GB351172A - A method and apparatus for tanking aircraft in the air - Google Patents
A method and apparatus for tanking aircraft in the airInfo
- Publication number
- GB351172A GB351172A GB13948/30A GB1394830A GB351172A GB 351172 A GB351172 A GB 351172A GB 13948/30 A GB13948/30 A GB 13948/30A GB 1394830 A GB1394830 A GB 1394830A GB 351172 A GB351172 A GB 351172A
- Authority
- GB
- United Kingdom
- Prior art keywords
- hose
- aircraft
- engagement
- receiving
- spring
- 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
- 230000004048 modification Effects 0.000 abstract 2
- 238000012986 modification Methods 0.000 abstract 2
- 239000000446 fuel Substances 0.000 abstract 1
Classifications
-
- 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
- B64D39/00—Refuelling during flight
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Loading And Unloading Of Fuel Tanks Or Ships (AREA)
Abstract
351,172. Refuelling aircraft. LINDE. QUIST, S., 8, Landhausstrasse, Wilmersdorf, Berlin. May 6, 1930, No. 13948. Conven. tion date, May 30,1929. Addition to 346,181. [Class 4.] Apparatus for receiving a hose for supplying fuel &c. to aircraft in flight as described in the parent Specification is mounted on the wing of the aircraft and is provided with a loop 4 which can be turned by the pilot forwardly over the receiving fork of the apparatus to facilitate the engagement of the hose therewith. The slot in the apparatus is made forwardly tapering and resilient to grip the hose when in operative position and various forms of valve for the hose end are described. In one valve, Fig. 3, a casing 9 having a cylindrical portion 10 slides over another cylinder 12, connected to the hose, to open ports 13 when the parts are drawn together by engagement of the discs 11, 14 with the receiving apparatus. A spring 18 maintains the parts in their normal position. In a modification, Fig. 4, a casing 20 supports an inner cylinder 22 having ports 21 normally covered by a slide 23. The slide 23 is moved against a spring 26 by a rod 24 connected to a disc 25 engaged by the receiving apparatus. In a further modification, Fig. 5, a disc valve 32 carried by a cylinder 29 is moved against a spring 31 by the engagement of the receiving apparatus with a disc 30.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE351172X | 1929-05-30 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB351172A true GB351172A (en) | 1931-06-25 |
Family
ID=6266880
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB13948/30A Expired GB351172A (en) | 1929-05-30 | 1930-05-06 | A method and apparatus for tanking aircraft in the air |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB351172A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105539864A (en) * | 2015-12-11 | 2016-05-04 | 中国航空工业集团公司西安飞机设计研究所 | Air fueling inflatable emergency unlocking device |
-
1930
- 1930-05-06 GB GB13948/30A patent/GB351172A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105539864A (en) * | 2015-12-11 | 2016-05-04 | 中国航空工业集团公司西安飞机设计研究所 | Air fueling inflatable emergency unlocking device |
| CN105539864B (en) * | 2015-12-11 | 2018-11-13 | 中国航空工业集团公司西安飞机设计研究所 | A kind of emergent disengaging gear of air refuelling inflatable |
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