GB786467A - Improvements in or relating to flexible couplings - Google Patents
Improvements in or relating to flexible couplingsInfo
- Publication number
- GB786467A GB786467A GB36008/55A GB3600855A GB786467A GB 786467 A GB786467 A GB 786467A GB 36008/55 A GB36008/55 A GB 36008/55A GB 3600855 A GB3600855 A GB 3600855A GB 786467 A GB786467 A GB 786467A
- Authority
- GB
- United Kingdom
- Prior art keywords
- discs
- sleeves
- shafts
- dec
- axial thrust
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D3/00—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
786,467. Universal joints. GENERAL MOTORS CORPORATION. Dec. 15, 1955 [Dec. 21, 1954], No. 36008/55. Class 80 (2). A coupling adapted to allow of slight angular misalignment and to transmit axial thrust is particularly applicable to the connection of the turbine rotor shaft 26 of a gas turbine engine to the compressor shaft 18. The coupling comprises a sleeve 40 in splined connection at 42 and 44 with the shafts 18 and 26 respectively for the transmission of torque and a series of interfitting flexible spring discs 66, 68, 70, 72 and 74 located between sleeves 46 and 62 for transmitting axial thrust. The spring discs interfit by means of annular grooves and flanges and the end discs engage radial flanges 64 and 96 on the sleeves 62 and 46, these sleeves being secured to shafts 26 and 18 respectively. The arrangement of spring discs prevent relative lateral movement and consequently relative axial displacement of the two shafts, but allows a slight angular displacement provided by the flexing of the discs.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US786467XA | 1954-12-21 | 1954-12-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB786467A true GB786467A (en) | 1957-11-20 |
Family
ID=22145383
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB36008/55A Expired GB786467A (en) | 1954-12-21 | 1955-12-15 | Improvements in or relating to flexible couplings |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB786467A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102014114473A1 (en) * | 2014-10-06 | 2016-04-07 | Rolls-Royce Deutschland Ltd & Co Kg | Gas turbine with at least two coaxial with each other and at least partially formed as hollow shafts waves |
-
1955
- 1955-12-15 GB GB36008/55A patent/GB786467A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102014114473A1 (en) * | 2014-10-06 | 2016-04-07 | Rolls-Royce Deutschland Ltd & Co Kg | Gas turbine with at least two coaxial with each other and at least partially formed as hollow shafts waves |
US10082037B2 (en) | 2014-10-06 | 2018-09-25 | Rolls-Royce Deutschland Ltd & Co Kg | Gas turbine having at least two shafts designed as hollow shafts at least in some areas and arranged coaxially relative to one another |
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