US2767658A - Multiple unit pump having frangible shear sections - Google Patents
Multiple unit pump having frangible shear sections Download PDFInfo
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- US2767658A US2767658A US517717A US51771755A US2767658A US 2767658 A US2767658 A US 2767658A US 517717 A US517717 A US 517717A US 51771755 A US51771755 A US 51771755A US 2767658 A US2767658 A US 2767658A
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- pump
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- driver gear
- shaft
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- 210000003739 neck Anatomy 0.000 description 24
- 230000008878 coupling Effects 0.000 description 18
- 238000010168 coupling process Methods 0.000 description 18
- 238000005859 coupling reaction Methods 0.000 description 18
- 238000005086 pumping Methods 0.000 description 7
- 230000002159 abnormal effect Effects 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 239000000446 fuel Substances 0.000 description 3
- 239000000543 intermediate Substances 0.000 description 3
- 238000007789 sealing Methods 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 230000007246 mechanism Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 240000007594 Oryza sativa Species 0.000 description 1
- 235000007164 Oryza sativa Nutrition 0.000 description 1
- 230000000415 inactivating effect Effects 0.000 description 1
- 235000009566 rice Nutrition 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D13/00—Pumping installations or systems
- F04D13/02—Units comprising pumps and their driving means
Definitions
- This invention relates generally to fuel pumps and more particularly relates to a multiple unit pump including two separate gear units in series staged relation with a centrifugal pump unit, all of the impellers being enclosed within a common housing :and being interrelated by a common driving mechanism particularly characterized by shear sections which will insure continued operation of related pairs of impellers despite jamming or seizure of one of the pumping units.
- Another object of the present invention is to provide a multiple pump which is particularly reliable for use as a fuel pump in an aircraft engine.
- Yet another object of the present invention is to provide a combination centrifugal-gear pump wherein the different impellers are interconnected by a common driving mechanism having improved structural and functional characteristics.
- the single gure of the drawings illustrates a crosssectional view of a multiple pump incorporating the structural features of the present invention.
- the multiple pump of the present invention is indicated generally at 10 and comprises a plurality of longitudinally aligned casing sections indicated at 11, 12, 13, 14, 16 and 17, respectively. All of the casing sections 11-17 are interconnected by suitable fasteners and it will be appreciated that the usual sealing members, such the O rings indicated at 18, are used to eifect a seal-tight assembly of the various pump components.
- the housing section 17 is formed to provide a pump inlet 19 adapted to communicate with a source of fuel supply.
- the housing sections 16 and 17 together form a volute pumping chamber 20 lin which is rotated a centrifugal impeller 21, thereby to initially pnessurize iiuid admitted into the pump through the inlet 19.
- the housing sections 11-14 are formed to provide la pair 'of adjacent pumping cavities 22 and 23, each of which receiving a pair of intermeshing gears including driven gears 24 and 26 and a pair of driver gears 27 iand 28.
- the gears 24, 27 cooperate to move fluid from the inlet side of the pumping cavity 22 to the outlet side thereof and the gears 26, 28 cooperate to impel fluid from the inlet Kside of the pumping chamber 23 to the outlet side thereof.
- gear units 24, 27 and 26, 28 are conveniently placed in series staged relation with the centrifugal impeller 21 and that the pump 10 is provided with a conventional outlet arrangement whereby the pumping medium initially pressurized by the centrifugal impeller 21 and subsequently pressurized by the gear units 24, 27 and 26, 28 is discharged to the ultimate point of utilization.
- the pump 10 is provided with a conventional outlet arrangement whereby the pumping medium initially pressurized by the centrifugal impeller 21 and subsequently pressurized by the gear units 24, 27 and 26, 28 is discharged to the ultimate point of utilization.
- additional details of the pumping flow relation between the pump inlet 19 yand the pump outlet is not believed to be necessary to the understanding of the principles of the present invention.
- the gear units of the pump Ml are preferably of the so-called pressure loaded type, each of the gears being associated with a movable pressure loaded bushing 30 having a sealing face 31 for engaging and sealing against an adjoining side face of a corresponding gear and having a :motive surface 32 spaced from an -adjoining wall of the pump casing, in this instance the casing sections 13, to form together therewith a pressure control chamber 33.
