GB2077364B - Wafer tip cap for rotor blades - Google Patents

Wafer tip cap for rotor blades

Info

Publication number
GB2077364B
GB2077364B GB8116712A GB8116712A GB2077364B GB 2077364 B GB2077364 B GB 2077364B GB 8116712 A GB8116712 A GB 8116712A GB 8116712 A GB8116712 A GB 8116712A GB 2077364 B GB2077364 B GB 2077364B
Authority
GB
United Kingdom
Prior art keywords
rotor blades
tip cap
wafer tip
wafer
cap
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
GB8116712A
Other versions
GB2077364A (en
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of GB2077364A publication Critical patent/GB2077364A/en
Application granted granted Critical
Publication of GB2077364B publication Critical patent/GB2077364B/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187Convection cooling
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
GB8116712A 1980-06-05 1981-06-01 Wafer tip cap for rotor blades Expired GB2077364B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US15654980A 1980-06-05 1980-06-05

Publications (2)

Publication Number Publication Date
GB2077364A GB2077364A (en) 1981-12-16
GB2077364B true GB2077364B (en) 1983-10-26

Family

ID=22560030

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8116712A Expired GB2077364B (en) 1980-06-05 1981-06-01 Wafer tip cap for rotor blades

Country Status (8)

Country Link
JP (1) JPS5728803A (en)
BE (1) BE889078A (en)
DE (1) DE3122485A1 (en)
FR (1) FR2484015A1 (en)
GB (1) GB2077364B (en)
IL (1) IL63012A (en)
NO (1) NO811831L (en)
SE (1) SE8103503L (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4411597A (en) * 1981-03-20 1983-10-25 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Tip cap for a rotor blade
FR2689176B1 (en) * 1992-03-25 1995-07-13 Snecma DAWN REFRIGERATED FROM TURBO-MACHINE.
US5476364A (en) * 1992-10-27 1995-12-19 United Technologies Corporation Tip seal and anti-contamination for turbine blades
JP2955252B2 (en) * 1997-06-26 1999-10-04 三菱重工業株式会社 Gas turbine blade tip shroud

Also Published As

Publication number Publication date
NO811831L (en) 1981-12-07
FR2484015A1 (en) 1981-12-11
GB2077364A (en) 1981-12-16
JPS5728803A (en) 1982-02-16
SE8103503L (en) 1981-12-06
IL63012A0 (en) 1981-09-13
IL63012A (en) 1984-10-31
DE3122485A1 (en) 1982-04-15
BE889078A (en) 1981-10-01

Similar Documents

Publication Publication Date Title
GB2067493B (en) Helicopter rotor blade tip
IL65240A (en) Tip cap for a rotor blade
GB2114676B (en) Turbine rotor blade
GB2111131B (en) An improved tip structure for cooled turbine rotor blade
GB8308295D0 (en) Turbine blade
GB2158160B (en) Rotor blade tip
JPS57181904A (en) Blade for turbine
GB2027495B (en) Turbine blade
GB2102505B (en) Airfoil blade
JPS5591499A (en) Rotor for helicopter
JPS5631897A (en) Blade form for rotor blade
GB8302209D0 (en) Rotor blades
JPS56131496A (en) Rotor for helicopter
GB2108534B (en) Forming braze-bonded abrasive turbine blade tip
GB2100809B (en) Root formation for rotor blade
JPS5762903A (en) Turbine blade
JPS56149296A (en) Blade having high performance for helicopter rotor
GB2119863B (en) Turbine rotor
GB2015658B (en) Turbine blade
AU568313B2 (en) Turbine blade
JPS56149297A (en) Rotor blade for helicopter
JPS5728802A (en) Rotor blade
JPS5787797A (en) Rotor for helicopter
JPS54115900A (en) Rotor blade espectally for rotor blade aircraft
GB2077364B (en) Wafer tip cap for rotor blades

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee