US3799128A - Engine cooling system radiator and fan shroud - Google Patents
Engine cooling system radiator and fan shroud Download PDFInfo
- Publication number
- US3799128A US3799128A US00339197A US33919773A US3799128A US 3799128 A US3799128 A US 3799128A US 00339197 A US00339197 A US 00339197A US 33919773 A US33919773 A US 33919773A US 3799128 A US3799128 A US 3799128A
- Authority
- US
- United States
- Prior art keywords
- engine
- radiator
- blades
- shroud
- tips
- 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 - Lifetime
Links
- 238000001816 cooling Methods 0.000 title claims abstract description 23
- 239000006260 foam Substances 0.000 claims abstract description 25
- 230000015572 biosynthetic process Effects 0.000 description 2
- XUKUURHRXDUEBC-KAYWLYCHSA-N Atorvastatin Chemical group C=1C=CC=CC=1C1=C(C=2C=CC(F)=CC=2)N(CC[C@@H](O)C[C@@H](O)CC(O)=O)C(C(C)C)=C1C(=O)NC1=CC=CC=C1 XUKUURHRXDUEBC-KAYWLYCHSA-N 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 230000000996 additive effect Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
Images
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
- F01P5/00—Pumping cooling-air or liquid coolants
- F01P5/02—Pumping cooling-air; Arrangements of cooling-air pumps, e.g. fans or blowers
- F01P5/06—Guiding or ducting air to, or from, ducted fans
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
- F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
Definitions
- An engine cooling system including a fan rotatably [58] Field of Search 123/4102, 41.04, 41.05, mounted on an engine, a fan Shroud secured to a radi l23/4l-49; 415/1741 119 ator, and a foam ring secured to an inner portion of the shroud immediately radially adjacent the tips of [56] References cued the fan blades such that the blades cut a clearance in UNITED TATE PA E T the foam ring during operation as required to compen- 3,053,694 9/1962 Daunt et a1.
- the cooling fan In current motor vehicles the cooling fan normally revolves in a shroud, the relationship therebetween providing a higher efficiency than for a shroudless fan, in drawing air through the radiator to cool the liquid which is circulated through the radiator and engine to control the temperature of the latter. It is well known that the less differential there is between the external diameter of the fan and the internal diameter of the shroud the more efficient will be the cooling process.
- a general object of this invention is to provide an improved simplified fan shroud arrangement which takes into consideration the above-described problem and efficiently compensates for same.
- Another object of the invention is to provide conventionally-mounted fan and shroud components which automatically compensate for the above described problem.
- a further object of the invention is to provide an improved fan and shroud arrangement wherein the shroud includes a foam insert positioned immediately radially adjacent the outer tips of the cooling fan blades such that any relative movement of the conventional engine-mounted fan with respect thereto will merely result in the fan blades cutting a clearance in the foam insert, resulting in a highly efficient cooling operation commensurate with the formation of the closest practicable operational clearance therebetween.
- FIG. 1 is a fragmentary side view of an engine cooling arrangement embodying the invention.
- FIG. 2 is an exploded view of the fan and shroud arrangement embodied in the invention.
- FIG. 1 illustrates a vehicular radiator and an engine 12 axially aligned therewith and spaced a predetermined distance apart therefrom.
- a cooling fan 14 including blades 16 is rotatably mounted on a shaft 18 on the front of the engine 12 and driven by a conventional belt 20 and pulley 22 combination.
- a fan shroud assembly 24 includes a rectangularshaped section 26 (FIG. 2) with mounting tabs or brackets 28 for mounting on the engine side of the radiator 10, the tabs 28 serving to permit the shroud assembly 24 to be aligned at installation with the cooling fan blades 16.
- a circular section 30 is formed on the rectangular section 26 and rigidly supported thereon by braces 32.
- a substantially venturi-shaped foam ring 34 is secured to the inner surface 36 (FIG. 1) and rearwardly extending edge 38 of the circular shroud section 30 in any suitable manner, such as by being glued thereon.
