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US2432576A - Gear pump for aeronautical apparatus - Google Patents

Gear pump for aeronautical apparatus Download PDF

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Publication number
US2432576A
US2432576A US466844A US46684442A US2432576A US 2432576 A US2432576 A US 2432576A US 466844 A US466844 A US 466844A US 46684442 A US46684442 A US 46684442A US 2432576 A US2432576 A US 2432576A
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US
United States
Prior art keywords
shaft
lubricant
pump
cylinder
seal
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
Application number
US466844A
Inventor
Albert E Koffer
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Motors Liquidation Co
Original Assignee
General Motors Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by General Motors Corp filed Critical General Motors Corp
Priority to US466844A priority Critical patent/US2432576A/en
Application granted granted Critical
Publication of US2432576A publication Critical patent/US2432576A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2/00Rotary-piston machines or pumps
    • F04C2/08Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
    • F04C2/12Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type
    • F04C2/14Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons
    • F04C2/18Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons with similar tooth forms
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S277/00Seal for a joint or juncture
    • Y10S277/907Passageway in rod or shaft

Definitions

  • This invention relates to aeronautical apparatus and more particularly to an oil pump.
  • One object of this invention is to simplify the pump structure so as to facilitate its manufacture and assembly.
  • Fig. 1 is a vertical sectional view taken on line I
  • Fig. 2 is a horizontal sectional view taken on line 22 of Fig. 1;
  • Fig. 3 is another vertical sectional view taken on line 3-3 of Fig. 1;
  • Fig. 4 is another horizontal sectional view taken on line 4-4 of Fig. 3.
  • reference numeral Ill designates a first casing element
  • reference numeral I2 designates a second casing element
  • reference numeral l4 designates the main gear casing which is sandwiched in between the casing elements [0 and 12.
  • the elements l0, l2 and I4 are held in proper assembled relationship by means of the bolts IS.
  • the pump is a gear type of pump having a first gear element I6 and a second gear element l8, both of which are disposedwithin the main pumping chamber formed in theelment l4.
  • the gear I6 is carried by a shaft 22 and may be formed integrally therewith or otherwise secured thereto.
  • the gear I8 is carried by the main drive shaft 24 and may be formed integrally therewith or secured thereto in any well-known manner.
  • the lower ends of the shafts 22 and 24 are journaled in a bearing member 26 and the upper ends of these shafts are journaled in a bearing member 28.
  • the bearing elements 26 and 28 are made from identical castings and ar similar in all respects except that the upper bearing member 23 is provided with an inlet passage 30 which conveys the oil or other medium to be I pumped from the main inlet 32 provided in the 2 element In to the intake port 34 provided in the element l4.
  • the I number of different shaped parts has been reduced.
  • a shaft seal cavity 38 is provided in the upper end of the casing section in and has mounted therein a shaft seal construction which prevents the lubricant from escaping from the main casing at the point where the shaft passes through the casing.
  • This shaft seal comprises a stationary sealing ring 38 which is held in place within the shaft seal cavity by means of a rubber-like gasket 40 arranged as shown in Fig. 1.
  • Ring 38 is provided with an inner diameter slightly greater than the outer diameter of the main drive shaft 24 so as .to provide a running clearance space for the shaft 24 at the point thereof surrounded by ring 38. This running clearance space forms a communicating means utilized for a purpose to be presently described.
  • the rubber-like gasket 40 is preferably made of neoprene or some similar synthetic rubber which is unaffected by lubricant.
  • a rotating seal ring 42 cooperates with the stationary seal ring 38 in accordance with well known practice and is biased into engagement with the stationary ring 38 by means of a plurality of spring washers 44 which press against the neoprene ring 46.
  • the neoprene ring 46 not only serves to seal the ring 42 to the shaft 24 but also serves to prevent relative rotation between the shaft 24 and the ring 42.
  • a suitable end thrust washer 48 keyed or otherwise secured to the shaft 24, serves as an abutment. for the spring washers 44.
  • the opposite ends of the bearing elements 26 and 28 are recessed so as to provide a space between the end of each bearing and the main casing.
