GB1207543A - Cooled seal - Google Patents

Cooled seal

Info

Publication number
GB1207543A
GB1207543A GB1053668A GB1053668A GB1207543A GB 1207543 A GB1207543 A GB 1207543A GB 1053668 A GB1053668 A GB 1053668A GB 1053668 A GB1053668 A GB 1053668A GB 1207543 A GB1207543 A GB 1207543A
Authority
GB
United Kingdom
Prior art keywords
seal member
packing
cooling air
passages
laminμ
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
GB1053668A
Inventor
Robert Leon Allen
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.)
Motors Liquidation Co
Original Assignee
Motors Liquidation Co
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 Motors Liquidation Co filed Critical Motors Liquidation Co
Priority to GB1053668A priority Critical patent/GB1207543A/en
Publication of GB1207543A publication Critical patent/GB1207543A/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
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J15/00Sealings
    • F16J15/44Free-space packings
    • F16J15/444Free-space packings with facing materials having honeycomb-like structure

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

1,207,543. Seals. GENERAL MOTORS CORP. 5 March, 1968, No. 10536/68. Heading F2B. [Also in Division F1] A seal member 28 for a gas turbine labyrinth packing comprises two or more perforated metal laminµ bonded together with the perforations overlapping to form passages for flow of fluid. As shown, three perforated sheet metal laminµ are employed and cooling air is fed to a space 35 above the packing through hollow nozzle vanes 9 and holes 31 in the inner shroud 18. The cooling air is then metered through the passages in the seal member 28 and into the gap between the seal member and a labyrinth member 17. The seal member 28 may be made by photo-etching and diffusion bonding and, if desired, the passages may be calibrated or provided only towards the high pressure edge of the packing. The cooling air may also serve as a barrier against the passage of gas through the packing.
GB1053668A 1968-03-05 1968-03-05 Cooled seal Expired GB1207543A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1053668A GB1207543A (en) 1968-03-05 1968-03-05 Cooled seal

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1053668A GB1207543A (en) 1968-03-05 1968-03-05 Cooled seal

Publications (1)

Publication Number Publication Date
GB1207543A true GB1207543A (en) 1970-10-07

Family

ID=9969637

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1053668A Expired GB1207543A (en) 1968-03-05 1968-03-05 Cooled seal

Country Status (1)

Country Link
GB (1) GB1207543A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3514392A1 (en) * 1984-04-27 1985-11-07 General Electric Co., Schenectady, N.Y. ROTARY SEAL

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3514392A1 (en) * 1984-04-27 1985-11-07 General Electric Co., Schenectady, N.Y. ROTARY SEAL

Similar Documents

Publication Publication Date Title
GB1271819A (en) Improvements in film cooling of structural members in gas turbine engines
GB1464389A (en) Rotor vane
GB1125920A (en) Turbomachine rotors
GB1438229A (en) Porous sheet adapted to be cooled by fluid flow
GB1256040A (en) Hollow sheet metal turbine blades
GB1276377A (en) Gas turbine engine with improved gas seal
GB590420A (en) Improvements in and relating to gas turbines
GB1493913A (en) Turbomachine stator interstage seal
GB1525746A (en) Gas turbine engines including labyrinth seals
GB1225926A (en)
GB1342663A (en) Steam turbine stage
GB1081458A (en) Blade assembly for a fluid flow machine such as a gas turbine engine
GB1267317A (en) Transpiration cooling
ES8200502A1 (en) Jet pump with labyrinth seal
GB1484951A (en) Cooling system for a gas turbine engine
GB1282250A (en) Laminated high temperature resistant materials
GB1438379A (en) Cooling arrangement for duct walls
GB1386590A (en) Turbine rotor
GB1257746A (en)
GB1324790A (en) Gas turbine engine compressors
GB1457634A (en) Converging-diverging supersonic nozzles
GB1152331A (en) Improvements in Gas Turbine Blade Cooling
GB1314927A (en) Seals in aerodynamic pressure-wave machines
GB1285369A (en) Improvements in or relating to blades for fluid flow machines
GB1262690A (en) Improvements in fluid handling apparatus and sealing means therefor

Legal Events

Date Code Title Description
PS Patent sealed
PE20 Patent expired after termination of 20 years