- the smallest inside diameter of the foam ring 34 is substantially the same diameter as the outermost diameter of the blades 16, the shroud assembly 24 being mounted on'the radiator 10 at assembly such that the ring 34 practically touches or just clears the outer edges of the blades 16 (FIG. 1).
- the invention provides an engine cooling system incorporating conventional components with a simplified shroud additive for automatically and efficiently providing the most efficient operational clearance between the fan and the shroud.
- an engine cooling system comprising a fan including a plurality of blades and rotatably mounted on said engine intermediate said engine and said radiator, a shroud assembly having a mounting portion mounted on said radiator and a shroud portion extending axially past the outer tips of said plurality of blades, and a foam ring secured to the inner surface of said extended shroud portion immediately adjacent said outer tips of said plurality of blades, said tips serving to cut a clearance in said foam ring compensating for any relative movement between said engine and said radiator.
- an engine cooling system comprising a fan including a plurality of blades and rotatably mounted on said engine intermediate said engine and said radiator, a shroud having a rectangular section mounted on said radiator and a circular section formed on said rectangular section and extending axially past the outer tips of said plurality of blades, and a foam ring secured to the inner surface of said circular shroud section immediately adjacent said outer tips of said plurality of blades, said tips serving to cut a clearance in said foam ring compensating for any relative movement between said engine and said radiator.
- an engine cooling system comprising a fan including a plurality of blades and rotatably mounted on said engine intermediate said engine and said radiator, a shroud having a rectangular section mounted on said radiator and a circular section formed on said rectangular section and extending axially past the outer tips of said plurality of blades, and a foam ring having a venturishaped radial inner surface and a substantially cylindrical radial outer surface, said outer surface being secured to the inner surface of said circular shroud section immediately adjacent said outer tips of said plurality of blades, said tips serving to cut a clearance in said venturi-shaped inner surface of said foam ring compensating for any relative movement between said engine and said radiator.
- an engine cooling system comprising a fan including a plurality of blades and rotatably mounted on said engine intermediate said engine and said radiator, a shroud having a rectangular section mounted on said radiator and a circular section formed on said rectangular section and extending axially past the outer tips of said plurality of blades, and a foam ring having a venturishaped radial inner surface and a two-diameter radial outer surface, the smaller radial outer surface being secured to the inner surface of said circular shroud section adjacent the end thereof and immediately adjacent said outer tips of said plurality of blades, the shoulder between the two outer surfaces abutting against said end of said circular shroud section, said tips serving to cut a clearance in said venturi-shaped inner surface of said foam ring compensating for any relative movement between said engine and said radiator.
Abstract
An engine cooling system including a fan rotatably mounted on an engine, a fan shroud secured to a radiator, and a foam ring secured to an inner portion of the shroud immediately radially adjacent the tips of the fan blades such that the blades cut a clearance in the foam ring during operation as required to compensate for any relative movement between the engine and radiator to thus provide for a highly efficient fan-shroud clearance.
Description
United States Patent 1191 Small Mar. 26, 1974 [54] ENGINE COOLING SYSTEM RADIATOR 3,487,519 1/1970 Davidson 415/174 UX AND FAN S R 3,519,282 7/1970 Davis 415/214 UX 3,547,455 12/1970 Daunt 415/214 UX [75] In n Robert 0 Small, g, Mleh- 3,575,427 4/1971 Lapac etal. 415/174 ux 3,689,971 9/1972 Davidson 415/174 X [73 1 Asslgnee' Minors Cmpm'atmn 3,756,741 9/1973 Woell, Jr. 415/174 Detroit, M1ch.