- the pressure control chamber 33 communicates with pump discharge in the usual manner to effect pressure loading of the movable bushings against the gears.
- each ⁇ of the driver gears 27 and 28, ⁇ as well as the centrifugal impeller 21, is driven in common from a single power take-olf.
- the casing section 11 is closed by a cover member 34 suitably bored and counterbored to seat and retain a thrust ring 36 as well as a bearing and seal assembly 37 for rotatably journalling a first driving member indicated generally at 38.
- the driving Imember 38 more particularly has a splined shaft portion 39 extending outwardly of the cover member 34 which is adapted to be coupled to a suitable prime mover.
- the driving member 38 has a neck portion 40 inwardly of the splined portion 39 which terminates in a radially outwardly extending bearing surface 41 engaging against the thrust ring 36.
- Extending inwardly into the pump and specifically into the hollow cavity 42 formed within the casing section 11 is an annular collar portion 43 formed as an integral part of the driving member 38.
- the collar portion 43 is splined as at 44 along the inner wall surf-face and therewith effects a driving relation with a correspondingly splined end portion 46 on a quill shaft 47.
- the splined end portion 46 of the quill shaft 47 telescopes into the collar portion 43.
- a coil spring 48 has -one end bottomed against the driving member 38 and has its opposite end bottomed against the end of the quill shaft 47.
- the quill shaft 47 is sutiiciently small in diameter to extend freely through a hollow bore 49 formed in the driver gear 27 as well as through a bore portion 50 formed in the driver gear 28.
- the collar portion 43 is provided with a second internal splined portion indicated at 51 which lies axially adjacent the splined portion 44 and which telescopically engages a shaft extension 52 formed on the driver gear 27.
- shaft extension 52 has a correspondingly splined external coupling portion whereby the driver gear 27 and the driving member 38 are interconnected in co-rotatable relation.
- the collar portion 43 of the driving member 38 is provided with a shear neck 53.
- the shear neck 53 will break and the end of the collar portion 43 coextensive with the splined portion 51 will, in effect, be disconnected from the driving member 38. In such event, the driving member will continue to drive the quill shaft 47 without interruption through the splined portion 44 of the collar portion 43.
- the gear 28 is provided with a shaft extension 60 which extends out of the housing section 14 into a cavity 61 formed in the housing section 16.
- the cavity 61 in effect, functions as a gear casing since a gear 62 is keyed as at 63 to the shaft extension 60 for co-rotation with the driver gear 28.
- the gear 62 meshes with a gear 64 journalled on a reduced neck 66 integrally formed as a shaft extension on the driven gear 26.
- a bearing sleeve 67 is interposed between the neck 66 of the gear 64 whereby the gear 64 and the driven gear 26 may rotate at different rotational speeds.
- the gear units 24, 27 and 26, 28 ⁇ should be rotated at a much slower speed than the centrifugal impeller 21, the rotating characteristics of the two types of impellers being different. Accordingly, the gear 62 is much larger in diameter than the gear 64 so that a speed increase will occur in the gear train within the gear case 61 to rotate the centrifugal impeller 21 at relatively high speeds.
- the centrifugal impeller 21 is connected for co-rotation with the gear 64, for ex ample, the gear 64 has an extended portion 68 to which the ⁇ impeller 21 is keyed as at 69 and fastened as at 70.
- the gear member 64 is independently journalled by suitable bearing means 71 in the casing section 16.
- the shaft extension 6i) on the driver gear 2S is particularly characterized by the formation of shear neck 72.
- the shear neck 72 is formed axially adjacent an internally splined portion 73 formed in the end of the bore 50 of the driver gear 28 and cooperating with an externally splined driving portion 74 formed on the end of the quill shaft 47.
- the shear neck 72 is located at some point between the shaft extension 60 of the hub of the ⁇ driver gear 28.
- the quill shaft 47 is also characterized, according to the present invention, by the formation of a shear neck 76 formed adjacent the splined portion 74 and preferably between the opposite ends of the quill shaft 47.
- a multiple pump having three longitudinally spaced co-axi'ally aligned rotatable members provided by a driv ing member,a first driver gear inwardly adjacent thereto, and a second driver vgear inwardly adjacent said first driver gear, respectively, a collar connecting said driving member and said first driver gear and having a first reduced 'shear neck formed therein outwardly of its connection to said first driver gear, a shaft Vmember connected to said second driver gear and extending outwardly through said first driver gear for connection to said driving member outwardly of said first shear neck, a fourth rotatable centrifugal impeller member, means forming a coupling and effecting a driving connection between.
