GB499507A - Apparatus for controlling the operation of lights on aircraft and other vehicles - Google Patents
Apparatus for controlling the operation of lights on aircraft and other vehiclesInfo
- Publication number
- GB499507A GB499507A GB2230437A GB2230437A GB499507A GB 499507 A GB499507 A GB 499507A GB 2230437 A GB2230437 A GB 2230437A GB 2230437 A GB2230437 A GB 2230437A GB 499507 A GB499507 A GB 499507A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pistons
- cylinders
- lamps
- openings
- pair
- 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
- 239000007788 liquid Substances 0.000 abstract 2
- 238000005461 lubrication Methods 0.000 abstract 1
- 230000004048 modification Effects 0.000 abstract 1
- 238000012986 modification Methods 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
- B64D47/00—Equipment not otherwise provided for
- B64D47/02—Arrangements or adaptations of signal or lighting devices
- B64D47/04—Arrangements or adaptations of signal or lighting devices the lighting devices being primarily intended to illuminate the way ahead
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Lighting Device Outwards From Vehicle And Optical Signal (AREA)
Abstract
499,507. Directing vehicle lamps. DUNLOP RUBBER CO., Ltd., BEHARRELL, G. E., WRIGHT, J., and TREVASKIS, H. Aug. 13, 1937, No. 22304. [Class 75 (iii)] In hydraulic apparatus for simultaneously tilting a pair of aircraft or other vehicle lamps through equal angles and comprising a casing 1 containing a pair of pistons 9, operated by rotating a screwed spindle 8 to force liquid from the cylinders 4 through openings 25 into pipe lines 27 and a pair of cylinders 30 containing spring-pressed pistons 33 connected by links 37 to the lamps, a liquid reservoir 21, fixed to, or formed on, the casing 1, communicates through a passage 18, openings 17 and radial passages 24 with the cylinders 4 and spring-pressed valves 11 are provided in the pistons 9 for closing the openings 17 during the initial forward movement of the pistons. The valves are retracted by shoulders 14 when the pistons are returned to the initial positions. As shown, the reservoir 21 is secured by a plug 20 with interconnected passages 19, 23. The spindle 8, which may be rotated directly, or through gearing, by a hand wheel &c., is held against axial movement by a collar 8a and a thrust peg 8b and operates a sliding sleeve 6 having arms 7a engaging grooves in projections 9a on the pistons 9. An air trap is provided in each pipe 27. The pistons 33 have flanged heads 34 engaging washers 35 slidable in the cylinders 30, which are mounted on ball-headed pins 38 on the vehicle. Circumferential grooves 10 are provided in the pistons 9, 33 for lubrication purposes. More than two lamps may be operated by providing additional pistons and cylinders. The Provisional Specification describes also a modification in which the pistons in the cylinders 4 are mounted in flexible diaphragms and carry spindles for operating leaf springs to close the inlets to the cylinders, and the lamp operating devices comprise shafts controlled by expansible bags.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2230437A GB499507A (en) | 1937-08-13 | 1937-08-13 | Apparatus for controlling the operation of lights on aircraft and other vehicles |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2230437A GB499507A (en) | 1937-08-13 | 1937-08-13 | Apparatus for controlling the operation of lights on aircraft and other vehicles |
Publications (1)
Publication Number | Publication Date |
---|---|
GB499507A true GB499507A (en) | 1939-01-25 |
Family
ID=10177210
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2230437A Expired GB499507A (en) | 1937-08-13 | 1937-08-13 | Apparatus for controlling the operation of lights on aircraft and other vehicles |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB499507A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2324340A1 (en) * | 1973-05-14 | 1974-11-28 | Westfaelische Metall Industrie | DEVICE FOR ADJUSTING THE INCLINATION OF VEHICLE HEADLIGHTS |
-
1937
- 1937-08-13 GB GB2230437A patent/GB499507A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2324340A1 (en) * | 1973-05-14 | 1974-11-28 | Westfaelische Metall Industrie | DEVICE FOR ADJUSTING THE INCLINATION OF VEHICLE HEADLIGHTS |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2424233A (en) | Landing gear | |
GB730526A (en) | Power steering device | |
US2317636A (en) | Dual tire inflater | |
US2252772A (en) | Hydraulic steering stabilizer | |
SE7600348L (en) | HYDRAULIC MOUNTAIN DRILL | |
US2659615A (en) | Dual hydraulic swivel joint | |
GB499507A (en) | Apparatus for controlling the operation of lights on aircraft and other vehicles | |
US3521527A (en) | Rotary vane suspension units for endless track vehicles and the like | |
US2448064A (en) | Retractable landing gear for aircraft | |
US2350683A (en) | Fluid drive | |
GB725920A (en) | Improvements in or relating to power steering for motor vehicles | |
GB582545A (en) | A self-priming liquid spring unit | |
US2046918A (en) | Lifting jack | |
US2411119A (en) | Steering mechanism | |
US2233468A (en) | Variable pitch propeller | |
GB704058A (en) | Improved power steering mechanism for road vehicles | |
US1934719A (en) | Power actuator | |
US2631795A (en) | Hydraulically controlled steering mechanism for aircraft | |
US2455133A (en) | Parking device | |
US3444787A (en) | Rotary vane suspension units for endless track vehicles and the like | |
US3528114A (en) | Rotary vane suspension units for endless track vehicles and the like | |
US2037055A (en) | Braking mechanism | |
US2545529A (en) | Selector valve | |
GB520994A (en) | Improvements relating to retractable undercarriages for aircraft | |
US2426938A (en) | Hydraulic steering gear |