[ Filedi 1973 Primary Examiner-A1 Lawrence Smith [21] Appl No: 339197 Attorney, Agent, or Firm-John P. Moran 52 US. Cl 123/4149, 415/174, 415/214 1 ABSTRACT [51] '1 CL F01! 11/10 F04d 29/021 F04d 29/08 An engine cooling system including a fan rotatably [58] Field of Search 123/4102, 41.04, 41.05, mounted on an engine, a fan Shroud secured to a radi l23/4l-49; 415/1741 119 ator, and a foam ring secured to an inner portion of the shroud immediately radially adjacent the tips of [56] References cued the fan blades such that the blades cut a clearance in UNITED TATE PA E T the foam ring during operation as required to compen- 3,053,694 9/1962 Daunt et a1. 415/174 x Sate for ny r l ov men be ween the engine 3,294,315 12/1966 Stewart et a1 415/214 and radiator to thus provide for a highly efficient fan- 3,313,476 4/1967 Ross 415/174 UX shroud clearance. 3,321,931 5/1967 Lehmkuhl 415/119 3,346,175 10/1967 Wiles 415/214 UX 4 Claims, 2 Drawing Figures ENGINE COOLING SYSTEM RADIATOR AND FAN SHROUD -This invention relates generally to engine cooling systems and, more particularly, to an improved fan-shroud arrangement therefor.
In current motor vehicles the cooling fan normally revolves in a shroud, the relationship therebetween providing a higher efficiency than for a shroudless fan, in drawing air through the radiator to cool the liquid which is circulated through the radiator and engine to control the temperature of the latter. It is well known that the less differential there is between the external diameter of the fan and the internal diameter of the shroud the more efficient will be the cooling process.
However, it is also well known that, with the shroud mounted on the radiator and the fan rotatably mounted on the engine, relative radial movement of the fan and the shroud is apt to occur at various times, such as when the engine is started and/or when the vehicle is traveling over rough terrain. Because of this, it has been the custom to provide a substantial annular clearance between the external diameter of the fan blades and the internal diameter of the shroud.
In lieu of the predetermined annular clearance provision, it has been proposed to provide a fan shroud having an internal venturi-shaped section and an external box section, wherein the two sections are interconnected by a suitable flexible sealing ring, permitting the two sections to be mounted respectively on the engine and the radiator, thus avoiding any relative movement between the fan and the adjacent venturi-shaped shroud section (U.S. Pat. No. 3,144,859 Walton, dated Aug. 18,1964).
A general object of this invention is to provide an improved simplified fan shroud arrangement which takes into consideration the above-described problem and efficiently compensates for same.
Another object of the invention is to provide conventionally-mounted fan and shroud components which automatically compensate for the above described problem. I
A further object of the invention is to provide an improved fan and shroud arrangement wherein the shroud includes a foam insert positioned immediately radially adjacent the outer tips of the cooling fan blades such that any relative movement of the conventional engine-mounted fan with respect thereto will merely result in the fan blades cutting a clearance in the foam insert, resulting in a highly efficient cooling operation commensurate with the formation of the closest practicable operational clearance therebetween.
These and other objects and advantages of the invention will be apparent when reference is made to the following description and accompanying drawings, wherein:
FIG. 1 is a fragmentary side view of an engine cooling arrangement embodying the invention; and
FIG. 2 is an exploded view of the fan and shroud arrangement embodied in the invention.
Referring now to the drawings in greater detail, FIG. 1 illustrates a vehicular radiator and an engine 12 axially aligned therewith and spaced a predetermined distance apart therefrom. A cooling fan 14 including blades 16 is rotatably mounted on a shaft 18 on the front of the engine 12 and driven by a conventional belt 20 and pulley 22 combination.
A fan shroud assembly 24 includes a rectangularshaped section 26 (FIG. 2) with mounting tabs or brackets 28 for mounting on the engine side of the radiator 10, the tabs 28 serving to permit the shroud assembly 24 to be aligned at installation with the cooling fan blades 16. A circular section 30 is formed on the rectangular section 26 and rigidly supported thereon by braces 32.
A substantially venturi-shaped foam ring 34 is secured to the inner surface 36 (FIG. 1) and rearwardly extending edge 38 of the circular shroud section 30 in any suitable manner, such as by being glued thereon. The smallest inside diameter of the foam ring 34 is substantially the same diameter as the outermost diameter of the blades 16, the shroud assembly 24 being mounted on'the radiator 10 at assembly such that the ring 34 practically touches or just clears the outer edges of the blades 16 (FIG. 1).
