the gas turbine engine 10. The clamping 15 means 72 comprises two pairs of clamping members 74, 76.
Each pair of clamping members 74, 76 comprises a fixed clamping member 78 and a slidable clamping member 80 to allow the device to be securely fixed to the variable inlet guide vanes.
20 Referring back to Fig. 1, the use of the drive assembly 30 will now be described. In use, the drive assembly 30 is inserted by an inspector through the fan 12 of the gas turbine engine 10 such that the engagement portion 34 engages onto one of the blades of the 25 intermediate pressure compressor 14. The clamping members 74, 76 are arranged to clamp the drive assembly 30 to the inlet guide vanes. In order to rotate the intermediate pressure compressor 14, the engagement mechanism 34 is arranged such that the track member 42 extends generally 30 tangentially to the annulus of the intermediate pressure compressor 14 and the motor 32 can then be operated. The track member 42 is caused to rotate about the rotary members 42, 62 by the transmission of the driving force via the cable assembly 36 and the gear assembly 40 to the wheel 35 46. As a result, the drive assembly 36 rotates the intermediate pressure compressor 14 about a main axis. The
motor 32 can be controlled by control means (not shown) provided on the casing 33 or by remote control means.
In order to prevent the shaft 35 damaging the gas turbine engine lO when the drive assembly 30 is inserted S therein, the shaft 35 can be coated with a suitable shrink wrap plastics material to prevent metal to metal contact.
The main body 38 of the engagement mechanism 34 can be coated with the same material, also to prevent metal to metal contact with the blades of the intermediate pressure 10 compressor.
There is thus described a drive assembly which can be readily used to rotate the internal components of a gas turbine engine for inspection during maintenance.
Various modifications can be made without departing 15 from the scope of the invention, for example, the elongate member need not be the exact shape as shown in the drawings. Whilst endeavouring in the foregoing specification to
draw attention to those features of the invention believed 20 to be of particular importance it should be understood that the Applicant claims protection in respect of any patentable feature or combination of features hereinbefore referred to and/or shown in the drawings whether or not particular emphasis has been placed thereon.

Claims (24)

Claims:
1. A drive assembly characterised by drive means for providing a driving force, an engagement mechanism for 5 drivingly engaging an article, an elongate member extending between the drive means and the engagement mechanism, and transmission means extending along the elongate member to transmit the driving force from the drive means to the engagement mechanism to drive the article.
10
2. A drive assembly according to claim 1, wherein the drive means comprises a motor.
3. A drive assembly according to claim 2, wherein the assembly includes a casing to hold the drive means, the casing being substantially cylindrical.
15
4. A drive assembly according to any preceding claim wherein the transmission means is flexible and extends longitudinally through the elongate member.
5. A drive assembly according to claim 4, wherein the transmission means comprises an elongate transmission 20 element.
6. A drive assembly according to claim 5, wherein the elongate transmission element comprises a cable and the transmission means further includes a cable housing extending substantially the length of the elongate member 25 to guide the cable.
7. A drive assembly according to any preceding claim, wherein the engagement mechanism comprises a gear assembly and a movable engagement member engageable with the article, wherein the engagement member can be driven by the 30 drive means.
8. A drive assembly according to claim 7, wherein the gear assembly comprises a worm gear arrangement comprising a worm gear to which the transmission means may be connected, and a driving wheel in driving engagement with 35 the worm gear.
9. A drive assembly according to claim 8, wherein the
wheel is a toothed wheel or a pulley.
10. A drive assembly according to claims 8 or 9, wherein the engagement member is mounted on the wheel, and a second wheel is provided, wherein the engagement member extends 5 around the driving wheel and the second wheel.
11. A drive assembly according to claims 7 to 10, wherein the engagement member is flexible.
12. A drive assembly according to claims 7 to 10, wherein the engagement member comprises an endless track member 10 having a surface to drive the article by friction engagement therewith.
13. A drive assembly according to any preceding claim, wherein the elongate member is hollow and comprises a tubular member, the drive means being provided at a first 15 end of the elongate member and the engagement mechanism being provided at a second opposite end of the elongate member.
14. A drive assembly according to claim 13, wherein the engagement mechanism is pivotally attached to the elongate 20 member.
15. A drive assembly according to any preceding claim wherein the assembly further includes clamping means to clamp the drive assembly to an article.
16. A drive assembly according to claim 15, wherein the 25 clamping means comprises a first pair of clamping members to clampingly engage a first region of the article and a second pair of clamping members to clampingly a engage a second region of the article, at least one clamping member of each of said first and second pairs of clamping members 30 is movable along the elongate member to effect said clamping to the article.
17. A method of using a drive assembly according to any preceding claim, characterized by inserting the assembly into a gas turbine engine to engage a component thereof 35 with the engagement mechanism operating the drive means to drive the engagement mechanism, thereby driving said
component.
18. A method according to claim 17, characterized by inserting the drive assembly into the gas turbine engine via the front of the engine to engage a rotary component of 5 the engine.
19. A method according to claim 18, wherein the rotary component comprises an intermediate pressure compressor.
20. A method according to any of claims 17 to 19, wherein where the driving assembly includes clamping means, the lO method includes clamping the assembly to a further component of the engine.
21. A method according to claim 20, wherein the further component comprises an inlet guide vane of the engine.
22. A drive assembly substantially as herein described 15 with reference to Figs. 1 to 3 of the accompanying drawings.
23. A method substantially as herein described with reference to Fig. 4 of the accompanying drawings.
24. Any novel subject matter or combination including 20 novel subject matter disclosed herein, whether or not within the scope of or relating to the same invention as any of the preceding claims.
GB0224717A 2002-10-24 2002-10-24 Drive assembly having an elongate member Withdrawn GB2394523A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0224717A GB2394523A (en) 2002-10-24 2002-10-24 Drive assembly having an elongate member

