GB381899A - Improvements in or relating to means for the cooling of the vanes of rotors of rotary gas engines - Google Patents

Improvements in or relating to means for the cooling of the vanes of rotors of rotary gas engines

Info

Publication number
GB381899A
GB381899A GB15310/32A GB1531032A GB381899A GB 381899 A GB381899 A GB 381899A GB 15310/32 A GB15310/32 A GB 15310/32A GB 1531032 A GB1531032 A GB 1531032A GB 381899 A GB381899 A GB 381899A
Authority
GB
United Kingdom
Prior art keywords
rotors
vanes
relating
cooling
gas engines
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
GB15310/32A
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 GB381899A publication Critical patent/GB381899A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means
    • F01D5/085—Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

381,899. Turbines. PICKER, L., 38, Rue du M¶le, Geneva, Switzerland. May 30, 1932, No. 15310. Convention date, May 30, 1931. [Class 110 (iii).] Gas turbine rotors are cooled by water which enters a drum 9 through a hollow shaft 14 and is ejected through the pipes 10 to the blades 3. The water escapes through a sleeve 16 and is forced by a centrifugal pump 19 through a passage 21 to the turbine casing 23 which it cools before escaping by an outlet 24. The pump is mounted on the turbine shaft.
GB15310/32A 1931-05-30 1932-05-30 Improvements in or relating to means for the cooling of the vanes of rotors of rotary gas engines Expired GB381899A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE381899X 1931-05-30

Publications (1)

Publication Number Publication Date
GB381899A true GB381899A (en) 1932-10-13

Family

ID=6355820

Family Applications (1)

Application Number Title Priority Date Filing Date
GB15310/32A Expired GB381899A (en) 1931-05-30 1932-05-30 Improvements in or relating to means for the cooling of the vanes of rotors of rotary gas engines

Country Status (1)

Country Link
GB (1) GB381899A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2554368A (en) * 1944-08-23 1951-05-22 United Aircraft Corp Turbine rotor cooling
GB2278646A (en) * 1993-03-01 1994-12-07 Howard Bidwell Turbine using i.c. engine exhaust gas

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2554368A (en) * 1944-08-23 1951-05-22 United Aircraft Corp Turbine rotor cooling
GB2278646A (en) * 1993-03-01 1994-12-07 Howard Bidwell Turbine using i.c. engine exhaust gas

Similar Documents

Publication Publication Date Title
GB609926A (en) Improvements in or relating to internal-combustion turbines
GB666536A (en) Stator blades for a gas turbine
GB511597A (en) Improvements in or relating to gas turbine driven blowers
GB381899A (en) Improvements in or relating to means for the cooling of the vanes of rotors of rotary gas engines
GB693727A (en) Improvements relating to bladed rotary fluid-flow machines
GB577017A (en) Improvements in turbines
GB742288A (en) Improvements in the cooling of turbines
GB252424A (en) An improved water turbine
GB702740A (en) Improvements in or relating to bladed rotors for axial flow turbines and similarly bladed fluid flow machines
GB544909A (en) High speed propulsion plant
GB586551A (en) Improvements in or relating to internal combustion power turbine plant for propulsion in air
GB624777A (en) Improvements in or relating to stator casings for compressors and like machines
GB373940A (en) Improvements in and relating to turbines
GB448026A (en) Improvements in and relating to centrifugal machines with hollow impellers
GB463390A (en) Improvements in and relating to elastic fluid turbines
GB502414A (en) Improvements in turbines
GB740944A (en) Improvements in and relating to thermal turbines
GB412006A (en) Improvements in rotary engines
GB586553A (en) Improvements in or relating to turbines
GB415986A (en) Improvements in and relating to turbo-generators
GB679467A (en) Improvements in gas turbines
GB432652A (en) Improved constant pressure gas turbine plant
GB314156A (en) Improvements in turbines
GB347766A (en) Improvements relating to centrifugal compressors and pumps
GB492645A (en) Improvements in two-stage screw impeller fans