  • the oil enters the pump through the inlet 32 and leaves through the passage 50 provided in the member 14.
  • the pressures at the outlet are extremely high with the result that there is a tendency for the oil to flow along the shafts and escape adjacent the ends of the shafts.
  • the main shaft bearings are adequately lubricated by the oil flowing along the shafts.
  • the shaft 24 is provided with a central oil passage 54 which has its lower end communicating with the space 56. provided between the bearing formed between the upper end of the bearing ele-.
  • the chamber 62 communicates with the inlet passage 32 whereby the oil all returns to the inlet side of the pump rather than escaping to the outside. It will also be noted that the oil flowing upwardly along the shafts from the gear cavity will be dis charged into the chamber 62 from whence the oil will return to the inlet of the pump.
  • the bearing elements 26 and 2B are made from some suitable bearing material such as Sabeco, whereas the casing elements may be made from any cheap material which may be formed, such as by casting or moulding.
  • a pump means forming a pumping cylinder, cylinder heads disposed on opposite sides thereof, a pair of pumping gears within said cylinder, shaft means projecting from opposite sides of each of said. gears into said. cylinder heads, said cylinder heads including bearing inserts for said shaft means, said b'earing inserts having substantially identical outer dimensions, a passage in one of said bearing inserts through which fluid to be pumped enters into said pumping cylinder, said shaft means including a drive shaft projecting through one of said cylinder heads, an outboard shaft seal for said drive shaft including a pair of relatively rotatable seal rings having seal surfaces in engagement with one another, means including a lubricant passage in said drive shaft whereby lubricant is centrifugally discharged to said shaft seal from a point substantially opposite said seal surfaces and means whereby the excess lubricant supplied to said seal surfaces is thereafter introduced into said pumping cylinder.
  • a lubricant pump means forming a lubricant pumping cylinder, cylinder heads disposed on opposite sides thereof, a pair of pumping gears in said cylinder, shaft means projecting from opposite sides of each of said gears into said cylinder heads, said shaft means including a drive shaft projecting through one of said cylinder heads, a shaft seal for preventing the escape of lubricant along said drive shaft, said cylinder heads including bearing inserts for said shaft means, a low pressure lubricant inl t.
  • a h p 4 i sure lubricant outlet a shaft seal lubricating cavity
  • lubricant collecting reservoirs at the outer ends of said bearing inserts for collecting the lubricant escaping from said cylinder along said shaft means, one of said reservoirs communicating with said low pressure lubricant inlet, means for conveying lubricant from another of said reservoirs through one of said shafts and into said cavity, and means for returning lubricant from said cavity to said low pressure lubricant inlet;
  • apump means forming a pumping cylinder, cylinder heads disposed on opposite sides thereof, a pair of pumping gears in said cylinder, shaft means projecting from opposite sides of each of said gears into said cylinder heads, said shaft means including a drive shaft projecting through one of said cylinder heads, a shaft seal for preventing the escape of lubricant along said drive shaft, a low pressure inlet, a high pressure outlet, a shaft seal lubricating cavity, lubricant collecting reservoirs adjacent the outer ends of said shaft means for collecting the lubricant escaping from said cylinder along said shaft means, one of said reservoirs communicating with said low pressure lubricant inlet, means for conveying lubricant from another of said reservoirs through one of said shafts and into said cavity, and means for returning lubricant from said cavity to said low pressure inlet.
  • a pump means forming a pumping cylinder, cylinder heads disposed on opposite sides thereof, pumping means in said cylinder, shaft means extending from opposite sides of said pumping means into said cylinder heads, said shaft means including a drive shaft projecting through one of said heads, a shaft seal adjacent the projecting end of said shaft for preventing the escape of lubricant along said drive shaft, a suction port, an outlet port, means forming a shaft seal lubricating cavity adjacent said suction port and in communication with said suction port, means forming a lubricant collecting reservoir at the inner end of said drive shaft for collecting the lubricant escaping from said cylinder along said drive shaft, said drive shaft being provided with a lubricant passage for con veying lubricant from said lubricant collecting reservoir at the inner end of the drive shaft to said shaft seal lubricating cavity.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Rotary Pumps (AREA)