Now, any relative movement of the engine 12 with respect to the shroud assembly 24, as a result of vibrations, for example, will cause the respective fan blades 16 outer edges to cut a clearance in the foam ring 34. There results a highly efficient cooling operation due to the formation of the closest practicable operational clearance 40 between the ring 34 and the blades 16, short of mounting the shroud on the engine itself.
It should be apparent that the invention provides an engine cooling system incorporating conventional components with a simplified shroud additive for automatically and efficiently providing the most efficient operational clearance between the fan and the shroud.
While but one embodiment of the invention has been shown and described, other modifications thereof are possible.
I claim:
1. For use with a vehicular engine and radiator, an engine cooling system comprising a fan including a plurality of blades and rotatably mounted on said engine intermediate said engine and said radiator, a shroud assembly having a mounting portion mounted on said radiator and a shroud portion extending axially past the outer tips of said plurality of blades, and a foam ring secured to the inner surface of said extended shroud portion immediately adjacent said outer tips of said plurality of blades, said tips serving to cut a clearance in said foam ring compensating for any relative movement between said engine and said radiator.
2. For use with a vehicular engine and radiator, an engine cooling system comprising a fan including a plurality of blades and rotatably mounted on said engine intermediate said engine and said radiator, a shroud having a rectangular section mounted on said radiator and a circular section formed on said rectangular section and extending axially past the outer tips of said plurality of blades, and a foam ring secured to the inner surface of said circular shroud section immediately adjacent said outer tips of said plurality of blades, said tips serving to cut a clearance in said foam ring compensating for any relative movement between said engine and said radiator.
3. For use with a vehicular engine and radiator, an engine cooling system comprising a fan including a plurality of blades and rotatably mounted on said engine intermediate said engine and said radiator, a shroud having a rectangular section mounted on said radiator and a circular section formed on said rectangular section and extending axially past the outer tips of said plurality of blades, and a foam ring having a venturishaped radial inner surface and a substantially cylindrical radial outer surface, said outer surface being secured to the inner surface of said circular shroud section immediately adjacent said outer tips of said plurality of blades, said tips serving to cut a clearance in said venturi-shaped inner surface of said foam ring compensating for any relative movement between said engine and said radiator.
4. For use with a vehicular engine and radiator, an engine cooling system comprising a fan including a plurality of blades and rotatably mounted on said engine intermediate said engine and said radiator, a shroud having a rectangular section mounted on said radiator and a circular section formed on said rectangular section and extending axially past the outer tips of said plurality of blades, and a foam ring having a venturishaped radial inner surface and a two-diameter radial outer surface, the smaller radial outer surface being secured to the inner surface of said circular shroud section adjacent the end thereof and immediately adjacent said outer tips of said plurality of blades, the shoulder between the two outer surfaces abutting against said end of said circular shroud section, said tips serving to cut a clearance in said venturi-shaped inner surface of said foam ring compensating for any relative movement between said engine and said radiator.
Claims (4)
1. For use with a vehicular engine and radiator, an engine cooling system comprising a fan including a plurality of blades and rotatably mounted on said engine intermediate said engine and said radiator, a shroud assembly having a mounting portion mounted on said radiator and a shroud portion extending axially past the outer tips of said plurality of blades, and a foam ring secured to the inner surface of said extended shroud portion immediately adjacent said outer tips of said plurality of blades, said tips serving to cut a clearance in said foam ring compensating for any relative movement between said engine and said radiator.
2. For use with a vehicular engine and radiator, an engine cooling system comprising a fan including a plurality of blades and rotatably mounted on said engine intermediate said engine and said radiator, a shroud having a rectangular section mounted on said radiator and a circular section formed on said rectangular section and extending axially past the outer tips of said plurality of blades, and a foam ring secured to the inner surface of said circular shroud section immediately adjacent said outer tips of said plurality of blades, said tips serving to cut a clearance in said foam ring compensating for any relative movement between said engine and said radiator.