- said second driver ⁇ gear and said fourth rotatable centrifugal impeller member for unison rotation
- said second ⁇ driver gear having a second reduced shear neck formed therein between said driving connection for said fourth rotatable centrifugal impeller member and said second driver gear
- said shaft member having a third reduced shear neck formed therein intermediate the connections to ⁇ said second driver gear and said driving member thereof, said first and second shear necks yielding selectively under abnormal load to permit uninterrupted operation of either one of said first and second driver gears in combination with said fourth rotatable centrifugal impeller member upon binding of the other, said third shear neck yielding under abnormal load upon said fourth rotatable centrifugal impeller member.
- a multiple pump comprising a casing having an opening at one end, a cover on said casing for said opening, at .least three longitudinally spaced co-axially aligned rotatablev members provided by a first driving member extending through said casing, a first driver gear inwardly adjacent said driving member and a second driver gear inwardly adjacent said first driver gear, respectively, said second driver gear having a shaft extension extending inwardly adjacent said second driver gear, gear train means connected to said shaft extension, a centrifugal impeller driven by said gear train means, a collar connected to said driving member and said first driver gear, said collar having a reduced shear neck formed therein outwardly of its connection to said rst driver gear providing a first frangible coupling, said driver gears having bores extending therethrough and a shaft connected to said second driver gear in the bore thereof and extending outwardly through said bore of said first driver gear and being connected to said driving member outwardly of said first frangible coupling, said shaft being coupled to said shaft extension of
- a first driving member a first driver gear longitudinally adjacent said driving member and a second driver gear longitudinally adjacent said first driver gear, respectively, said second driver gear having a shaft extension extending longitudinally adjacent said second driver gear, coupling means connected to said shaft extension, a centrifugal impeller driven by said coupling means, a collar connected to said driving member and said first driver gear, said collar having a reduced shear neck formed therein outwardly of its con nection to said firstdriver gear providing a first frangible coupling, said driver gears having bores extending therethrough and a shaft connected to said second driver gear in the bore thereof and extending outwardly through said bore of said first driver gear and being connected to said driving member outwardly of said first frangible coupling, a coupling connection between said shaft and said shaft extension of said second driver gear, said shaft extension having a second reduced shear neck formed therein between said second driver gear and said coupling connection, said shaft having a third reduced shear neck formed therein intermediate the connections thereof to said coupling
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Rotary Pumps (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
Oct. 23, 1 956 U J. F. MURRAY 2,767,658
MULTIPLE UNIT PUMP HAVING PRANGTBLE SHEAR sEcTloNs Fild June 24, 1955 Z: 177 ME75 United States Patent MULTIPLE UNIT PUMP HAVING FRANGIBLE SI-IEAR SECTIONS John F. Murray, Northfield, Ohio, assignor to Thompson Products, Inc., Cleveland, Ohio, a corporation of Ohio Application June 24, 195s, serial No. 517,717
s Claims. (c1. s-4) This invention relates generally to fuel pumps and more particularly relates to a multiple unit pump including two separate gear units in series staged relation with a centrifugal pump unit, all of the impellers being enclosed within a common housing :and being interrelated by a common driving mechanism particularly characterized by shear sections which will insure continued operation of related pairs of impellers despite jamming or seizure of one of the pumping units.
It is an fobject of the present invention to provide an improved multiple pump assembly specifically characterized by advantageous safety features.
Another object of the present invention is to provide a multiple pump which is particularly reliable for use as a fuel pump in an aircraft engine.
Yet another object of the present invention is to provide a combination centrifugal-gear pump wherein the different impellers are interconnected by a common driving mechanism having improved structural and functional characteristics.
Many other features, advantages and additional objects of the present invention will become manifest to those versed in the art upon making reference to the detailed description which follows and the accompanying sheet of drawings in which a preferred structural embodiment of a multiple pump incorporating the principles of the present invention is shown by way of illustrative example.
On the drawings:
The single gure of the drawings illustrates a crosssectional view of a multiple pump incorporating the structural features of the present invention.