Description

Dec. 16, 1947. A. E. KOFFER 2,432,576
AR PUMP 25, 1942 2 Sheets-Sheet 2 Patented Dec. 16, 1947 GEAR PUMP FOR AERONAUTICAL APPARATUS Albert E. Koffen Dayton, Ohio, assignor to General Motors Corporation, Dayton, Ohio, a corporation of Delaware Application November 25, 1942, Serial No. 466,844
4 Claims. (01. 103-126) This invention relates to aeronautical apparatus and more particularly to an oil pump.
One object of this invention is to simplify the pump structure so as to facilitate its manufacture and assembly.
ing drawings, wherein a preferred form of the present invention is clearly shown.
In the drawings:
Fig. 1 is a vertical sectional view taken on line I| of Fig. 2;
Fig. 2 is a horizontal sectional view taken on line 22 of Fig. 1;
Fig. 3 is another vertical sectional view taken on line 3-3 of Fig. 1; and
Fig. 4 is another horizontal sectional view taken on line 4-4 of Fig. 3. I
Referring now to Fig. 1, wherein I have shown a preferred embodiment of my invention, reference numeral Ill designates a first casing element, reference numeral I2 designates a second casing element, and reference numeral l4 designates the main gear casing which is sandwiched in between the casing elements [0 and 12. The elements l0, l2 and I4 are held in proper assembled relationship by means of the bolts IS.
The pump is a gear type of pump having a first gear element I6 and a second gear element l8, both of which are disposedwithin the main pumping chamber formed in theelment l4.
The gear I6 is carried by a shaft 22 and may be formed integrally therewith or otherwise secured thereto. The gear I8 is carried by the main drive shaft 24 and may be formed integrally therewith or secured thereto in any well-known manner. The lower ends of the shafts 22 and 24 are journaled in a bearing member 26 and the upper ends of these shafts are journaled in a bearing member 28.
In order to simplify the manufacture and assembly of the parts, the bearing elements 26 and 28 are made from identical castings and ar similar in all respects except that the upper bearing member 23 is provided with an inlet passage 30 which conveys the oil or other medium to be I pumped from the main inlet 32 provided in the 2 element In to the intake port 34 provided in the element l4. By virtue of this similarity, the I number of different shaped parts has been reduced.
A shaft seal cavity 38 is provided in the upper end of the casing section in and has mounted therein a shaft seal construction which prevents the lubricant from escaping from the main casing at the point where the shaft passes through the casing. This shaft seal comprises a stationary sealing ring 38 which is held in place within the shaft seal cavity by means of a rubber-like gasket 40 arranged as shown in Fig. 1. Ring 38 is provided with an inner diameter slightly greater than the outer diameter of the main drive shaft 24 so as .to provide a running clearance space for the shaft 24 at the point thereof surrounded by ring 38. This running clearance space forms a communicating means utilized for a purpose to be presently described. The rubber-like gasket 40 is preferably made of neoprene or some similar synthetic rubber which is unaffected by lubricant. A rotating seal ring 42 cooperates with the stationary seal ring 38 in accordance with well known practice and is biased into engagement with the stationary ring 38 by means of a plurality of spring washers 44 which press against the neoprene ring 46. The neoprene ring 46 not only serves to seal the ring 42 to the shaft 24 but also serves to prevent relative rotation between the shaft 24 and the ring 42. A suitable end thrust washer 48, keyed or otherwise secured to the shaft 24, serves as an abutment. for the spring washers 44.
It will be noted that the opposite ends of the bearing elements 26 and 28 are recessed so as to provide a space between the end of each bearing and the main casing. The oil enters the pump through the inlet 32 and leaves through the passage 50 provided in the member 14. In a pump of this type, the pressures at the outlet are extremely high with the result that there is a tendency for the oil to flow along the shafts and escape adjacent the ends of the shafts. Thus, the main shaft bearings are adequately lubricated by the oil flowing along the shafts. In order to prevent the oil flowing along the shaft from leaving the main pump casing, I hav provided means formaintaining the ends of the shaft at a pressure corresponding to the inlet pressure and for returning the escaping oil to the inlet of the p p.
The shaft 24 is provided with a central oil passage 54 which has its lower end communicating with the space 56. provided between the bearing formed between the upper end of the bearing ele-.
