GB762328A - Improvements in or relating to fuel pumping systems for aero engines - Google Patents
Improvements in or relating to fuel pumping systems for aero enginesInfo
- Publication number
- GB762328A GB762328A GB25526/54A GB2552654A GB762328A GB 762328 A GB762328 A GB 762328A GB 25526/54 A GB25526/54 A GB 25526/54A GB 2552654 A GB2552654 A GB 2552654A GB 762328 A GB762328 A GB 762328A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pump
- gear
- pumps
- centrifugal
- stage
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- D—TEXTILES; PAPER
- D05—SEWING; EMBROIDERING; TUFTING
- D05B—SEWING
- D05B19/00—Programme-controlled sewing machines
Landscapes
- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Sewing Machines And Sewing (AREA)
- Rotary Pumps (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
762,328. Centrifugal pumps; gear pumps; gas turbine and jet propulsion plant. THOMPSON PRODUCTS, Inc. Sept. 2, 1954 [Nov. 19, 1953], No. 25526/54. Classes 110 (1), 110 (2) and 110(3). A fuel pumping system for an aircraft engine having a burner unit comprises a multi-stage pump having a casing formed with an opening by means of which a by-pass duct is connected between the discharge side of the final pump stage and a point of intermediate pressure between successive stages of the pump. Preferably, the pump comprises a centrifugal first stage, followed by a gear, piston or other positive-displacement stage. Any stage may comprise pumps in parallel. The discharge may pass through a heat exchanger to cool oil used to lubricate gear-boxes and bearings. Fig. 3 shows a centrifugal pump 1 feeding gear pumps 2a, 2b, 2c in parallel, the common discharge passing by way of a flow control unit 3 to the burners 4 of an aircraft gas turbine engine. At high altitude, excess fuel is by-passed from the control unit 3 by way of a duct 5 to a point P between the centrifugal and gear pump stages. The gear pumps 2a, 2b have additional by-pass ducts 9, 10 opened at predetermined altitudes by alltitude-responsive valves 11, 12 respectively. The gear pumps 2a and 2b may be of different capacities, to give the assembly some of the advantages of a variable-displacement pump. In Fig. 4, main burners 4 and reheat burners 4a are supplied by separate pump units, the by-pass ducts 5, 5a of which are interconnected at 15 through a constriction 16. This ensures that, even though the flow to the reheat burners 4a is cut off completely at the inlet to the pump 13a, the gear pumps 2a do not run completely dry. Non- return valves 14, 14a are provided. In a modification, Fig. 6 (not shown), the valves 14, 14a are omitted and the reheat fuel pump comprises one gear pump 2a instead of two, the flow through the by-pass duct of the reheat fuel pump being controlled by a valve which opens when the delivery pressure reaches the re-circulating value. In the embodiment shown in Fig. 5, the main and reheat pumps have a common centrifugal first stage 1a which forms part of the reheat pump. The main and reheat pump may be separately engine-driven or incorporated in a single unit having a common drive. Fig. 8 shows a fuel pump comprising a centrifugal first stage, followed by two gear pump stages operating in parallel. The input shaft 38 is splined to the tubular hub 36a of the driving gear 36 of one of the gear pumps, and is internally splined to one end of a solid shaft 40, the other end of which is splined to the tubular hub 34a of the driving gear 34 of the other gear pump. Shear necks 42, 43, 44 permit uninterrupted operation of one gear pump in the event of binding or seizure of the other gear pump. The impeller 23 of the centrifugal first stage is driven from the tubular hub 34a through gears 45, 46, the stub shaft 47 carrying the impeller being journalled on an extension 48 of the tubular hub of the driven gear 35 of the adjacent gear pump. Passages (not shown) are provided to connect the discharge of the centrifugal pump to the inlets of the gear pumps and to connect the outlets of the gear pumps, by way of non-return valves, to a common discharge. Each pump gear 34, 35, 36, 37 is journalled at one end in a bushing 49 which is pressed into sealing engagement with the gear by fuel at the discharge pressure, introduced into a chamber 52 through a passage (not shown). Initial loading of the bushings 49 is provided by springs 54.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US762328XA | 1953-11-19 | 1953-11-19 | |
DE336252X | 1954-11-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB762328A true GB762328A (en) | 1956-11-28 |
Family
ID=31979301
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB25526/54A Expired GB762328A (en) | 1953-11-19 | 1954-09-02 | Improvements in or relating to fuel pumping systems for aero engines |
GB32057/55A Expired GB792328A (en) | 1953-11-19 | 1955-11-09 | Improvements in or relating to sewing machines |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB32057/55A Expired GB792328A (en) | 1953-11-19 | 1955-11-09 | Improvements in or relating to sewing machines |
Country Status (5)
Country | Link |
---|---|
US (1) | US2854935A (en) |
BE (1) | BE542467A (en) |