As shown on the drawings:
The multiple pump of the present invention is indicated generally at 10 and comprises a plurality of longitudinally aligned casing sections indicated at 11, 12, 13, 14, 16 and 17, respectively. All of the casing sections 11-17 are interconnected by suitable fasteners and it will be appreciated that the usual sealing members, such the O rings indicated at 18, are used to eifect a seal-tight assembly of the various pump components.
The housing section 17 is formed to provide a pump inlet 19 adapted to communicate with a source of fuel supply. The housing sections 16 and 17 together form a volute pumping chamber 20 lin which is rotated a centrifugal impeller 21, thereby to initially pnessurize iiuid admitted into the pump through the inlet 19.
The housing sections 11-14 are formed to provide la pair 'of adjacent pumping cavities 22 and 23, each of which receiving a pair of intermeshing gears including driven gears 24 and 26 and a pair of driver gears 27 iand 28. The gears 24, 27 cooperate to move fluid from the inlet side of the pumping cavity 22 to the outlet side thereof and the gears 26, 28 cooperate to impel fluid from the inlet Kside of the pumping chamber 23 to the outlet side thereof. Those versed in the art will appreciate that the gear units 24, 27 and 26, 28 are conveniently placed in series staged relation with the centrifugal impeller 21 and that the pump 10 is provided with a conventional outlet arrangement whereby the pumping medium initially pressurized by the centrifugal impeller 21 and subsequently pressurized by the gear units 24, 27 and 26, 28 is discharged to the ultimate point of utilization. For that rice reason, additional details of the pumping flow relation between the pump inlet 19 yand the pump outlet is not believed to be necessary to the understanding of the principles of the present invention.
The gear units of the pump Ml are preferably of the so-called pressure loaded type, each of the gears being associated with a movable pressure loaded bushing 30 having a sealing face 31 for engaging and sealing against an adjoining side face of a corresponding gear and having a :motive surface 32 spaced from an -adjoining wall of the pump casing, in this instance the casing sections 13, to form together therewith a pressure control chamber 33. The pressure control chamber 33 communicates with pump discharge in the usual manner to effect pressure loading of the movable bushings against the gears.
According to the principles of the present invention, each `of the driver gears 27 and 28, `as well as the centrifugal impeller 21, is driven in common from a single power take-olf. Referring to the lefthand side of the drawing, it will be noted that the casing section 11 is closed by a cover member 34 suitably bored and counterbored to seat and retain a thrust ring 36 as well as a bearing and seal assembly 37 for rotatably journalling a first driving member indicated generally at 38. The driving Imember 38 more particularly has a splined shaft portion 39 extending outwardly of the cover member 34 which is adapted to be coupled to a suitable prime mover.
The driving member 38 has a neck portion 40 inwardly of the splined portion 39 which terminates in a radially outwardly extending bearing surface 41 engaging against the thrust ring 36. Extending inwardly into the pump and specifically into the hollow cavity 42 formed within the casing section 11 is an annular collar portion 43 formed as an integral part of the driving member 38. The collar portion 43 is splined as at 44 along the inner wall surf-face and therewith effects a driving relation with a correspondingly splined end portion 46 on a quill shaft 47. The splined end portion 46 of the quill shaft 47 telescopes into the collar portion 43. A coil spring 48 has -one end bottomed against the driving member 38 and has its opposite end bottomed against the end of the quill shaft 47. The quill shaft 47 is sutiiciently small in diameter to extend freely through a hollow bore 49 formed in the driver gear 27 as well as through a bore portion 50 formed in the driver gear 28.
The collar portion 43 is provided with a second internal splined portion indicated at 51 which lies axially adjacent the splined portion 44 and which telescopically engages a shaft extension 52 formed on the driver gear 27.
It will be understood that the shaft extension 52 has a correspondingly splined external coupling portion whereby the driver gear 27 and the driving member 38 are interconnected in co-rotatable relation.
Between the splined portions 44 and 51, the collar portion 43 of the driving member 38 is provided with a shear neck 53. Thus, if for any reason the gear pump units 24, 27 jam or seize or become otherwise inoperative, thereby setting up abnormal load conditions, the shear neck 53 will break and the end of the collar portion 43 coextensive with the splined portion 51 will, in effect, be disconnected from the driving member 38. In such event, the driving member will continue to drive the quill shaft 47 without interruption through the splined portion 44 of the collar portion 43.
