GB552749A - Improvements relating to towing devices for aircraft with particular reference to tow cable tension control - Google Patents
Improvements relating to towing devices for aircraft with particular reference to tow cable tension controlInfo
- Publication number
- GB552749A GB552749A GB1351441A GB1351441A GB552749A GB 552749 A GB552749 A GB 552749A GB 1351441 A GB1351441 A GB 1351441A GB 1351441 A GB1351441 A GB 1351441A GB 552749 A GB552749 A GB 552749A
- Authority
- GB
- United Kingdom
- Prior art keywords
- cable
- tension
- towing
- aircraft
- fitting
- 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
- 230000005540 biological transmission Effects 0.000 abstract 1
- 230000002441 reversible effect Effects 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
- B64D3/00—Aircraft adaptations to facilitate towing or being towed
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Throttle Valves Provided In The Intake System Or In The Exhaust System (AREA)
- Flexible Shafts (AREA)
Abstract
552,749. Towing. KRONFELD, R. Oct. 21, 1941, No. 13514. [Class 78 (ii)] [Also in Groups XXXIII and XXXV] A towing device for aircraft, drogues or targets includes means responsive to variations in the tension of the tow rope for automatically restoring the tension to its predetermined value. Fig. 1 shows the tail end of a towing aircraft carrying a fitting 3 slidable along a bar 11 against the tension of a spring 10. The towing cable 2 is connected to the fitting 3 by a quick-release device 4 and the fitting 3 is connected by a cable 5 to the throttle control so that an increase of tension in the cable 2 causes a reduction of the throttle opening. The cable 5 is connected to an intermediate member-such as a toothed wheel to which the throttle lever can be coupled by a spring pawl. The elevator or screw-pitch control may be actuated by the variations in cable tension. Alternatively the cable may be passed over a pulley and around a winch which is driven by a reversible electro-motor or hydraulic motor to wind up or pay out the cable as the pulley is displaced against centring springs by the variations in the tension of the cable. Fig. 4 shows the two sections 2a, 2b of a towing cable of a glider connected through springs 29, 30 to quick release points 31, 32 on the wings, and by extensions of these cables to air brakes 27, 27a, so that relaxation of tension in either cable results in the air brake being raised. Actuation of the quick release devices also moves catches for retaining the air brakes in their inoperative position. Where electric transmission is used the tension spring assembly may actuate the controls of both the towed and towing aircraft.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1351441A GB552749A (en) | 1941-10-21 | 1941-10-21 | Improvements relating to towing devices for aircraft with particular reference to tow cable tension control |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1351441A GB552749A (en) | 1941-10-21 | 1941-10-21 | Improvements relating to towing devices for aircraft with particular reference to tow cable tension control |
Publications (1)
Publication Number | Publication Date |
---|---|
GB552749A true GB552749A (en) | 1943-04-22 |
Family
ID=10024351
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1351441A Expired GB552749A (en) | 1941-10-21 | 1941-10-21 | Improvements relating to towing devices for aircraft with particular reference to tow cable tension control |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB552749A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2432548A (en) * | 1945-05-08 | 1947-12-16 | Moulton B Taylor | Automatic control |
US2436988A (en) * | 1943-04-20 | 1948-03-02 | Bell Charles Stanley | Towed aircraft and means for towing the same |
US2470294A (en) * | 1945-05-10 | 1949-05-17 | Wurlitzer Co | Aircraft release device |
US2612327A (en) * | 1947-03-06 | 1952-09-30 | United Aircraft Corp | Towed glider with automatic tow cable release |
US2898058A (en) * | 1954-01-20 | 1959-08-04 | Del Mar Engineering Lab Inc | Tow target |
GB2211159A (en) * | 1987-11-03 | 1989-06-28 | Takahiro Hashi | Tow rope with forking portions for towing a handlebar-type vehicle |
CN112373712A (en) * | 2020-11-17 | 2021-02-19 | 中航通飞华南飞机工业有限公司 | Water traction landing method and system for large-scale seaplane |
-
1941
- 1941-10-21 GB GB1351441A patent/GB552749A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2436988A (en) * | 1943-04-20 | 1948-03-02 | Bell Charles Stanley | Towed aircraft and means for towing the same |
US2432548A (en) * | 1945-05-08 | 1947-12-16 | Moulton B Taylor | Automatic control |
US2470294A (en) * | 1945-05-10 | 1949-05-17 | Wurlitzer Co | Aircraft release device |
US2612327A (en) * | 1947-03-06 | 1952-09-30 | United Aircraft Corp | Towed glider with automatic tow cable release |
US2898058A (en) * | 1954-01-20 | 1959-08-04 | Del Mar Engineering Lab Inc | Tow target |
GB2211159A (en) * | 1987-11-03 | 1989-06-28 | Takahiro Hashi | Tow rope with forking portions for towing a handlebar-type vehicle |
CN112373712A (en) * | 2020-11-17 | 2021-02-19 | 中航通飞华南飞机工业有限公司 | Water traction landing method and system for large-scale seaplane |
CN112373712B (en) * | 2020-11-17 | 2023-10-20 | 中航通飞华南飞机工业有限公司 | Water traction landing method and system for large-scale water plane |
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