3. For use with a vehicular engine and radiator, an engine cooling system comprising a fan including a plurality of blades and rotatably mounted on said engine intermediate said engine and said radiator, a shroud having a rectangular section mounted on said radiator and a circular section formed on said rectangular section and extending axially past the outer tips of said plurality of blades, and a foam ring having a venturi-shaped radial inner surface and a substantially cylindrical rAdial outer surface, said outer surface being secured to the inner surface of said circular shroud section immediately adjacent said outer tips of said plurality of blades, said tips serving to cut a clearance in said venturi-shaped inner surface of said foam ring compensating for any relative movement between said engine and said radiator.
4. For use with a vehicular engine and radiator, an engine cooling system comprising a fan including a plurality of blades and rotatably mounted on said engine intermediate said engine and said radiator, a shroud having a rectangular section mounted on said radiator and a circular section formed on said rectangular section and extending axially past the outer tips of said plurality of blades, and a foam ring having a venturi-shaped radial inner surface and a two-diameter radial outer surface, the smaller radial outer surface being secured to the inner surface of said circular shroud section adjacent the end thereof and immediately adjacent said outer tips of said plurality of blades, the shoulder between the two outer surfaces abutting against said end of said circular shroud section, said tips serving to cut a clearance in said venturi-shaped inner surface of said foam ring compensating for any relative movement between said engine and said radiator.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US00339197A US3799128A (en) | 1973-03-08 | 1973-03-08 | Engine cooling system radiator and fan shroud |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US00339197A US3799128A (en) | 1973-03-08 | 1973-03-08 | Engine cooling system radiator and fan shroud |
Publications (1)
Publication Number | Publication Date |
---|---|
US3799128A true US3799128A (en) | 1974-03-26 |
Family
ID=23327933
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US00339197A Expired - Lifetime US3799128A (en) | 1973-03-08 | 1973-03-08 | Engine cooling system radiator and fan shroud |
Country Status (1)
Country | Link |
---|---|
US (1) | US3799128A (en) |
Cited By (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5427248U (en) * | 1977-07-27 | 1979-02-22 | ||
US4213426A (en) * | 1978-11-09 | 1980-07-22 | General Motors Corporation | Shrouding for engine mounted cooling fan |
US4398508A (en) * | 1981-02-20 | 1983-08-16 | Volvo White Truck Corporation | Engine cooling fan construction |
EP0098397A1 (en) * | 1982-07-09 | 1984-01-18 | Iveco Magirus Aktiengesellschaft | A fan shroud attached to a water cooler of an internal-combustion engine |
EP0109823A1 (en) * | 1982-11-18 | 1984-05-30 | Ingersoll-Rand Company | Rotary displacement machine |
US4460185A (en) * | 1982-08-23 | 1984-07-17 | General Electric Company | Seal including a non-metallic abradable material |
US4478552A (en) * | 1982-11-08 | 1984-10-23 | Thompson Stanley E | Method and apparatus for fan blade tip clearance |
DE4014496C1 (en) * | 1990-05-07 | 1991-07-18 | Audi Ag, 8070 Ingolstadt, De | Cooling system between radiator and engine of motor vehicle - includes plastic section fixed to radiator and guide collar made of soft elastic elastomer which surrounds fan blades |