At the other end of the pump, the gear 28 is provided with a shaft extension 60 which extends out of the housing section 14 into a cavity 61 formed in the housing section 16. The cavity 61, in effect, functions as a gear casing since a gear 62 is keyed as at 63 to the shaft extension 60 for co-rotation with the driver gear 28.
The gear 62 meshes with a gear 64 journalled on a reduced neck 66 integrally formed as a shaft extension on the driven gear 26. A bearing sleeve 67 is interposed between the neck 66 of the gear 64 whereby the gear 64 and the driven gear 26 may rotate at different rotational speeds.
For greatest efficiency, the gear units 24, 27 and 26, 28 `should be rotated at a much slower speed than the centrifugal impeller 21, the rotating characteristics of the two types of impellers being different. Accordingly, the gear 62 is much larger in diameter than the gear 64 so that a speed increase will occur in the gear train within the gear case 61 to rotate the centrifugal impeller 21 at relatively high speeds.
It will be appreciatedthat the centrifugal impeller 21 is connected for co-rotation with the gear 64, for ex ample, the gear 64 has an extended portion 68 to which the` impeller 21 is keyed as at 69 and fastened as at 70. The gear member 64 is independently journalled by suitable bearing means 71 in the casing section 16.
According to the principles of the present invention, the shaft extension 6i) on the driver gear 2S is particularly characterized by the formation of shear neck 72. The shear neck 72 is formed axially adjacent an internally splined portion 73 formed in the end of the bore 50 of the driver gear 28 and cooperating with an externally splined driving portion 74 formed on the end of the quill shaft 47. Preferably, the shear neck 72 is located at some point between the shaft extension 60 of the hub of the` driver gear 28. Thus, if an abnormal load occurs because of binding or seizure of the gear pump unit 26, 28, the shear neck 72 will sever inactivating the pump unit 26, 28 while permitting the gear pump unit 24, 27
to operate in conjunction with the centrifugal impeller 21.`
The quill shaft 47 is also characterized, according to the present invention, by the formation of a shear neck 76 formed adjacent the splined portion 74 and preferably between the opposite ends of the quill shaft 47. Thus, if an abnormal load is developed because of binding or seizure of the centrifugal impeller 211, only the quill shaft 47 will be broken, a separate part which can be conveniently replaced without requiring disassembly of the entire pump and without requiring replacement of any of the expensive gear parts of the pump 10. Moreover, any broken parts of the quill shaft 47 can be conveniently removed from the pump merely by removing the cover member 34 at the end of the casing.
Although various minor modifications might be suggested by those versed in the art, it should be understood that I wish to embody within the scope of the patent warranted hereon all such modifications as reasonably and properly come within the scope of my contribution to the art.
I claim as my invention:
l.` A multiple pump having three longitudinally spaced co-axi'ally aligned rotatable members provided by a driv ing member,a first driver gear inwardly adjacent thereto, and a second driver vgear inwardly adjacent said first driver gear, respectively, a collar connecting said driving member and said first driver gear and having a first reduced 'shear neck formed therein outwardly of its connection to said first driver gear, a shaft Vmember connected to said second driver gear and extending outwardly through said first driver gear for connection to said driving member outwardly of said first shear neck, a fourth rotatable centrifugal impeller member, means forming a coupling and effecting a driving connection between. said second driver `gear and said fourth rotatable centrifugal impeller member for unison rotation, said second `driver gear having a second reduced shear neck formed therein between said driving connection for said fourth rotatable centrifugal impeller member and said second driver gear, said shaft member having a third reduced shear neck formed therein intermediate the connections to `said second driver gear and said driving member thereof, said first and second shear necks yielding selectively under abnormal load to permit uninterrupted operation of either one of said first and second driver gears in combination with said fourth rotatable centrifugal impeller member upon binding of the other, said third shear neck yielding under abnormal load upon said fourth rotatable centrifugal impeller member.
