GB517331A - Improvements connected with the catapulting of aircraft - Google Patents
Improvements connected with the catapulting of aircraftInfo
- Publication number
- GB517331A GB517331A GB2185338A GB2185338A GB517331A GB 517331 A GB517331 A GB 517331A GB 2185338 A GB2185338 A GB 2185338A GB 2185338 A GB2185338 A GB 2185338A GB 517331 A GB517331 A GB 517331A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- carriage
- drogue
- car
- cable
- 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
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/04—Launching or towing gear
- B64F1/06—Launching or towing gear using catapults
Abstract
517,331. Launching aircraft; drag anchors. SANDOR, N. July 22, 1938, Nos. 21853/38 and 6205/39. [Classes 4 and 114] A catapulting system for aircraft comprises a moving body which imparts an initial speed or acceleration to the aircraft, the kinetic energy of the moving body in conjunction with a resistance being then utilized to impart an additional substantially constant acceleration to the aircraft until take-off speed is reached. In the form shown in Fig. 1, an aircraft 15 is mounted on a carriage 13 adapted to run along the top of a car 2 which runs on rails 1. The car 2 is driven by motors, which may be carried on an auxiliary vehicle, or by the propellers of the aircraft itself. Upon the car 2 attaining a suitable speed, a body 19 is caused to apply brakes to rails and, being thus retarded, accelerate the carriage 13 relative to the car 2 by means of cables 16 and 21 attached to the body 19. The car 2 may be composed of a plurality of bogie trucks and be provided with an upper runway on which the carriage 13 is mounted, this runway being engaged by horizontally and vertically disposed rollers on the carriage. Hydraulic buffers 49 and 50 are provided to arrest the carriage 13 and the body 19. A separate track may be provided at each side of the rails 1 for the aircraft wheels to run on. For reloading purposes a cradle supporting the aircraft to be launched is provided with a base member adapted to engage in a groove in the carriage 13 whereby an empty cradle may be displaced from the carriage and replaced by a fresh cradle supporting an aircraft. In another form, Fig. 9, an aircraft 15 is launched from the deck of a moving aircraft carrier. The aircraft is drawn along the deck by a cable 16a passing round a drum 17a which is driven by a smaller drum 13a over which passes a cable 21a connected with the drogue 19a, which is dropped into the sea at the desired moment. In another form, Fig. 10 (not shown) a seaplane is towed by a ship through a small boat which carries drums 17a and 18a and from which the drogue is thrown overboard at the desired moment. The drogue described is fitted with a resistance-presenting surface 67, Fig. 11, the position of which is controlled by a servomotor 63 in dependence on the tension applied to the cable 21a towing the drogue. As a spring 57 is compressed by the tension in 'the cable a rack and pinion 58, 59 actuates a valve 61 to control the flow past the servomotor. The cable may be attached to another vessel or to a point ashore instead of to the drogue.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2185338A GB517331A (en) | 1938-07-22 | 1938-07-22 | Improvements connected with the catapulting of aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2185338A GB517331A (en) | 1938-07-22 | 1938-07-22 | Improvements connected with the catapulting of aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB517331A true GB517331A (en) | 1940-01-26 |
Family
ID=10169912
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2185338A Expired GB517331A (en) | 1938-07-22 | 1938-07-22 | Improvements connected with the catapulting of aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB517331A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105501458A (en) * | 2014-09-24 | 2016-04-20 | 田忠林 | Track block chain shipboard aircraft catapult |
CN108408072A (en) * | 2018-05-08 | 2018-08-17 | 西北工业大学 | A kind of carrier-borne recovery method of fixed-wing UAV and system |
CN109878754A (en) * | 2019-04-18 | 2019-06-14 | 太原科技大学 | The airport power-assisted lifting gear of superconduction external rotor electric machine dragging |
CN112829961A (en) * | 2021-02-19 | 2021-05-25 | 王运宏 | Aircraft carrier catapult |
CN113018881A (en) * | 2021-04-25 | 2021-06-25 | 航天创客(北京)科技有限公司 | Aerospace science popularization model self-adaptive ejection device |
CN113148218A (en) * | 2021-03-31 | 2021-07-23 | 潍坊新力蒙水产技术有限公司 | Descending type integrated external power track electronic floating-shooting aviation device |
CN113492687A (en) * | 2020-04-07 | 2021-10-12 | 中国航天科工飞航技术研究院(中国航天海鹰机电技术研究院) | Magnetic suspension sledge ejection device |
CN114368489A (en) * | 2021-07-26 | 2022-04-19 | 李敏 | Brand-new aircraft carrier mechanical catapult structure |
-
1938
- 1938-07-22 GB GB2185338A patent/GB517331A/en not_active Expired
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105501458A (en) * | 2014-09-24 | 2016-04-20 | 田忠林 | Track block chain shipboard aircraft catapult |
CN105501458B (en) * | 2014-09-24 | 2018-05-08 | 田忠林 | Rail sliding car chain carrier-based aircraft ejector |
CN108408072A (en) * | 2018-05-08 | 2018-08-17 | 西北工业大学 | A kind of carrier-borne recovery method of fixed-wing UAV and system |
CN108408072B (en) * | 2018-05-08 | 2021-08-06 | 西北工业大学 | Shipborne recovery method and system for fixed-wing unmanned aircraft |
CN109878754A (en) * | 2019-04-18 | 2019-06-14 | 太原科技大学 | The airport power-assisted lifting gear of superconduction external rotor electric machine dragging |
CN113492687A (en) * | 2020-04-07 | 2021-10-12 | 中国航天科工飞航技术研究院(中国航天海鹰机电技术研究院) | Magnetic suspension sledge ejection device |
CN112829961A (en) * | 2021-02-19 | 2021-05-25 | 王运宏 | Aircraft carrier catapult |
CN113148218A (en) * | 2021-03-31 | 2021-07-23 | 潍坊新力蒙水产技术有限公司 | Descending type integrated external power track electronic floating-shooting aviation device |
CN113018881A (en) * | 2021-04-25 | 2021-06-25 | 航天创客(北京)科技有限公司 | Aerospace science popularization model self-adaptive ejection device |
CN114368489A (en) * | 2021-07-26 | 2022-04-19 | 李敏 | Brand-new aircraft carrier mechanical catapult structure |
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