US5066194A (en) * | 1991-02-11 | 1991-11-19 | Carrier Corporation | Fan orifice structure and cover for outside enclosure of an air conditioning system |
US5215437A (en) * | 1991-12-19 | 1993-06-01 | Carrier Corporation | Inlet orifice and centrifugal flow fan assembly |
US5762034A (en) * | 1996-01-16 | 1998-06-09 | Board Of Trustees Operating Michigan State University | Cooling fan shroud |
US5884589A (en) * | 1995-04-10 | 1999-03-23 | Hitachi Construction Machinery Co., Ltd. | Cooling apparatus for heat exchanger |
WO2001083950A1 (en) * | 2000-05-03 | 2001-11-08 | Siemens Automotive Inc. | Turbomachine with rotor-shroud seal structure |
US20020112680A1 (en) * | 2000-12-28 | 2002-08-22 | Kenji Oki | Vehicle radiator device |
US6450760B1 (en) * | 1999-11-22 | 2002-09-17 | Komatsu Ltd. | Fan device |
US6454527B2 (en) * | 2000-07-31 | 2002-09-24 | Komatsu Ltd. | Noise reduction mechanism of fan device and molding method of porous damping material therefor |
US6663739B2 (en) | 1998-05-15 | 2003-12-16 | Elliott Turbomachinery Co., Inc. | Method for forming a fluid seal between rotating and stationary members |
GB2397342A (en) * | 2002-12-19 | 2004-07-21 | Flakt Woods Ltd | Fan duct with abradable coating surrounding blade tips |
US20050173926A1 (en) * | 2004-02-06 | 2005-08-11 | Soqi Kabushiki Kaisha | Generating apparatus |
US20060042569A1 (en) * | 2004-08-30 | 2006-03-02 | Brian Jacquay | Engine cooling fan shroud |
US20060177306A1 (en) * | 2002-03-30 | 2006-08-10 | University Of Central Florida | High efficiency air conditioner condenser fan with performance enhancements |
US20070231128A1 (en) * | 2006-03-31 | 2007-10-04 | Caterpiller Inc. | Fan assembly |
GB2449938A (en) * | 2007-06-08 | 2008-12-10 | Cummins Power Generation Ltd | Fan alignment tool |
US20150204351A1 (en) * | 2012-08-16 | 2015-07-23 | Hitachi Construction Machinery Co., Ltd. | Cooling Fan Mounting Structure for Construction Machine |
EP2990655A1 (en) * | 2014-08-26 | 2016-03-02 | CNH Industrial Italia S.p.A. | Fan assembly with shroud wear ring for a work vehicle |
US10197294B2 (en) | 2016-01-15 | 2019-02-05 | Johnson Controls Technology Company | Foam substructure for a heat exchanger |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3053694A (en) * | 1961-02-20 | 1962-09-11 | Gen Electric | Abradable material |
US3294315A (en) * | 1964-09-28 | 1966-12-27 | Buffalo Forge Co | Fan construction |
US3313476A (en) * | 1965-05-03 | 1967-04-11 | Electrolux Corp | Centrifugal fan having substantially reduced internal air recirculation |
US3321931A (en) * | 1965-05-03 | 1967-05-30 | Whirlpool Co | Fan structure |
US3346175A (en) * | 1966-04-01 | 1967-10-10 | Gen Motors Corp | Plastic coating for compressors |
US3487519A (en) * | 1967-08-31 | 1970-01-06 | Hudson Eng Co | Method of making axial flow fans |
US3519282A (en) * | 1966-03-11 | 1970-07-07 | Gen Electric | Abradable material seal |
US3547455A (en) * | 1969-05-02 | 1970-12-15 | Gen Electric | Rotary seal including organic abradable material |
US3575427A (en) * | 1969-11-03 | 1971-04-20 | United Aircraft Corp | Composite abradable seal |
US3689971A (en) * | 1967-08-31 | 1972-09-12 | Eugene M Davidson | Axial flow fans |
US3756741A (en) * | 1971-12-17 | 1973-09-04 | Jacuzzi Bros Inc | Jet propulsion pump assembly |
-
1973
- 1973-03-08 US US00339197A patent/US3799128A/en not_active Expired - Lifetime
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3053694A (en) * | 1961-02-20 | 1962-09-11 | Gen Electric | Abradable material |
US3294315A (en) * | 1964-09-28 | 1966-12-27 | Buffalo Forge Co | Fan construction |
