GB1089297A - Bladed rotors particularly for engine cooling fans,air turbines and aircraft propellers - Google Patents
Bladed rotors particularly for engine cooling fans,air turbines and aircraft propellersInfo
- Publication number
- GB1089297A GB1089297A GB38704/63A GB3870463A GB1089297A GB 1089297 A GB1089297 A GB 1089297A GB 38704/63 A GB38704/63 A GB 38704/63A GB 3870463 A GB3870463 A GB 3870463A GB 1089297 A GB1089297 A GB 1089297A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- engine cooling
- cooling fans
- bladed rotors
- air turbines
- 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
- 238000001816 cooling Methods 0.000 title 1
- 230000002787 reinforcement Effects 0.000 abstract 3
- 238000001746 injection moulding Methods 0.000 abstract 2
- 229910000639 Spring steel Inorganic materials 0.000 abstract 1
- 229910000831 Steel Inorganic materials 0.000 abstract 1
- 239000000463 material Substances 0.000 abstract 1
- 238000000465 moulding Methods 0.000 abstract 1
- 229920003023 plastic Polymers 0.000 abstract 1
- 239000004033 plastic Substances 0.000 abstract 1
- 239000010959 steel Substances 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D7/00—Controlling wind motors
- F03D7/02—Controlling wind motors the wind motors having rotation axis substantially parallel to the air flow entering the rotor
- F03D7/022—Adjusting aerodynamic properties of the blades
- F03D7/0224—Adjusting blade pitch
-
- 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
- B64C11/30—Blade pitch-changing mechanisms
- B64C11/32—Blade pitch-changing mechanisms mechanical
- B64C11/34—Blade pitch-changing mechanisms mechanical automatic
- B64C11/346—Blade pitch-changing mechanisms mechanical automatic actuated by the centrifugal force or the aerodynamic drag acting on auxiliary masses or surfaces
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P7/00—Controlling of coolant flow
- F01P7/02—Controlling of coolant flow the coolant being cooling-air
- F01P7/06—Controlling of coolant flow the coolant being cooling-air by varying blade pitch
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/325—Rotors specially for elastic fluids for axial flow pumps for axial flow fans
- F04D29/329—Details of the hub
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/38—Blades
- F04D29/382—Flexible blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2260/00—Function
- F05B2260/70—Adjusting of angle of incidence or attack of rotating blades
- F05B2260/74—Adjusting of angle of incidence or attack of rotating blades by turning around an axis perpendicular the rotor centre line
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2260/00—Function
- F05B2260/70—Adjusting of angle of incidence or attack of rotating blades
- F05B2260/75—Adjusting of angle of incidence or attack of rotating blades the adjusting mechanism not using auxiliary power sources, e.g. servos
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2260/00—Function
- F05B2260/70—Adjusting of angle of incidence or attack of rotating blades
- F05B2260/77—Adjusting of angle of incidence or attack of rotating blades the adjusting mechanism driven or triggered by centrifugal forces
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
1,089,297. Injection moulding rotor; blades. DOWTY HYDRAULIC UNITS Ltd; Sept. 28, 1964 [Oct. 1, 1963], No.38704/63... Heading B5A [Also in Divisions B7 and F1] The rotor of a fan, air turbine or aircraft propeller comprises a steel hub structure 14, 15 and a reinforcement frame 19 within each rotor blade, the hub structure and reinforcement frames being encased in an integral hub cover and blade sheathing structure 21 of resilient plastics material formed by injection moulding. Each reinforcement frame 19, comprising bars 20 carried by a backbone member 18 of spring steel, is accurately located within the mould by an extension (not shown) of the member 18, the extensions being cut from the tips of the blades after moulding. Additional location may be provided by wires interconnecting the ends of the bars 20.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB38704/63A GB1089297A (en) | 1963-10-01 | 1963-10-01 | Bladed rotors particularly for engine cooling fans,air turbines and aircraft propellers |