ment 28 and the casing section I0, through the running clearance space heretofore described and which permits cavity 60 to communicate with the chamber 62. As best shown in Figs. 3 and 4, the chamber 62 communicates with the inlet passage 32 whereby the oil all returns to the inlet side of the pump rather than escaping to the outside. It will also be noted that the oil flowing upwardly along the shafts from the gear cavity will be dis charged into the chamber 62 from whence the oil will return to the inlet of the pump.
For convenience in describing this pump, I have referred to it as a vertical pump, whereas it is obvious that the pump may be disposed horizontally or at any other angle and that the pump may be used for pumping liquids other than those normally thought of as lubricants.
The bearing elements 26 and 2B are made from some suitable bearing material such as Sabeco, whereas the casing elements may be made from any cheap material which may be formed, such as by casting or moulding.
While the form of embodiment of the invention as herein disclosed constitutes a preferred form, it is to be understood that other forms might be adopted, all coming within the scope of the claims which follow.
What is claimed is as follows:
1. In a pump, means forming a pumping cylinder, cylinder heads disposed on opposite sides thereof, a pair of pumping gears within said cylinder, shaft means projecting from opposite sides of each of said. gears into said. cylinder heads, said cylinder heads including bearing inserts for said shaft means, said b'earing inserts having substantially identical outer dimensions, a passage in one of said bearing inserts through which fluid to be pumped enters into said pumping cylinder, said shaft means including a drive shaft projecting through one of said cylinder heads, an outboard shaft seal for said drive shaft including a pair of relatively rotatable seal rings having seal surfaces in engagement with one another, means including a lubricant passage in said drive shaft whereby lubricant is centrifugally discharged to said shaft seal from a point substantially opposite said seal surfaces and means whereby the excess lubricant supplied to said seal surfaces is thereafter introduced into said pumping cylinder.
2. In a lubricant pump, means forming a lubricant pumping cylinder, cylinder heads disposed on opposite sides thereof, a pair of pumping gears in said cylinder, shaft means projecting from opposite sides of each of said gears into said cylinder heads, said shaft means including a drive shaft projecting through one of said cylinder heads, a shaft seal for preventing the escape of lubricant along said drive shaft, said cylinder heads including bearing inserts for said shaft means, a low pressure lubricant inl t. a h p 4 i sure lubricant outlet, a shaft seal lubricating cavity, lubricant collecting reservoirs at the outer ends of said bearing inserts for collecting the lubricant escaping from said cylinder along said shaft means, one of said reservoirs communicating with said low pressure lubricant inlet, means for conveying lubricant from another of said reservoirs through one of said shafts and into said cavity, and means for returning lubricant from said cavity to said low pressure lubricant inlet;
3. In apump, means forming a pumping cylinder, cylinder heads disposed on opposite sides thereof, a pair of pumping gears in said cylinder, shaft means projecting from opposite sides of each of said gears into said cylinder heads, said shaft means including a drive shaft projecting through one of said cylinder heads, a shaft seal for preventing the escape of lubricant along said drive shaft, a low pressure inlet, a high pressure outlet, a shaft seal lubricating cavity, lubricant collecting reservoirs adjacent the outer ends of said shaft means for collecting the lubricant escaping from said cylinder along said shaft means, one of said reservoirs communicating with said low pressure lubricant inlet, means for conveying lubricant from another of said reservoirs through one of said shafts and into said cavity, and means for returning lubricant from said cavity to said low pressure inlet.
4. In a pump, means forming a pumping cylinder, cylinder heads disposed on opposite sides thereof, pumping means in said cylinder, shaft means extending from opposite sides of said pumping means into said cylinder heads, said shaft means including a drive shaft projecting through one of said heads, a shaft seal adjacent the projecting end of said shaft for preventing the escape of lubricant along said drive shaft, a suction port, an outlet port, means forming a shaft seal lubricating cavity adjacent said suction port and in communication with said suction port, means forming a lubricant collecting reservoir at the inner end of said drive shaft for collecting the lubricant escaping from said cylinder along said drive shaft, said drive shaft being provided with a lubricant passage for con veying lubricant from said lubricant collecting reservoir at the inner end of the drive shaft to said shaft seal lubricating cavity.
ALBERT E. KOFFER.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS
US466844A 1942-11-25 1942-11-25 Gear pump for aeronautical apparatus Expired - Lifetime US2432576A (en)