US3313476A (en) * | 1965-05-03 | 1967-04-11 | Electrolux Corp | Centrifugal fan having substantially reduced internal air recirculation |
US3321931A (en) * | 1965-05-03 | 1967-05-30 | Whirlpool Co | Fan structure |
US3519282A (en) * | 1966-03-11 | 1970-07-07 | Gen Electric | Abradable material seal |
US3346175A (en) * | 1966-04-01 | 1967-10-10 | Gen Motors Corp | Plastic coating for compressors |
US3487519A (en) * | 1967-08-31 | 1970-01-06 | Hudson Eng Co | Method of making axial flow fans |
US3689971A (en) * | 1967-08-31 | 1972-09-12 | Eugene M Davidson | Axial flow fans |
US3547455A (en) * | 1969-05-02 | 1970-12-15 | Gen Electric | Rotary seal including organic abradable material |
US3575427A (en) * | 1969-11-03 | 1971-04-20 | United Aircraft Corp | Composite abradable seal |
US3756741A (en) * | 1971-12-17 | 1973-09-04 | Jacuzzi Bros Inc | Jet propulsion pump assembly |
Cited By (39)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5427248U (en) * | 1977-07-27 | 1979-02-22 | ||
US4213426A (en) * | 1978-11-09 | 1980-07-22 | General Motors Corporation | Shrouding for engine mounted cooling fan |
US4398508A (en) * | 1981-02-20 | 1983-08-16 | Volvo White Truck Corporation | Engine cooling fan construction |
EP0098397A1 (en) * | 1982-07-09 | 1984-01-18 | Iveco Magirus Aktiengesellschaft | A fan shroud attached to a water cooler of an internal-combustion engine |
DE3225653A1 (en) * | 1982-07-09 | 1984-03-15 | Iveco Magirus AG, 7900 Ulm | COOLER COVER FIXED TO A WATER COOLER OF INTERNAL COMBUSTION ENGINES |
US4460185A (en) * | 1982-08-23 | 1984-07-17 | General Electric Company | Seal including a non-metallic abradable material |
US4478552A (en) * | 1982-11-08 | 1984-10-23 | Thompson Stanley E | Method and apparatus for fan blade tip clearance |
EP0109823A1 (en) * | 1982-11-18 | 1984-05-30 | Ingersoll-Rand Company | Rotary displacement machine |
DE4014496C1 (en) * | 1990-05-07 | 1991-07-18 | Audi Ag, 8070 Ingolstadt, De | Cooling system between radiator and engine of motor vehicle - includes plastic section fixed to radiator and guide collar made of soft elastic elastomer which surrounds fan blades |
US5066194A (en) * | 1991-02-11 | 1991-11-19 | Carrier Corporation | Fan orifice structure and cover for outside enclosure of an air conditioning system |
US5215437A (en) * | 1991-12-19 | 1993-06-01 | Carrier Corporation | Inlet orifice and centrifugal flow fan assembly |
US5884589A (en) * | 1995-04-10 | 1999-03-23 | Hitachi Construction Machinery Co., Ltd. | Cooling apparatus for heat exchanger |
US5762034A (en) * | 1996-01-16 | 1998-06-09 | Board Of Trustees Operating Michigan State University | Cooling fan shroud |
US5881685A (en) * | 1996-01-16 | 1999-03-16 | Board Of Trustees Operating Michigan State University | Fan shroud with integral air supply |
US6663739B2 (en) | 1998-05-15 | 2003-12-16 | Elliott Turbomachinery Co., Inc. | Method for forming a fluid seal between rotating and stationary members |
US6450760B1 (en) * | 1999-11-22 | 2002-09-17 | Komatsu Ltd. | Fan device |
US6471472B1 (en) * | 2000-05-03 | 2002-10-29 | Siemens Canada Limited | Turbomachine shroud fibrous tip seal |
WO2001083950A1 (en) * | 2000-05-03 | 2001-11-08 | Siemens Automotive Inc. | Turbomachine with rotor-shroud seal structure |
US6454527B2 (en) * | 2000-07-31 | 2002-09-24 | Komatsu Ltd. | Noise reduction mechanism of fan device and molding method of porous damping material therefor |
US20020112680A1 (en) * | 2000-12-28 | 2002-08-22 | Kenji Oki | Vehicle radiator device |
ES2204259A1 (en) * | 2000-12-28 | 2004-04-16 | Honda Giken Kogyo Kabushiki Kaisha | Vehicle radiator device |
