GB719124A - A new or improved apparatus for finishing surfaces of turbine type blades - Google Patents

A new or improved apparatus for finishing surfaces of turbine type blades

Info

Publication number
GB719124A
GB719124A GB31303/52A GB3130352A GB719124A GB 719124 A GB719124 A GB 719124A GB 31303/52 A GB31303/52 A GB 31303/52A GB 3130352 A GB3130352 A GB 3130352A GB 719124 A GB719124 A GB 719124A
Authority
GB
United Kingdom
Prior art keywords
valve
line
cylinder
blade
pump
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
GB31303/52A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB719124A publication Critical patent/GB719124A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B24GRINDING; POLISHING
    • B24BMACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
    • B24B21/00Machines or devices using grinding or polishing belts; Accessories therefor
    • B24B21/16Machines or devices using grinding or polishing belts; Accessories therefor for grinding other surfaces of particular shape
    • B24B21/165Machines or devices using grinding or polishing belts; Accessories therefor for grinding other surfaces of particular shape for vanes or blades of turbines, propellers, impellers, compressors and the like

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)

Abstract

719,124. Grinding turbine blades. JAMESON, J. L. Dec. 10, 1952, [Dec. 12, 1951.] No. 31303/52. Class 60. A machine for finishing the surface of a turbine blade 3 comprises a blade holder 90, Fig. 2, a die 2, means to move an abrasive band 4 between the blade and the die and fluid-pressure operated mechanism to effect relative member between the latter two members firstly at one rate until they reach a position with their surfaces close to one another and then at a reduced rate which is maintained throughout the finishing operation. In the preferred embodiment, the holder 90 is secured to a movable hydraulic cylinder 91 sliding on a stationary piston 92, Fig. 5. The cycle of operations is initiated by closing a switch 96 to displace a solenoid operated valve 122 which connects a line 95 to a pump 99 through a line 98<SP>1</SP> so that the cylinder 91 moves down quickly. Exhaust from the upper side of the cylinder takes place through a line 94, a valve 109 in a regulating unit 119 and a line 112 which is connected with a discharge line 113 through the valve 122. This action continues until a cam block 107 adjustably mounted on the cylinder 91 closes a micro-switch 108 to displace a solenoid operated valve 104 which permits fluid from the pump 99 to close the valve 109. The cylinder 91 now exhausts through an adjustable needle valve 110 so that its rate of movement is reduced during the abrading operation. The movement of the cylinder 91 is reversed when a second adjustably mounted cam block 114 opens a second micro-switch 115 to operate the valve 122 which connects the line 95 to the discharge line 113 and the line 112 to the pump 99. Fluid from the pump passing through the line 112 opens a valve 117 and hence bypasses the valve 110. A self-recuperating dashpot 126 having a plunger 123 for engagement by a lug 133 on the cylinder 91 cushions the final part of the rapid downward movement of the latter. The abrasive band 4, Fig. 2, passes over guide rollers 4<SP>1</SP> and is trapped between a roller 4<SP>2</SP> and a driven band 4<SP>4</SP> by which it is driven. Convex and concave blade surfaces can be finished and a guide 4<SP>3</SP> is arranged to exert sufficient drag on the abrasive band to provide a slack portion which can be pressed into the concavity of the die block when convex surfaces are being treated. The blade 3, Fig. 7, has one end located in a socket 136 and its other end held by a screw operated releasable swinging clamp 137. A jet 130 delivers oil to the band. Specification 591,890 is referred to.
GB31303/52A 1951-12-12 1952-12-10 A new or improved apparatus for finishing surfaces of turbine type blades Expired GB719124A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US719124XA 1951-12-12 1951-12-12

Publications (1)

Publication Number Publication Date
GB719124A true GB719124A (en) 1954-11-24

Family

ID=22104396

Family Applications (1)

Application Number Title Priority Date Filing Date
GB31303/52A Expired GB719124A (en) 1951-12-12 1952-12-10 A new or improved apparatus for finishing surfaces of turbine type blades

Country Status (1)

Country Link
GB (1) GB719124A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2156715A (en) * 1984-03-14 1985-10-16 Amada Co Ltd Abrading machine
CN113579949A (en) * 2021-09-28 2021-11-02 湖南致用科技有限公司 Polishing machine tool for polishing multidimensional welding points

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2156715A (en) * 1984-03-14 1985-10-16 Amada Co Ltd Abrading machine
CN113579949A (en) * 2021-09-28 2021-11-02 湖南致用科技有限公司 Polishing machine tool for polishing multidimensional welding points

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