GB322861A - Improvements in or relating to apparatus for launching aircraft - Google Patents
Improvements in or relating to apparatus for launching aircraftInfo
- Publication number
- GB322861A GB322861A GB3277228A GB3277228A GB322861A GB 322861 A GB322861 A GB 322861A GB 3277228 A GB3277228 A GB 3277228A GB 3277228 A GB3277228 A GB 3277228A GB 322861 A GB322861 A GB 322861A
- Authority
- GB
- United Kingdom
- Prior art keywords
- trolly
- sheaves
- frame
- cable
- rails
- 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
- 239000004450 Cordite Substances 0.000 abstract 1
- 239000012530 fluid Substances 0.000 abstract 1
- 230000000979 retarding effect Effects 0.000 abstract 1
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—Ground or aircraft-carrier-deck installations for launching aircraft
- B64F1/06—Ground or aircraft-carrier-deck installations for launching aircraft using catapults
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Orthopedics, Nursing, And Contraception (AREA)
Abstract
322,861. Forbes, W. A. D. Nov, 9, 1928. Launching ways.-A launching device for aircraft comprises a trolly propelled through rope and sheave gear from a prime mover along a track which can be increased in length by one or more extending portions, the increased travel of the trolly being obtained without having to accaelerate and retard any masses other than the aircraft, trolly and interconnecting rope and sheave gear. The apparatus comprises a frame which may be fixed, or mounted on a central pivot and rails 6 to which it can be clamped in any position to suit the direction of the wind. Two sliding extensions 3 are provided to lengthen the run of a trolly 11. These may be moved together or separately by electromotors, or by a hand winch actuating cable drums 20, or by temporarily securing the trolly to each extension in turn and utilizing the prime mover. They are secured in their extended positions by bolts 22, Fig. VII. A cylinder 8 on the main frame has a piston connected to a crosshead 24 carrying a number of sheaves. A cable 12 anchored to the frame at 15a is passed around two of the cross head sheaves 16a, 16b, and around two sheaves 17a, 17<a1> on the frame as shown in Fig. V ; the cable then passes over two sheaves 18a, 19<a> on the forward extension 3 and is connected to a balance pulley 14 or lever on the trolly which is connected to a duplicate cable passed around a similar set of sheaves. A similar pair of cables 13 passed around pulleys 19<b>, 18<b> on the rear extension and around pulleys 17b, 17<b1>, and 16b, 16<b1> on the frame and crosshead respectively act as retarding cables at the end of the run. The piston is moved by hydraulic or pneumatic means or by exploding a propellent such as cordite and is retarded at the end of its stroke by expelling fluid through a restricted passage into a reservoir 10. The pulleys 18<a>, 19<a>, 18<b>, 19<b> enable the trolly to be moved irrespective of the position of the extensions 3, and vice versa without affecting the lengths of the cables 12, 13. The trolly has two sets of wheels 23, Fig. VII, one set running in rails 2 on the main frame, and the other in rails 4 on the extensions 3.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3277228A GB322861A (en) | 1928-11-09 | 1928-11-09 | Improvements in or relating to apparatus for launching aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3277228A GB322861A (en) | 1928-11-09 | 1928-11-09 | Improvements in or relating to apparatus for launching aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB322861A true GB322861A (en) | 1929-12-19 |
Family
ID=10343763
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3277228A Expired GB322861A (en) | 1928-11-09 | 1928-11-09 | Improvements in or relating to apparatus for launching aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB322861A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE739372C (en) * | 1931-10-11 | 1943-09-23 | Ernst Heinkel Flugzeugwerke G | Rotatable aircraft launch track |
CN102530261A (en) * | 2011-12-09 | 2012-07-04 | 朱惠芬 | Launching return linkage type high-power aircraft carrier catapult |
CN113815883A (en) * | 2021-08-20 | 2021-12-21 | 中国船舶重工集团公司第七0四研究所 | High-energy-level emission and multi-level braking test system and method |
-
1928
- 1928-11-09 GB GB3277228A patent/GB322861A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE739372C (en) * | 1931-10-11 | 1943-09-23 | Ernst Heinkel Flugzeugwerke G | Rotatable aircraft launch track |
CN102530261A (en) * | 2011-12-09 | 2012-07-04 | 朱惠芬 | Launching return linkage type high-power aircraft carrier catapult |
CN102530261B (en) * | 2011-12-09 | 2014-03-19 | 刘真 | Launching return linkage type high-power aircraft carrier catapult |
CN113815883A (en) * | 2021-08-20 | 2021-12-21 | 中国船舶重工集团公司第七0四研究所 | High-energy-level emission and multi-level braking test system and method |
CN113815883B (en) * | 2021-08-20 | 2023-08-18 | 中国船舶重工集团公司第七0四研究所 | High-energy-level emission and multi-stage braking test system and method |
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