2. A multiple pump comprising a casing having an opening at one end, a cover on said casing for said opening, at .least three longitudinally spaced co-axially aligned rotatablev members provided by a first driving member extending through said casing, a first driver gear inwardly adjacent said driving member and a second driver gear inwardly adjacent said first driver gear, respectively, said second driver gear having a shaft extension extending inwardly adjacent said second driver gear, gear train means connected to said shaft extension, a centrifugal impeller driven by said gear train means, a collar connected to said driving member and said first driver gear, said collar having a reduced shear neck formed therein outwardly of its connection to said rst driver gear providing a first frangible coupling, said driver gears having bores extending therethrough and a shaft connected to said second driver gear in the bore thereof and extending outwardly through said bore of said first driver gear and being connected to said driving member outwardly of said first frangible coupling, said shaft being coupled to said shaft extension of said second driver gear, said shaft extension having a second reduced shear neck formed therein between said second driver gear and the coupling between said shaft and said shaft extension, said shaft having a third reduced shear neck formed therein inter mediate the connections to said second driver gear and said driving member thereof to provide a third frangible coupling, said first frangible coupling and said second shear neck yielding torsionally to permit uninterrupted operation of one of said driver gears in combination with said centrifugal impeller upon binding or seizure of the other, said third frangible coupling yielding torsionally upon binding or seizure of the centrifugal impeller.
3. in a multiple pump, a first driving member, a first driver gear longitudinally adjacent said driving member and a second driver gear longitudinally adjacent said first driver gear, respectively, said second driver gear having a shaft extension extending longitudinally adjacent said second driver gear, coupling means connected to said shaft extension, a centrifugal impeller driven by said coupling means, a collar connected to said driving member and said first driver gear, said collar having a reduced shear neck formed therein outwardly of its con nection to said firstdriver gear providing a first frangible coupling, said driver gears having bores extending therethrough and a shaft connected to said second driver gear in the bore thereof and extending outwardly through said bore of said first driver gear and being connected to said driving member outwardly of said first frangible coupling, a coupling connection between said shaft and said shaft extension of said second driver gear, said shaft extension having a second reduced shear neck formed therein between said second driver gear and said coupling connection, said shaft having a third reduced shear neck formed therein intermediate the connections thereof to said coupling connection and to said driving member to provide a third frangible coupling, said first frangible coupling and said second shear neck yielding torsionally to permit uninterrupted operation of one of said driver gears in combination with said centrifugal impeller upon binding orseizure of the other, said third frangible coupling yielding torsionally upon binding or seizure of the centrifugal impeller.
References Cited in the file of this patent UNITED STATES PATENTS V2,625,106 Hoffman Ian. 13, 1953 2,665,637 Lauck Jan. 12, 1954 2,665,638 Lauck Jan. 12, 1954 2,699,724 Murray et al. Jan. 1S, `1955 2,726,604 Aspelin et a1 Dec. 13, 1955
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US517717A US2767658A (en) | 1955-06-24 | 1955-06-24 | Multiple unit pump having frangible shear sections |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US517717A US2767658A (en) | 1955-06-24 | 1955-06-24 | Multiple unit pump having frangible shear sections |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2767658A true US2767658A (en) | 1956-10-23 |
Family
ID=24060938
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US517717A Expired - Lifetime US2767658A (en) | 1955-06-24 | 1955-06-24 | Multiple unit pump having frangible shear sections |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2767658A (en) |
