GB1361256A – Gas turbine engine blades
– Google Patents
GB1361256A – Gas turbine engine blades
– Google Patents
Gas turbine engine blades
Info
Publication number
GB1361256A
GB1361256A
GB3977871A
GB3977871A
GB1361256A
GB 1361256 A
GB1361256 A
GB 1361256A
GB 3977871 A
GB3977871 A
GB 3977871A
GB 3977871 A
GB3977871 A
GB 3977871A
GB 1361256 A
GB1361256 A
GB 1361256A
Authority
GB
United Kingdom
Prior art keywords
holes
insert
blade
coolant
fins
Prior art date
1971-08-25
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
GB3977871A
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.)
1971-08-25
Filing date
1971-08-25
Publication date
1974-07-24
1971-08-25
Application filed by Rolls Royce PLC
filed
Critical
Rolls Royce PLC
1971-08-25
Priority to GB3977871A
priority
Critical
patent/GB1361256A/en
1972-08-22
Priority to US00282779A
priority
patent/US3782852A/en
1972-08-22
Priority to DE2241192A
priority
patent/DE2241192C3/en
1972-08-22
Priority to US00282778A
priority
patent/US3806274A/en
1972-08-23
Priority to AU45872/72A
priority
patent/AU467301B2/en
1972-08-24
Priority to SE7210988A
priority
patent/SE378645B/xx
1972-08-24
Priority to FR7230138A
priority
patent/FR2150476B1/fr
1972-08-24
Priority to IT5233772A
priority
patent/IT962212B/en
1972-08-25
Priority to JP8465972A
priority
patent/JPS5310206B2/ja
1974-07-24
Publication of GB1361256A
publication
Critical
patent/GB1361256A/en
Status
Expired
legal-status
Critical
Current
Links
Espacenet
Global Dossier
Discuss
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
F01D5/12—Blades
F01D5/14—Form or construction
F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
F01D5/187—Convection cooling
F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
Abstract
1361256 Gas turbine blades ROLLS-ROYCE (1971) Ltd 25 Aug 1972 [25 Aug 1971] 39778/71 Heading FIT A hollow gas turbine blade contains a doublewalled insert 14 which is spaced from the blade walls 17, 18 but inclined fins 15 defining inflow and outflow regions for coolant fluid. The latter, e.g. liquid, air or other gas, may be supplied at the blade root end 13 and flows longitudinally part pimples 16. Some coolant discharges through leading edge film cooling holes 24 whilst the remainder enters the open forward end 22 of insert 14 and flows chord-wise over spacers 21 to leave the insert through holes or slots 23 and enter the outflow region 27 rearward of fins 15. Pedestals 19 are provided in region 27. Coolant leaves the latter through trailing edge holes 25, when provided, or at the blade tip 12. Bleed holes may be provided in the root end of fins 15 to allow a small amount of coolant to flow directly to region 27 without passing through insert 14. Inclined fins may be provided instead of or in addition to pimples 16. The forward edge of insert 14 may be closed and provided with holes analogous to holes 23. The blade may be for a rotor or stator.
