GB562925A - Improvements in or relating to fuel-pumping systems - Google Patents
Improvements in or relating to fuel-pumping systemsInfo
- Publication number
- GB562925A GB562925A GB222743A GB222743A GB562925A GB 562925 A GB562925 A GB 562925A GB 222743 A GB222743 A GB 222743A GB 222743 A GB222743 A GB 222743A GB 562925 A GB562925 A GB 562925A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shaft
- motor
- fuel
- pump
- impeller
- 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
- 238000005086 pumping Methods 0.000 title 1
- 239000000446 fuel Substances 0.000 abstract 5
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical group [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 abstract 1
- 230000004888 barrier function Effects 0.000 abstract 1
- 238000001816 cooling Methods 0.000 abstract 1
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
- F04D29/00—Details, component parts, or accessories
- F04D29/60—Mounting; Assembling; Disassembling
- F04D29/605—Mounting; Assembling; Disassembling specially adapted for liquid pumps
- F04D29/606—Mounting in cavities
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/14—Filling or emptying
- B64D37/16—Filling systems
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
- F02M37/04—Feeding by means of driven pumps
- F02M37/08—Feeding by means of driven pumps electrically driven
- F02M37/10—Feeding by means of driven pumps electrically driven submerged in fuel, e.g. in reservoir
- F02M37/103—Mounting pumps on fuel tanks
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
562,925. Fuel pumps. STEVENS, A. H. (Thompson Products, Inc.). Feb. 10, 1943, No. 2227. [Class 110 (i)] A fuel pump for aircraft &c. is mounted in a tank 11 formed between the upper and lower skins 14, 15 of the aeroplane, the support comprising a bracket 111 ... 113 fixed to the wall 13 and to an inset portion 110 of the skin 15. The motor 10 is in a liquid-tight casing connected to the pump casing 25 by a channel through which passes the lead 58 to the motor and which forms an inlet for cooling air drawn in to the motor casing by suction produced in a pipe 108 projecting into the slip stream from the space 69 between the motor or pump casings. The shaft 63 connecting motor and pump is sealed against leakage by a flexible ring 81 pressed between a fixed annulus 79 seated on a shoulder 68 and a screwed sleeve 82. In addition, a graphitic carbon ring 85 rotating with the shaft has sliding contact with 79, and is packed by a resilient washer 86 pressed against it by a spring 92 abutting on a cup 87 housing the washer. A flame barrier between the motor and pump comprises a sleeve 72, 74 loosely surrounding the shaft and a second sleeve 77 spaced from 74 and having a portion 76 gripping the shaft so as to rotate therewith. The shaft 63 is keyed to the impeller 91 by curved keys 98 engaging curved slots 96, 100 in the impeller and shaft respectively. The pump casing, has a cap 34, by removing which the impeller may be removed from the shaft. The inner parts 126 of the impeller blades 127 agitate..the entering fuel and separate bubbles of gas which pass up through the fuel in the tank and escape by the vent 21<1>. The fuel is delivered by pipes 28, 29.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB222743A GB562925A (en) | 1943-02-10 | 1943-02-10 | Improvements in or relating to fuel-pumping systems |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB222743A GB562925A (en) | 1943-02-10 | 1943-02-10 | Improvements in or relating to fuel-pumping systems |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB562925A true GB562925A (en) | 1944-07-21 |
Family
ID=9735823
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB222743A Expired GB562925A (en) | 1943-02-10 | 1943-02-10 | Improvements in or relating to fuel-pumping systems |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB562925A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2972308A (en) * | 1957-03-12 | 1961-02-21 | Thompson Ramo Wooldridge Inc | Sealed stator submerged electric fuel pump |
-
1943
- 1943-02-10 GB GB222743A patent/GB562925A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2972308A (en) * | 1957-03-12 | 1961-02-21 | Thompson Ramo Wooldridge Inc | Sealed stator submerged electric fuel pump |
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