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2710205A (en) * 1952-03-18 1955-06-07 Ingersoll Rand Co Sealing device for rotary pump shafts
US2873127A (en) * 1956-03-01 1959-02-10 Worthington Corp Mechanical seal
US2993230A (en) * 1958-05-05 1961-07-25 American Enka Corp Melt-spinning system
US3157404A (en) * 1962-03-19 1964-11-17 Jabsco Pump Co Shaft seal with corrugated frustoconical spring for driving or restraining sealing member
US4629405A (en) * 1979-08-10 1986-12-16 Hoechst Aktiengesellschaft Gear pump having an automatic lubricator
US5251914A (en) * 1987-05-28 1993-10-12 Tatum David M Sealing assembly for relatively movable members
US6135741A (en) * 1998-12-23 2000-10-24 Parker-Hannifin Corporation Recirculating flow path for gear pump
US20090191078A1 (en) * 2008-01-29 2009-07-30 Dario Colombo Lubricating pump

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1379587A (en) * 1919-08-16 1921-05-24 Doherty Res Co Pump
DE426666C (en) * 1924-05-06 1926-03-16 Fr August Neidig Axis bearings for two and multi-axis capsule machines
US1894943A (en) * 1928-04-25 1933-01-24 Rotorite Corp Sealed coupling
DE572631C (en) * 1931-03-01 1933-03-18 Tavannes Watch Co Sa Gear pump
US2105428A (en) * 1934-06-02 1938-01-11 Brown & Sharpe Mfg Gear pump seal
US2127151A (en) * 1935-03-23 1938-08-16 York Ice Machinery Corp Sealed joint for rotary shafts
US2202913A (en) * 1938-03-18 1940-06-04 Pump Engineering Service Corp Gear pump
US2302966A (en) * 1940-01-02 1942-11-24 Bendix Aviat Corp Pump
US2329990A (en) * 1942-02-12 1943-09-21 Ingersoll Rand Co Sealing device

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1379587A (en) * 1919-08-16 1921-05-24 Doherty Res Co Pump
DE426666C (en) * 1924-05-06 1926-03-16 Fr August Neidig Axis bearings for two and multi-axis capsule machines
US1894943A (en) * 1928-04-25 1933-01-24 Rotorite Corp Sealed coupling
DE572631C (en) * 1931-03-01 1933-03-18 Tavannes Watch Co Sa Gear pump
US2105428A (en) * 1934-06-02 1938-01-11 Brown & Sharpe Mfg Gear pump seal
US2127151A (en) * 1935-03-23 1938-08-16 York Ice Machinery Corp Sealed joint for rotary shafts
US2202913A (en) * 1938-03-18 1940-06-04 Pump Engineering Service Corp Gear pump
US2302966A (en) * 1940-01-02 1942-11-24 Bendix Aviat Corp Pump
US2329990A (en) * 1942-02-12 1943-09-21 Ingersoll Rand Co Sealing device

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2710205A (en) * 1952-03-18 1955-06-07 Ingersoll Rand Co Sealing device for rotary pump shafts
US2873127A (en) * 1956-03-01 1959-02-10 Worthington Corp Mechanical seal
US2993230A (en) * 1958-05-05 1961-07-25 American Enka Corp Melt-spinning system
US3157404A (en) * 1962-03-19 1964-11-17 Jabsco Pump Co Shaft seal with corrugated frustoconical spring for driving or restraining sealing member
US4629405A (en) * 1979-08-10 1986-12-16 Hoechst Aktiengesellschaft Gear pump having an automatic lubricator
US5251914A (en) * 1987-05-28 1993-10-12 Tatum David M Sealing assembly for relatively movable members
US6135741A (en) * 1998-12-23 2000-10-24 Parker-Hannifin Corporation Recirculating flow path for gear pump
US20090191078A1 (en) * 2008-01-29 2009-07-30 Dario Colombo Lubricating pump
EP2085616A1 (en) * 2008-01-29 2009-08-05 Agusta S.p.A. Combined scavenging roots pump and feed pump
US8113803B2 (en) 2008-01-29 2012-02-14 Agusta S.P.A. Lubricating system for aircraft drive

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