US6971438B2 (en) | 2000-12-28 | 2005-12-06 | Honda Giken Kogyo Kabushiki Kaisha | Vehicle radiator device |
US7618233B2 (en) * | 2002-03-30 | 2009-11-17 | University Of Central Florida Research Foundation, Inc. | High efficiency air conditioner condenser fan with performance enhancements |
US20060177306A1 (en) * | 2002-03-30 | 2006-08-10 | University Of Central Florida | High efficiency air conditioner condenser fan with performance enhancements |
GB2397342A (en) * | 2002-12-19 | 2004-07-21 | Flakt Woods Ltd | Fan duct with abradable coating surrounding blade tips |
US20050173926A1 (en) * | 2004-02-06 | 2005-08-11 | Soqi Kabushiki Kaisha | Generating apparatus |
US20060042569A1 (en) * | 2004-08-30 | 2006-03-02 | Brian Jacquay | Engine cooling fan shroud |
US7165515B2 (en) * | 2004-08-30 | 2007-01-23 | International Truck Intellectual Property Company, Llc | Engine cooling fan shroud |
US20070231128A1 (en) * | 2006-03-31 | 2007-10-04 | Caterpiller Inc. | Fan assembly |
GB2449938A (en) * | 2007-06-08 | 2008-12-10 | Cummins Power Generation Ltd | Fan alignment tool |
GB2449938B (en) * | 2007-06-08 | 2012-04-11 | Cummins Power Generation Ltd | Engine alignment tool |
US20150204351A1 (en) * | 2012-08-16 | 2015-07-23 | Hitachi Construction Machinery Co., Ltd. | Cooling Fan Mounting Structure for Construction Machine |
EP2990655A1 (en) * | 2014-08-26 | 2016-03-02 | CNH Industrial Italia S.p.A. | Fan assembly with shroud wear ring for a work vehicle |
US20160060844A1 (en) * | 2014-08-26 | 2016-03-03 | CNH Industrial America, LLC | Shroud wear ring for a work vehicle |
CN105386993A (en) * | 2014-08-26 | 2016-03-09 | 凯斯纽荷兰(中国)管理有限公司 | Fan assembly with shroud wear ring for work vehicle |
US10174481B2 (en) * | 2014-08-26 | 2019-01-08 | Cnh Industrial America Llc | Shroud wear ring for a work vehicle |
CN105386993B (en) * | 2014-08-26 | 2019-06-14 | 凯斯纽荷兰(中国)管理有限公司 | A kind of fan component and its Working vehicle for Working vehicle |
US10197294B2 (en) | 2016-01-15 | 2019-02-05 | Johnson Controls Technology Company | Foam substructure for a heat exchanger |
US11073293B2 (en) | 2016-01-15 | 2021-07-27 | Johnson Controls Technology Company | Foam substructure for a heat exchanger |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3799128A (en) | Engine cooling system radiator and fan shroud | |
US4396351A (en) | Engine cooling fan | |
US3794001A (en) | Variable tip clearance engine cooling fan shroud | |
US4451202A (en) | Axial cooling fan for internal combustion engines | |
US3272188A (en) | Combination fan and water pump drive | |
EP0238080B1 (en) | Alternator for automobile | |
US4213426A (en) | Shrouding for engine mounted cooling fan | |
EP2333347B1 (en) | Axial flow fan with hub isolation slots | |
EP0014072B1 (en) | Viscous fan drive | |
US3635285A (en) | Cooling fan | |
US4210835A (en) | Fan with a cooled motor | |
US4153389A (en) | Fan-fan drive assembly | |
US3021442A (en) | Dynamoelectric machine | |
US5410992A (en) | Cooling system for automotive engine | |
US4169693A (en) | Fluid coupling device and fan mounting arrangement | |
US2225209A (en) | Motor cooling control | |
JPS6325199B2 (en) | ||
US6494681B2 (en) | Combined axial flow and centrifugal fan in an electrical motor | |
US2032224A (en) | Fan | |
US10823042B2 (en) | Air blowing fan device | |
US4488518A (en) | Engine cooling device | |
US2896595A (en) | Method and apparatus for cooling of radiators of engines and the like | |
US5645401A (en) | Axial fan for a radiator of a motor vehicle engine | |
US2206488A (en) | Water pump | |
ATE167439T1 (en) | DRIVE UNIT WITH AN INTERNAL COMBUSTION ENGINE AND A HYDRODYNAMIC RETARDER |