GB3977871A
1971-08-25
1971-08-25
Gas turbine engine blades
Expired
GB1361256A
(en)
Priority Applications (9)
Application Number
Priority Date
Filing Date
Title
GB3977871A
GB1361256A
(en)
1971-08-25
1971-08-25
Gas turbine engine blades
US00282779A
US3782852A
(en)
1971-08-25
1972-08-22
Gas turbine engine blades
DE2241192A
DE2241192C3
(en)
1971-08-25
1972-08-22
Hollow gas turbine blade
US00282778A
US3806274A
(en)
1971-08-25
1972-08-22
Gas turbine engine blades
AU45872/72A
AU467301B2
(en)
1971-08-25
1972-08-23
Gas turbine engine blades
SE7210988A
SE378645B
(en)
1971-08-25
1972-08-24
FR7230138A
FR2150476B1
(en)
1971-08-25
1972-08-24
IT5233772A
IT962212B
(en)
1971-08-25
1972-08-24
IMPROVEMENT IN ROTORS FOR GAS TURBINES
JP8465972A
JPS5310206B2
(en)
1971-08-25
1972-08-25
Applications Claiming Priority (2)
Application Number
Priority Date
Filing Date
Title
GB3977871A
GB1361256A
(en)
1971-08-25
1971-08-25
Gas turbine engine blades
US28277972A
1972-08-22
1972-08-22
Publications (1)
Publication Number
Publication Date
GB1361256A
true
GB1361256A
(en)
1974-07-24
Family
ID=26264234
Family Applications (1)
Application Number
Title
Priority Date
Filing Date
GB3977871A
Expired
GB1361256A
(en)
1971-08-25
1971-08-25
Gas turbine engine blades
Country Status (6)
Country
Link
US
(2)
US3806274A
(en)
AU
(1)
AU467301B2
(en)
DE
(1)
DE2241192C3
(en)
FR
(1)
FR2150476B1
(en)
GB
(1)
GB1361256A
(en)
SE
(1)
SE378645B
(en)
Families Citing this family (33)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
GB1400285A
(en)
*
1972-08-02
1975-07-16
Rolls Royce
Hollow cooled vane or blade for a gas turbine engine
US3902820A
(en)
*
1973-07-02
1975-09-02
Westinghouse Electric Corp
Fluid cooled turbine rotor blade
US4153386A
(en)
*
1974-12-11
1979-05-08
United Technologies Corporation
Air cooled turbine vanes
NL7802688A
(en)
*
1978-03-13
1979-09-17
Philips Nv
DEVICE FOR CONVERSION FROM ACOUSTIC TO ELECTRICAL VIBRATIONS AND VERSIONS, EQUIPPED WITH AT LEAST ONE CONDENSER ELECTRICAL ELEMENT CONNECTED TO AN ELECTRONIC CIRCUIT.
US4278400A
(en)
*
1978-09-05
1981-07-14
United Technologies Corporation
Coolable rotor blade
FR2468727A1
(en)
*
1979-10-26
1981-05-08
Snecma
IMPROVEMENT TO COOLED TURBINE AUBES
FR2473621A1
(en)
*
1980-01-10
1981-07-17
Snecma
DAWN OF TURBINE DISPENSER
US4515526A
(en)
*
1981-12-28
1985-05-07
United Technologies Corporation
Coolable airfoil for a rotary machine
US5232343A
(en)
*
1984-05-24
1993-08-03
General Electric Company
Turbine blade
GB2189553B
(en)
*
1986-04-25
1990-05-23
Rolls Royce
Cooled vane
US5097660A
(en)
*
1988-12-28
1992-03-24
Sundstrand Corporation
Coanda effect turbine nozzle vane cooling
US5022817A
(en)
*
1989-09-12
1991-06-11
Allied-Signal Inc.
Thermostatic control of turbine cooling air
US5279111A
(en)
*
1992-08-27
1994-01-18
Inco Limited
Gas turbine cooling
DE19634238A1
(en)
*
1996-08-23
1998-02-26
Asea Brown Boveri
Coolable shovel
JPH10266803A
(en)
*
1997-03-25
1998-10-06
Mitsubishi Heavy Ind Ltd
Gas turbine cooling moving blade
DE59709275D1
(en)
*
1997-07-14
2003-03-13
Alstom Switzerland Ltd
Cooling system for the trailing edge area of a hollow gas turbine blade
SE512384C2
(en)
1998-05-25
2000-03-06
Abb Ab
Component for a gas turbine
DE59808481D1
(en)
*
1998-11-09
2003-06-26
Alstom Switzerland Ltd
Cooled components with conical cooling channels
DE19860787B4
(en)
*
1998-12-30
2007-02-22
Alstom
Turbine blade with cooling channels
US6955525B2
(en)
*
2003-08-08
2005-10-18
Siemens Westinghouse Power Corporation
Cooling system for an outer wall of a turbine blade
SE526847C2
(en)
*
2004-02-27
2005-11-08
Demag Delaval Ind Turbomachine
A component comprising a guide rail or a rotor blade for a gas turbine
EP1847684A1
(en)
*
2006-04-21
2007-10-24
Siemens Aktiengesellschaft
Turbine blade
US7497655B1
(en)
*
2006-08-21
2009-03-03
Florida Turbine Technologies, Inc.
Turbine airfoil with near-wall impingement and vortex cooling
US7563072B1
(en)
2006-09-25
2009-07-21
Florida Turbine Technologies, Inc.