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2941473A (en) * | 1955-05-17 | 1960-06-21 | Thompson Ramo Wooldridge Inc | Coupling apparatus for a multiple unit fuel pump |
| US2950046A (en) * | 1956-01-28 | 1960-08-23 | Heraeus Gmbh W C | High vacuum pump |
| US2957418A (en) * | 1957-01-28 | 1960-10-25 | William V Edwards | Gear fuel pump |
| US3008426A (en) * | 1957-01-28 | 1961-11-14 | Thompson Ramo Wooldridge Inc | Gear fuel pump |
| US3026810A (en) * | 1956-09-12 | 1962-03-27 | Borg Warner | Variable displacement pump |
| US3037455A (en) * | 1957-09-04 | 1962-06-05 | Ford Motor Co | Pumps |
| US3045899A (en) * | 1958-06-05 | 1962-07-24 | Nat Tank Co | Motor-compressor unit |
| US3093081A (en) * | 1959-01-29 | 1963-06-11 | New York Air Brake Co | Pumping device |
| US3547557A (en) * | 1968-10-14 | 1970-12-15 | Chandler Evans Inc | Fluid pump and delivery system |
| US3589836A (en) * | 1968-11-04 | 1971-06-29 | Trw Inc | Unitized pump system |
| US4439109A (en) * | 1980-12-05 | 1984-03-27 | Plessey Overseas Limited | Pump for pumping a liquid containing solid contaminants |
| US4553914A (en) * | 1984-02-24 | 1985-11-19 | Chandler Evans Inc. | Method and apparatus for main fuel pumping system having backup pump |
| US4859156A (en) * | 1986-07-23 | 1989-08-22 | Sanden Corporation | Coupling mechanism for a compressor |
| US20150377235A1 (en) * | 2014-06-26 | 2015-12-31 | Snecma | Two stage pump, particularly provided as main pump for supplying an aircraft engine with fuel |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2625106A (en) * | 1950-09-12 | 1953-01-13 | Gen Electric | Composite pump for prime mover oil systems |
| US2665637A (en) * | 1947-05-07 | 1954-01-12 | Borg Warner | Pumping system |
| US2665638A (en) * | 1949-10-21 | 1954-01-12 | Borg Warner | Gear pump |
| US2699724A (en) * | 1950-06-14 | 1955-01-18 | Thompson Prod Inc | Multiple gear pump |
| US2726604A (en) * | 1951-06-15 | 1955-12-13 | Thompson Prod Inc | Mixed flow multiple pump |
-
1955
- 1955-06-24 US US517717A patent/US2767658A/en not_active Expired - Lifetime
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2665637A (en) * | 1947-05-07 | 1954-01-12 | Borg Warner | Pumping system |
| US2665638A (en) * | 1949-10-21 | 1954-01-12 | Borg Warner | Gear pump |
| US2699724A (en) * | 1950-06-14 | 1955-01-18 | Thompson Prod Inc | Multiple gear pump |
| US2625106A (en) * | 1950-09-12 | 1953-01-13 | Gen Electric | Composite pump for prime mover oil systems |
| US2726604A (en) * | 1951-06-15 | 1955-12-13 | Thompson Prod Inc | Mixed flow multiple pump |
Cited By (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2941473A (en) * | 1955-05-17 | 1960-06-21 | Thompson Ramo Wooldridge Inc | Coupling apparatus for a multiple unit fuel pump |
| US2950046A (en) * | 1956-01-28 | 1960-08-23 | Heraeus Gmbh W C | High vacuum pump |
| US3026810A (en) * | 1956-09-12 | 1962-03-27 | Borg Warner | Variable displacement pump |
| US2957418A (en) * | 1957-01-28 | 1960-10-25 | William V Edwards | Gear fuel pump |
| US3008426A (en) * | 1957-01-28 | 1961-11-14 | Thompson Ramo Wooldridge Inc | Gear fuel pump |
| US3037455A (en) * | 1957-09-04 | 1962-06-05 | Ford Motor Co | Pumps |
| US3045899A (en) * | 1958-06-05 | 1962-07-24 | Nat Tank Co | Motor-compressor unit |
| US3093081A (en) * | 1959-01-29 | 1963-06-11 | New York Air Brake Co | Pumping device |
| US3547557A (en) * | 1968-10-14 | 1970-12-15 | Chandler Evans Inc | Fluid pump and delivery system |
| US3589836A (en) * | 1968-11-04 | 1971-06-29 | Trw Inc | Unitized pump system |
| US4439109A (en) * | 1980-12-05 | 1984-03-27 | Plessey Overseas Limited | Pump for pumping a liquid containing solid contaminants |
| US4553914A (en) * | 1984-02-24 | 1985-11-19 | Chandler Evans Inc. | Method and apparatus for main fuel pumping system having backup pump |
| US4859156A (en) * | 1986-07-23 | 1989-08-22 | Sanden Corporation | Coupling mechanism for a compressor |
| US20150377235A1 (en) * | 2014-06-26 | 2015-12-31 | Snecma | Two stage pump, particularly provided as main pump for supplying an aircraft engine with fuel |
| US9752575B2 (en) * | 2014-06-26 | 2017-09-05 | Snecma | Two stage pump, particularly provided as main pump for supplying an aircraft engine with fuel |
| GB2529301B (en) * | 2014-06-26 | 2020-12-16 | Snecma | Two stage pump, particularly provided as main pump for supplying an aircraft engine with fuel |
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