GB1055165A - Improvements in or relating to engine cooling fans - Google Patents
Improvements in or relating to engine cooling fansInfo
- Publication number
- GB1055165A GB1055165A GB25164A GB25164A GB1055165A GB 1055165 A GB1055165 A GB 1055165A GB 25164 A GB25164 A GB 25164A GB 25164 A GB25164 A GB 25164A GB 1055165 A GB1055165 A GB 1055165A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade
- pitch
- blades
- plate
- hub
- 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
-
- 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
Abstract
1,055,165. Axial-flow fans; cooling cylinders. DOWTY HYDRAULIC UNITS Ltd. March 25, 1964 [April 11, 1963 (2); Jan. 2, 1964], Nos. 14621/63; 14622/63 and 251/64. Headings F1B and F1C. An engine-driven cooling fan has blades whose pitch is automatically adjusted by centrifugal moments inherent in the blades, against the action of generally radially-directed torsion springs. A belt-driven fan hub 12, Fig. 5, formed by rivetting together two steel pressings 14, 15, has tubular projections on each of which a sheet metal blade 18 is rotatably mounted. The hub parts may be formed by machining and the tubular extensions welded thereto. The blade roots may extend into sockets formed in the hub. Each blade root carries a pin 22 which extends through slots 21 in the associated tubular extension, the slot extremities providing the limits of angular adjustment of the blades. Centrifugal force reduces the pitch of each blade with an increase in speed against the action of a torsion spring, which may be of double-looped form, extending radially alongside or within the blade, Fig. 3 (not shown), and secured to a rivet 26 in the blade and a rivet in the hub. The torsion spring additionally absorbs the radial force exerted on the blade but if this force becomes excessive the pin 22 contacts the sides of its slots 21 and thereby takes up the load. Optional means for adjusting the fine pitch limit comprises a plate 50 provided with a stop 52 for each blade pin 22, the plate 50 being angularly adjustable to a position in which a spring-pressed pin 55 locates one of two or more holes 56, 57. The hole 56 provides a winter setting in which the whole range of blade adjustment is available down to a fine pitch of 17 degrees. The hole 57 provides a summer setting in which the finest pitch is 35 degrees. Alternatively, the pitch limit may be adjusted by cam means. The plate 50 may be arranged to be capable of rotating to a position in which the holes 56, 57 associated with one blade are moved to the vicinity of an adjacent blade and thereby provides settings for the coarse pitch limit thereof. A second plate 50 may be provided for controlling the coarse pitch limit of the blades. In an alternative embodiment, Fig. 4, the blade pitch may be further controlled, particularly at low speeds, by the temperature of the air passing through the fan. Two wax filled thermostats 40 attached to a finned plate 32 receive heat therefrom, and when the air temperature is approximately 10‹ F. higher than the set operating temperature they each extend a plunger 41 which, through a leaf spring 42, causes a plate 36, receiving the blade pins 22 in apertures 38, to be rotated and thereby coarsen the pitch of the blades and increase the speed at which the blades will commence to be adjusted centrifugally.
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BE646424D BE646424A (en) | 1963-04-11 | ||
GB25164A GB1055165A (en) | 1964-01-02 | 1964-01-02 | Improvements in or relating to engine cooling fans |
NL6403678A NL6403678A (en) | 1963-04-11 | 1964-04-07 | |
CH465864A CH415931A (en) | 1963-04-11 | 1964-04-10 | Fan for cooling an engine |
ES0298591A ES298591A1 (en) | 1963-04-11 | 1964-04-11 | Improvements in the construction of refrigerating fans (Machine-translation by Google Translate, not legally binding) |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB25164A GB1055165A (en) | 1964-01-02 | 1964-01-02 | Improvements in or relating to engine cooling fans |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1055165A true GB1055165A (en) | 1967-01-18 |
Family
ID=9701094
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB25164A Expired GB1055165A (en) | 1963-04-11 | 1964-01-02 | Improvements in or relating to engine cooling fans |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1055165A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113036607A (en) * | 2021-04-26 | 2021-06-25 | 王芳 | Switch board with dust removal and heat radiation structure |
-
1964
- 1964-01-02 GB GB25164A patent/GB1055165A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113036607A (en) * | 2021-04-26 | 2021-06-25 | 王芳 | Switch board with dust removal and heat radiation structure |
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