Turbine airfoil with near-wall spiral flow cooling circuit
US7722326B2
(en)
*
2007-03-13
2010-05-25
Siemens Energy, Inc.
Intensively cooled trailing edge of thin airfoils for turbine engines
US8636463B2
(en)
*
2010-03-31
2014-01-28
General Electric Company
Interior cooling channels
EP2378073A1
(en)
*
2010-04-14
2011-10-19
Siemens Aktiengesellschaft
Blade or vane for a turbomachine
US9228439B2
(en)
2012-09-28
2016-01-05
Solar Turbines Incorporated
Cooled turbine blade with leading edge flow redirection and diffusion
US9206695B2
(en)
*
2012-09-28
2015-12-08
Solar Turbines Incorporated
Cooled turbine blade with trailing edge flow metering
US9314838B2
(en)
2012-09-28
2016-04-19
Solar Turbines Incorporated
Method of manufacturing a cooled turbine blade with dense cooling fin array
US10443407B2
(en)
*
2016-02-15
2019-10-15
General Electric Company
Accelerator insert for a gas turbine engine airfoil
US10641103B2
(en)
2017-01-19
2020-05-05
United Technologies Corporation
Trailing edge configuration with cast slots and drilled filmholes
US10822963B2
(en)
*
2018-12-05
2020-11-03
Raytheon Technologies Corporation
Axial flow cooling scheme with castable structural rib for a gas turbine engine
Family Cites Families (10)
* Cited by examiner, † Cited by third party
Publication number
Priority date
Publication date
Assignee
Title
DE853534C
(en)
*
1943-02-27
1952-10-27
Maschf Augsburg Nuernberg Ag
Air-cooled gas turbine blade
US2888243A
(en)
*
1956-10-22
1959-05-26
Pollock Robert Stephen
Cooled turbine blade
US3057597A
(en)
*
1959-08-20
1962-10-09
Jr Andre J Meyer
Modification and improvements to cooled blades
US3370829A
(en)
*
1965-12-20
1968-02-27
Avco Corp
Gas turbine blade construction
US3540810A
(en)
*
1966-03-17
1970-11-17
Gen Electric
Slanted partition for hollow airfoil vane insert
US3560107A
(en)
*
1968-09-25
1971-02-02
Gen Motors Corp
Cooled airfoil
US3527544A
(en)
*
1968-12-12
1970-09-08
Gen Motors Corp
Cooled blade shroud
US3606574A
(en)
*
1969-10-23
1971-09-20
Gen Electric
Cooled shrouded turbine blade
BE755567A
(en)
*
1969-12-01
1971-02-15
Gen Electric
FIXED VANE STRUCTURE, FOR GAS TURBINE ENGINE AND ASSOCIATED TEMPERATURE ADJUSTMENT ARRANGEMENT
US3635587A
(en)
*
1970-06-02
1972-01-18
Gen Motors Corp
Blade cooling liner
1971
1971-08-25
GB
GB3977871A
patent/GB1361256A/en
not_active
Expired
1972
1972-08-22
US
US00282778A
patent/US3806274A/en
not_active
Expired – Lifetime
1972-08-22
DE
DE2241192A
patent/DE2241192C3/en
not_active
Expired
1972-08-22
US
US00282779A
patent/US3782852A/en
not_active
Expired – Lifetime
1972-08-23
AU
AU45872/72A
patent/AU467301B2/en
not_active
Expired
1972-08-24
SE
SE7210988A
patent/SE378645B/xx
unknown
1972-08-24
FR
FR7230138A
patent/FR2150476B1/fr
not_active
Expired
Also Published As
Publication number
Publication date
AU467301B2
(en)
1975-11-27
DE2241192B2
(en)
1977-07-21
AU4587272A
(en)
1974-03-07
SE378645B
(en)
1975-09-08
DE2241192C3
(en)
1978-03-09
FR2150476A1
(en)
1973-04-06
FR2150476B1
(en)
1979-04-06
US3782852A
(en)
1974-01-01
US3806274A
(en)
1974-04-23
DE2241192A1
(en)
1973-03-08
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Legal Events
Date
Code
Title
Description
1974-12-04
PS
Patent sealed [section 19, patents act 1949]
1983-03-30
PCNP
Patent ceased through non-payment of renewal fee
