IT8921119A0 - Pale controrotanti per eliche di aeroplano. - Google Patents
Pale controrotanti per eliche di aeroplano.Info
- Publication number
- IT8921119A0 IT8921119A0 IT8921119A IT2111989A IT8921119A0 IT 8921119 A0 IT8921119 A0 IT 8921119A0 IT 8921119 A IT8921119 A IT 8921119A IT 2111989 A IT2111989 A IT 2111989A IT 8921119 A0 IT8921119 A0 IT 8921119A0
- Authority
- IT
- Italy
- Prior art keywords
- counter
- rotating blades
- airplane propellers
- propellers
- airplane
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/16—Blades
- B64C11/20—Constructional features
- B64C11/26—Fabricated blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US27056588A | 1988-11-14 | 1988-11-14 |
Publications (2)
Publication Number | Publication Date |
---|---|
IT8921119A0 true IT8921119A0 (it) | 1989-07-07 |
IT1230305B IT1230305B (it) | 1991-10-18 |
Family
ID=23031826
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT8921119A IT1230305B (it) | 1988-11-14 | 1989-07-07 | Pale controrotanti per eliche di aeroplano. |
Country Status (7)
Country | Link |
---|---|
JP (1) | JPH02155721A (it) |
CN (1) | CN1042692A (it) |
DE (1) | DE3922455A1 (it) |
FR (1) | FR2639021A1 (it) |
GB (1) | GB2224784A (it) |
IT (1) | IT1230305B (it) |
SE (1) | SE8903784L (it) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5042968A (en) * | 1989-11-02 | 1991-08-27 | United Technologies Corporation | Propeller blade subassembly and method for making a propeller blade subassembly |
GB2293631B (en) * | 1994-09-30 | 1998-09-09 | Gen Electric | Composite fan blade trailing edge reinforcement |
US6290895B1 (en) * | 1997-10-14 | 2001-09-18 | General Electric Company | Selectively flexible caul and method of use |
DE102005030939A1 (de) * | 2005-06-30 | 2007-01-04 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines im Wesentlichen schalenförmigen Bauteils |
GB2450936B (en) * | 2007-07-13 | 2010-01-20 | Rolls Royce Plc | Bladed rotor balancing |
FR2970943B1 (fr) | 2011-01-31 | 2014-02-28 | Eurocopter France | Pale et procede de fabrication de ladite pale |
CN104514785B (zh) * | 2013-09-30 | 2016-12-07 | 哈尔滨飞机工业集团有限责任公司 | 桨叶大调整片胶接方法 |
CN104655081A (zh) * | 2013-11-25 | 2015-05-27 | 中国直升机设计研究所 | 一种桨叶结构预扭角测量方法 |
US10710705B2 (en) * | 2017-06-28 | 2020-07-14 | General Electric Company | Open rotor and airfoil therefor |
CN109458901B (zh) * | 2018-12-07 | 2020-05-19 | 中国航发南方工业有限公司 | 一种叶片辅助测量底座制造装置 |
CN110815859B (zh) * | 2019-11-29 | 2022-03-29 | 株洲时代新材料科技股份有限公司 | 一种复合材料叶片的设计制造方法及其复合材料叶片 |
FR3124216B1 (fr) | 2021-06-21 | 2023-10-20 | Safran Aircraft Engines | Procédé d’equilibrage d’aubes de soufflante avec usinage du bord de fuite |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1038707B (de) * | 1957-07-20 | 1958-09-11 | Costa Vasiljevic Dr Ing | Verfahren zur Herstellung von Fluegeln fuer Kreiselraeder |
US3799701A (en) * | 1972-02-28 | 1974-03-26 | United Aircraft Corp | Composite fan blade and method of construction |
DE3738785A1 (de) * | 1986-11-19 | 1988-05-26 | Gen Electric | Gegenlaeufig rotierende flugzeug-antriebsschaufeln |
US4810167A (en) * | 1986-12-08 | 1989-03-07 | Hartzell Propeller Inc. | Composite aircraft propeller blade |
-
1989
- 1989-05-27 CN CN89103688.1A patent/CN1042692A/zh active Pending
- 1989-07-07 DE DE3922455A patent/DE3922455A1/de not_active Withdrawn
- 1989-07-07 IT IT8921119A patent/IT1230305B/it active
- 1989-07-10 GB GB8915764A patent/GB2224784A/en not_active Withdrawn
- 1989-07-11 FR FR8909286A patent/FR2639021A1/fr active Pending
- 1989-07-11 JP JP1177306A patent/JPH02155721A/ja active Pending
- 1989-11-10 SE SE8903784A patent/SE8903784L/ not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
SE8903784D0 (sv) | 1989-11-10 |
GB2224784A (en) | 1990-05-16 |
GB8915764D0 (en) | 1989-08-31 |
DE3922455A1 (de) | 1990-05-17 |
IT1230305B (it) | 1991-10-18 |
JPH02155721A (ja) | 1990-06-14 |
CN1042692A (zh) | 1990-06-06 |
SE8903784L (sv) | 1990-05-15 |
FR2639021A1 (fr) | 1990-05-18 |
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