US399623A US3260312A (en) | 1963-10-01 | 1964-09-28 | Bladed rotors |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB38704/63A GB1089297A (en) | 1963-10-01 | 1963-10-01 | Bladed rotors particularly for engine cooling fans,air turbines and aircraft propellers |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1089297A true GB1089297A (en) | 1967-11-01 |
Family
ID=10405181
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB38704/63A Expired GB1089297A (en) | 1963-10-01 | 1963-10-01 | Bladed rotors particularly for engine cooling fans,air turbines and aircraft propellers |
Country Status (2)
Country | Link |
---|---|
US (1) | US3260312A (en) |
GB (1) | GB1089297A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2226369A (en) * | 1988-11-21 | 1990-06-27 | Usui Kokusai Sangyo Kk | Variable pitch fan blade |
GB2303329A (en) * | 1995-07-19 | 1997-02-19 | Ventilatoren Sirocco Howden Bv | Fan blade manufacture by rotational moulding and a radial fan hub |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3642382A (en) * | 1969-05-11 | 1972-02-15 | Aisin Seiki | Fan assembly |
US3751181A (en) * | 1970-01-31 | 1973-08-07 | Aisin Seiki | Fan for cooling automotive vehicle engine |
BE763443A (en) * | 1970-03-12 | 1971-07-16 | Ryba Anton | FAN, IN PARTICULAR FOR COOLING SYSTEMS ON MOTOR VEHICLES |
US3953149A (en) * | 1974-06-17 | 1976-04-27 | General Motors Corporation | Engine cooling fan |
US4046489A (en) * | 1975-10-08 | 1977-09-06 | Eagle Motive Industries, Inc. | Aerodynamic fan blade |
CA1117924A (en) * | 1977-09-05 | 1982-02-09 | Aubrey H. Wagstaffe | Temperature-sensitive actuator and fan |
US4671739A (en) * | 1980-07-11 | 1987-06-09 | Robert W. Read | One piece molded fan |
US4636142A (en) * | 1984-05-11 | 1987-01-13 | Household Manufacturing, Inc. | Rotating fan apparatus |
US5110261A (en) * | 1990-07-05 | 1992-05-05 | Hunter Fan Company | Fan blade |
US20100122459A1 (en) * | 2008-11-17 | 2010-05-20 | General Electric Company | Method of making wind turbine blade |
CN102207103A (en) * | 2011-03-31 | 2011-10-05 | 深圳市顺合泰电机有限公司 | High-stability rotating fan blade and production method thereof |
US10294955B2 (en) * | 2016-04-19 | 2019-05-21 | Ge Global Sourcing Llc | Fan apparatus |
US11591084B2 (en) * | 2017-01-03 | 2023-02-28 | The Texas A&M University System | Cycloidal rotor micro-air vehicle |
CN106917764B (en) * | 2017-03-21 | 2020-09-25 | 联想(北京)有限公司 | Fan, manufacturing method thereof and electronic equipment |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1308527A (en) * | 1919-07-01 | ntlson | ||
GB124253A (en) * | 1918-03-13 | 1919-03-13 | James Adair Muirhead | Improvements in Propellors. |
US1463153A (en) * | 1920-10-09 | 1923-07-31 | Westinghouse Electric & Mfg Co | Fan structure |
US1757292A (en) * | 1921-11-03 | 1930-05-06 | Frank W Caldwell | Cooling fan |
GB193827A (en) * | 1922-02-23 | 1924-03-20 | Anton Flettner | Improvements relating to propellers, turbines and the like |
US2359265A (en) * | 1941-05-10 | 1944-09-26 | Everel Propeller Corp | Propeller |
US3033293A (en) * | 1958-10-20 | 1962-05-08 | Otto L Bihlmire | Boat propeller |
US3044557A (en) * | 1959-01-08 | 1962-07-17 | American Metal Prod | Variable pitch fan blade |
-
1963
- 1963-10-01 GB GB38704/63A patent/GB1089297A/en not_active Expired
-
1964
- 1964-09-28 US US399623A patent/US3260312A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2226369A (en) * | 1988-11-21 | 1990-06-27 | Usui Kokusai Sangyo Kk | Variable pitch fan blade |
GB2226369B (en) * | 1988-11-21 | 1992-12-23 | Usui Kokusai Sangyo Kk | Fan blade. |
GB2303329A (en) * | 1995-07-19 | 1997-02-19 | Ventilatoren Sirocco Howden Bv | Fan blade manufacture by rotational moulding and a radial fan hub |
Also Published As
Publication number | Publication date |
---|---|
US3260312A (en) | 1966-07-12 |
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