GB2073631B - Blade twisting - Google Patents
Blade twistingInfo
- Publication number
- GB2073631B GB2073631B GB8012314A GB8012314A GB2073631B GB 2073631 B GB2073631 B GB 2073631B GB 8012314 A GB8012314 A GB 8012314A GB 8012314 A GB8012314 A GB 8012314A GB 2073631 B GB2073631 B GB 2073631B
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade twisting
- twisting
- blade
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D11/00—Bending not restricted to forms of material mentioned in only one of groups B21D5/00, B21D7/00, B21D9/00; Bending not provided for in groups B21D5/00 - B21D9/00; Twisting
- B21D11/14—Twisting
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8012314A GB2073631B (en) | 1980-04-15 | 1980-04-15 | Blade twisting |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8012314A GB2073631B (en) | 1980-04-15 | 1980-04-15 | Blade twisting |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2073631A GB2073631A (en) | 1981-10-21 |
GB2073631B true GB2073631B (en) | 1984-12-19 |
Family
ID=10512787
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8012314A Expired GB2073631B (en) | 1980-04-15 | 1980-04-15 | Blade twisting |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2073631B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11852035B2 (en) | 2019-05-07 | 2023-12-26 | Rtx Corporation | Multi-cover gas turbine engine component |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4841614A (en) * | 1988-02-12 | 1989-06-27 | United Technologies Corporation | Method for fabricating integrally bladed rotors |
DE69101246T2 (en) * | 1990-03-22 | 1994-09-22 | United Technologies Corp | Process for forming hollow blades. |
US5479705A (en) * | 1992-05-01 | 1996-01-02 | Rolls-Royce Plc | Method of manufacturing an article by superplastic forming and diffusion bonding |
GB9209464D0 (en) * | 1992-05-01 | 1992-06-17 | Rolls Royce Plc | A method of manufacturing an article by superplastic forming and diffusion bonding |
FR2752539B1 (en) * | 1996-08-22 | 1998-09-18 | Snecma | PROCESS FOR MANUFACTURING A HOLLOW BLADE OF A TURBOMACHINE AND HOT-SCALABLE TURNING EQUIPMENT |
GB0001753D0 (en) * | 2000-01-27 | 2000-03-15 | Sermatech Repair Services Limi | Thermal processing apparatus and method |
GB0117066D0 (en) | 2001-07-12 | 2001-09-05 | Bae Systems Plc | Creep forming a metallic compound |
JP4786077B2 (en) * | 2001-08-10 | 2011-10-05 | 本田技研工業株式会社 | Turbine vane and method for manufacturing the same |
JP4028442B2 (en) | 2002-06-26 | 2007-12-26 | 株式会社東芝 | Apparatus and method for correcting deformation of gas turbine blade |
GB0915949D0 (en) | 2009-09-11 | 2009-10-28 | Rolls Royce Plc | A die former |
GB201117183D0 (en) | 2011-10-06 | 2011-11-16 | Rolls Royce Plc | Method and equipment for shaping a cast component |
JP5702710B2 (en) * | 2011-12-21 | 2015-04-15 | 株式会社日立製作所 | Free forging method and forging apparatus |
RU2555274C1 (en) | 2013-12-12 | 2015-07-10 | Федеральное государственное бюджетное учреждение науки Институт проблем сверхпластичности металлов Российской академии наук (ИПСМ РАН) | Method of manufacturing of hollow fan blade |
US11014190B2 (en) | 2019-01-08 | 2021-05-25 | Raytheon Technologies Corporation | Hollow airfoil with catenary profiles |
US10808542B2 (en) | 2019-01-11 | 2020-10-20 | Raytheon Technologies Corporation | Method of forming gas turbine engine components |
US10995632B2 (en) | 2019-03-11 | 2021-05-04 | Raytheon Technologies Corporation | Damped airfoil for a gas turbine engine |
US11033993B2 (en) | 2019-03-20 | 2021-06-15 | Raytheon Technologies Corporation | Method of forming gas turbine engine components |
US11370016B2 (en) | 2019-05-23 | 2022-06-28 | Raytheon Technologies Corporation | Assembly and method of forming gas turbine engine components |
US11174737B2 (en) | 2019-06-12 | 2021-11-16 | Raytheon Technologies Corporation | Airfoil with cover for gas turbine engine |
US11248477B2 (en) | 2019-08-02 | 2022-02-15 | Raytheon Technologies Corporation | Hybridized airfoil for a gas turbine engine |
US11148221B2 (en) | 2019-08-29 | 2021-10-19 | Raytheon Technologies Corporation | Method of forming gas turbine engine components |
US11379629B2 (en) | 2020-02-21 | 2022-07-05 | Raytheon Technologies Corporation | System and process for designing internal components for a gas turbine engine |
CN111451339A (en) * | 2020-05-18 | 2020-07-28 | 淮安信息职业技术学院 | Eccentric connecting rod torsion device |
CN113976699B (en) * | 2021-10-18 | 2023-05-23 | 中国航发沈阳黎明航空发动机有限责任公司 | Titanium alloy hollow blade forming method based on constant strain rate torsion |
CN114798860B (en) * | 2022-04-19 | 2024-03-22 | 谭美珍 | Twisting device for hardware part machining |
-
1980
- 1980-04-15 GB GB8012314A patent/GB2073631B/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11852035B2 (en) | 2019-05-07 | 2023-12-26 | Rtx Corporation | Multi-cover gas turbine engine component |
Also Published As
Publication number | Publication date |
---|---|
GB2073631A (en) | 1981-10-21 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19960415 |