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0224717A GB2394523A (en) 2002-10-24 2002-10-24 Drive assembly having an elongate member

Publications (2)

Publication Number Publication Date
GB0224717D0 GB0224717D0 (en) 2002-12-04
GB2394523A true GB2394523A (en) 2004-04-28

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Family Applications (1)

Application Number Title Priority Date Filing Date
GB0224717A Withdrawn GB2394523A (en) 2002-10-24 2002-10-24 Drive assembly having an elongate member

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009032387A2 (en) * 2007-08-15 2009-03-12 General Electric Company Manual core rotation device
EP3048246A1 (en) * 2015-01-26 2016-07-27 Rolls-Royce plc Apparatus to enable rotation of a compressor
FR3067763A1 (en) * 2017-06-20 2018-12-21 Safran Aircraft Engines ROTATIONAL DRIVE SYSTEM FOR TURBOMACHINE ROTOR AND TURBOMACHINE ROTOR
GB2581334A (en) * 2019-02-06 2020-08-19 Rolls Royce Plc Fan blade walker system
US10823014B2 (en) * 2017-12-13 2020-11-03 General Electric Company Turbine engine for reducing rotor bow and method thereof

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1415053A (en) * 1972-02-10 1975-11-26 Skf Svenska Kullagerfab Ab Steering assemblies
GB1594354A (en) * 1977-06-02 1981-07-30 Rolls Royce Device for turning the rotor of a gas turbine engine
SU754925A1 (en) * 1978-11-09 1984-01-23 N N Pavlyatenko Device for rotating rotors
US5022876A (en) * 1989-10-23 1991-06-11 Etter D Christopher Transmission means
GB2266354A (en) * 1992-04-20 1993-10-27 Jupitor Corp Rotor rotating apparatus for inspection of a jet engine
US5839961A (en) * 1996-06-15 1998-11-24 Andreas Stihl Bearing arrangement for a drive shaft
EP1134059A2 (en) * 2000-03-15 2001-09-19 Bettcher Industries, Inc. Maintenance free flexible shaft drive transmission assembly

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1415053A (en) * 1972-02-10 1975-11-26 Skf Svenska Kullagerfab Ab Steering assemblies
GB1594354A (en) * 1977-06-02 1981-07-30 Rolls Royce Device for turning the rotor of a gas turbine engine
SU754925A1 (en) * 1978-11-09 1984-01-23 N N Pavlyatenko Device for rotating rotors
US5022876A (en) * 1989-10-23 1991-06-11 Etter D Christopher Transmission means
GB2266354A (en) * 1992-04-20 1993-10-27 Jupitor Corp Rotor rotating apparatus for inspection of a jet engine
US5839961A (en) * 1996-06-15 1998-11-24 Andreas Stihl Bearing arrangement for a drive shaft
EP1134059A2 (en) * 2000-03-15 2001-09-19 Bettcher Industries, Inc. Maintenance free flexible shaft drive transmission assembly

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009032387A3 (en) * 2007-08-15 2009-05-28 Gen Electric Manual core rotation device
JP2010537101A (en) * 2007-08-15 2010-12-02 ゼネラル・エレクトリック・カンパニイ Manual core rotating device
US7866234B2 (en) 2007-08-15 2011-01-11 General Electric Company Manual core rotation device
JP2012211587A (en) * 2007-08-15 2012-11-01 General Electric Co <Ge> Manual core rotation device
JP2012215177A (en) * 2007-08-15 2012-11-08 General Electric Co <Ge> Manual core rotation device
WO2009032387A2 (en) * 2007-08-15 2009-03-12 General Electric Company Manual core rotation device
US10260369B2 (en) * 2015-01-26 2019-04-16 Rolls-Royce Plc Apparatus to enable rotation of a compressor
EP3048246A1 (en) * 2015-01-26 2016-07-27 Rolls-Royce plc Apparatus to enable rotation of a compressor
US20160215649A1 (en) * 2015-01-26 2016-07-28 Rolls-Royce Plc Apparatus to enable rotation of a compressor
FR3067763A1 (en) * 2017-06-20 2018-12-21 Safran Aircraft Engines ROTATIONAL DRIVE SYSTEM FOR TURBOMACHINE ROTOR AND TURBOMACHINE ROTOR
WO2018234681A1 (en) * 2017-06-20 2018-12-27 Safran Aircraft Engines Turbomachine rotor rotating system and turbomachine rotor
CN110785541A (en) * 2017-06-20 2020-02-11 赛峰航空器发动机 Turbomachine rotor rotation system and turbomachine rotor
US11215086B2 (en) 2017-06-20 2022-01-04 Safran Aircraft Engines Turbomachine rotor rotating system and turbomachine rotor
RU2767258C2 (en) * 2017-06-20 2022-03-17 Сафран Эркрафт Энджинз System for rotating the rotor of a gas turbine engine and rotor of a gas turbine engine
CN110785541B (en) * 2017-06-20 2022-06-17 赛峰航空器发动机 Turbomachine rotor rotation system and turbomachine rotor
US10823014B2 (en) * 2017-12-13 2020-11-03 General Electric Company Turbine engine for reducing rotor bow and method thereof
GB2581334A (en) * 2019-02-06 2020-08-19 Rolls Royce Plc Fan blade walker system

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