GB468460A - Improved apparatus for the replenishment of containers for hydro-carbon liquids - Google Patents
Improved apparatus for the replenishment of containers for hydro-carbon liquidsInfo
- Publication number
- GB468460A GB468460A GB1494/36A GB149436A GB468460A GB 468460 A GB468460 A GB 468460A GB 1494/36 A GB1494/36 A GB 1494/36A GB 149436 A GB149436 A GB 149436A GB 468460 A GB468460 A GB 468460A
- Authority
- GB
- United Kingdom
- Prior art keywords
- tank
- pump
- valve
- pipe
- gases
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B67—OPENING, CLOSING OR CLEANING BOTTLES, JARS OR SIMILAR CONTAINERS; LIQUID HANDLING
- B67D—DISPENSING, DELIVERING OR TRANSFERRING LIQUIDS, NOT OTHERWISE PROVIDED FOR
- B67D7/00—Apparatus or devices for transferring liquids from bulk storage containers or reservoirs into vehicles or into portable containers, e.g. for retail sale purposes
- B67D7/04—Apparatus or devices for transferring liquids from bulk storage containers or reservoirs into vehicles or into portable containers, e.g. for retail sale purposes for transferring fuels, lubricants or mixed fuels and lubricants
- B67D7/0476—Vapour recovery systems
- B67D7/0478—Vapour recovery systems constructional features or components
- B67D7/048—Vapour flow control means, e.g. valves, pumps
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
468,460. Dispensing liquids. TECALEMIT, Ltd. Jan. 16, 1936, No. 1494. Convention date, Jan. 19, 1935. [Class 102 (i)] [Also in Group XVII] An aircraft or other petrol tank 2, Fig. 5, is filled from a supply tank 1 in a closed circuit, thus avoiding spilling of petrol and escape of inflammable gases. The apparatus may comprise only a pump 3 in the supply pipe 5 and a pipe 6, 9 for the return of gases and excess liquid to the tank 1, the pipe 6, 9 being provided with a float valve 10, which closes when liquid reaches the chamber 7, thus preventing further operation of the pump 3. The pipes 5, 6 may then be emptied by reversing the pump 3. A byepass 12 with check valve 14 may be provided, in order to avoid sudden stoppage of the pump 3 when the valve 10 closes. An air separator and filter 17, meter 18, and air byepass 19 as described in Specification 417,882 may be provided between the tank 1 and the pump 3. In order to avoid excess pressure in the tank 2, a pump 15 may be provided for drawing off gases. The pumps 3, 15 are either reversible or are provided with three-way valves for reversing the direction of flow. Excess pressure in the tank 2 may alternatively be avoided by means of a valve 27, Fig. 6, which is connected to a diaphragm 28, exposed on one side to the atmosphere and on the other side to the pressure in the tank 2. The return pipe 6 may be provided with a float valve, as in the arrangement previously described, or with a restricted orifice 31, which causes a rise in pressure when liquid commences to pass and consequent closing of the valve 27.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR468460X | 1935-01-19 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB468460A true GB468460A (en) | 1937-07-06 |
Family
ID=8902350
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1494/36A Expired GB468460A (en) | 1935-01-19 | 1936-01-16 | Improved apparatus for the replenishment of containers for hydro-carbon liquids |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB468460A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2009098012A2 (en) * | 2008-02-07 | 2009-08-13 | Airbus Operations Gmbh | Aircraft tank system refuelling unit and method for refuelling an aircraft |
| CN112423877A (en) * | 2018-07-12 | 2021-02-26 | 倪泰克解决方案有限公司 | Liquid treatment assembly |
-
1936
- 1936-01-16 GB GB1494/36A patent/GB468460A/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2009098012A2 (en) * | 2008-02-07 | 2009-08-13 | Airbus Operations Gmbh | Aircraft tank system refuelling unit and method for refuelling an aircraft |
| WO2009098012A3 (en) * | 2008-02-07 | 2009-10-29 | Airbus Operations Gmbh | Aircraft tank system refuelling unit and method for refuelling an aircraft |
| US8434721B2 (en) | 2008-02-07 | 2013-05-07 | Airbus Operations Gmbh | Aircraft tank system and method for refueling an aircraft using an eration/deaeration device with a shut-off valve |
| CN112423877A (en) * | 2018-07-12 | 2021-02-26 | 倪泰克解决方案有限公司 | Liquid treatment assembly |
| CN112423877B (en) * | 2018-07-12 | 2023-10-27 | 倪泰克解决方案有限公司 | Liquid handling assembly |
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