CH (1) | CH336252A (en) |
FR (1) | FR1137737A (en) |
GB (2) | GB762328A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1219799B (en) * | 1956-12-11 | 1966-06-23 | Georg Wiggermann | Unit of two two-wheel gear pumps, the specific delivery rate of which is infinitely variable |
GB2282186A (en) * | 1993-09-08 | 1995-03-29 | Rolls Royce Plc | Engine fuel metering system. |
GB2289722A (en) * | 1994-05-28 | 1995-11-29 | Rolls Royce Plc | Fuel supply for turbojet with afterburner |
GB2529301B (en) * | 2014-06-26 | 2020-12-16 | Snecma | Two stage pump, particularly provided as main pump for supplying an aircraft engine with fuel |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL240408A (en) * | 1954-06-18 | |||
BE543000A (en) * | 1954-11-30 | |||
BE548219A (en) * | 1955-10-29 | |||
NL213731A (en) * | 1956-06-18 | |||
US3055325A (en) * | 1957-02-26 | 1962-09-25 | Nippon Sewing Machine Mfg Co L | Sewing machine |
FR1221351A (en) * | 1958-03-19 | 1960-06-01 | Pfaff Ag G M | Decorative stitch device for sewing machine |
CH372904A (en) * | 1958-07-15 | 1963-10-31 | Forster Geb | Sewing machine for sewing decorative stitches |
US3217677A (en) * | 1958-10-20 | 1965-11-16 | Janome Sewing Machine Co Ltd | Ornamental stitch sewing machine |
NL244529A (en) * | 1958-10-21 | |||
US3025809A (en) * | 1959-01-02 | 1962-03-20 | Singer Mfg Co | Automatic ornamental stitch sewing mechanisms |
DE1189838B (en) * | 1959-01-09 | 1965-03-25 | Forster Geb | Decorative stitch device for sewing machines |
US3067702A (en) * | 1959-01-27 | 1962-12-11 | Riccar Sewing Machine Co Ltd | Automatic and hand-operated apparatus for use in rotary type zigzag sewing machines |
US3254618A (en) * | 1959-02-02 | 1966-06-07 | Janome Sewing Machine Co Ltd | Buttonhole stitching control device |
US3053207A (en) * | 1959-10-01 | 1962-09-11 | Nippon Sewing Machine Mfg Co L | Sewing machine |
US3064603A (en) * | 1959-10-21 | 1962-11-20 | Fuji Seimitsu Kogyo Kabushiki | Speed-changing cam device for zigzag sewing machines |
US3073266A (en) * | 1959-11-23 | 1963-01-15 | Guide Anthony | Spiral stitching attachment for sewing machines |
US3081724A (en) * | 1959-12-31 | 1963-03-19 | Necchi Spa | Zig-zag sewing machine |
NL269013A (en) * | 1960-09-07 | |||
DE2132064A1 (en) * | 1971-06-28 | 1973-01-11 | Meister Werke Gmbh | SETUP ON A ZIG-ZAG OR AUTOMATIC SEWING MACHINE TO ADJUST STITCH POSITION AND STITCH WIDTH |
US3807329A (en) * | 1972-11-29 | 1974-04-30 | Singer Co | Integrated sewing machine controls |
EP0009107B1 (en) * | 1978-09-14 | 1984-06-13 | Dorina Nähmaschinen GmbH | Zigzag sewing machine with a device for producing decorative stitches |
US4385572A (en) * | 1981-02-02 | 1983-05-31 | Martin Redovian | Drop-in pattern stitch assembly for a straight stitch sewing machine |
JP6552233B2 (en) * | 2015-03-20 | 2019-07-31 | 蛇の目ミシン工業株式会社 | sewing machine |
CN105041605A (en) * | 2015-08-03 | 2015-11-11 | 中国石油大学(北京) | High-viscosity oil multi-pump station airtight pipeline conveying system |
USD836681S1 (en) * | 2017-09-18 | 2018-12-25 | Brother Industries, Ltd. | Sewing machine |
USD836680S1 (en) * | 2017-09-18 | 2018-12-25 | Brother Industries, Ltd. | Sewing machine |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1338074A (en) * | 1916-05-24 | 1920-04-27 | Singer Mfg Co | Embroidery-sewing machine |
US2713838A (en) * | 1953-05-25 | 1955-07-26 | Singer Mfg Co | Needle-vibration controlling mechanisms for zigzag stitch sewing machines |
US2297197A (en) * | 1938-05-31 | 1942-09-29 | Bolter Wilhelm | Zigzag sewing machine |
CH311160A (en) * | 1952-05-12 | 1955-11-30 | Turissa Naehmaschinenfabrik Ag | Sewing machine with zigzag device. |
-
0
- BE BE542467D patent/BE542467A/xx unknown
-
1954
- 1954-09-02 GB GB25526/54A patent/GB762328A/en not_active Expired
-
1955
- 1955-10-11 CH CH336252D patent/CH336252A/en unknown
- 1955-10-26 FR FR1137737D patent/FR1137737A/en not_active Expired
- 1955-11-07 US US545482A patent/US2854935A/en not_active Expired - Lifetime
- 1955-11-09 GB GB32057/55A patent/GB792328A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1219799B (en) * | 1956-12-11 | 1966-06-23 | Georg Wiggermann | Unit of two two-wheel gear pumps, the specific delivery rate of which is infinitely variable |
GB2282186A (en) * | 1993-09-08 | 1995-03-29 | Rolls Royce Plc | Engine fuel metering system. |
US5495715A (en) * | 1993-09-08 | 1996-03-05 | Rolls-Royce Plc | Engine fuel metering system |
GB2282186B (en) * | 1993-09-08 | 1997-09-24 | Rolls Royce Plc | Engine fuel metering system |
GB2289722A (en) * | 1994-05-28 | 1995-11-29 | Rolls Royce Plc | Fuel supply for turbojet with afterburner |
GB2289722B (en) * | 1994-05-28 | 1997-09-10 | Rolls Royce Plc | Fuel supply arrangement for turbojet engines with afterburner |
GB2529301B (en) * | 2014-06-26 | 2020-12-16 | Snecma | Two stage pump, particularly provided as main pump for supplying an aircraft engine with fuel |
Also Published As
Publication number | Publication date |
---|---|
CH336252A (en) | 1959-02-15 |
FR1137737A (en) | 1957-06-03 |
US2854935A (en) | 1958-10-07 |
GB792328A (en) | 1958-03-26 |
BE542467A (en) |
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