GB350673A - Improvements relating to aircraft lights - Google Patents
Improvements relating to aircraft lightsInfo
- Publication number
- GB350673A GB350673A GB1415330A GB1415330A GB350673A GB 350673 A GB350673 A GB 350673A GB 1415330 A GB1415330 A GB 1415330A GB 1415330 A GB1415330 A GB 1415330A GB 350673 A GB350673 A GB 350673A
- Authority
- GB
- United Kingdom
- Prior art keywords
- reflector
- movement
- pivot
- axial movement
- lever
- 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
- 230000000881 depressing 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
- 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
350,673. Aircraft landing &c. lights. CHANCE BROS. & CO., Ltd. and GOODMAN, H. E. E., Lighthouse Works, Smethwick, Staffordshire. May 8, 1930, No. 14153. [Class 75 (ii).] Adjusting reflectors from a distance.-Relates to aircraft landing or like lights of the kind in which a gimbal-mounted reflector is capable also of axial movement as a whole for controlling both the direction of the beam and also its divergence and consists mainly of a double-jointed pilot's lever by which the movements of the reflector are effected. The reflector G is carried by a gimbal ring d, d<1> and is mounted for axial movement therein by means of spring-controlled sliding stems f. These movements are effected through four cables h attached to the reflector at symmetrically disposed points i and at their other ends carried over grooved segments p on the operating lever, Figs. 3 and 4. This latter comprises two parts j, k connected by a ball joint l, m and mounted at its lower end on a pivot which is normally locked against rotation by a wedge u causing sliding parts o of the pivot to engage serrated clutch faces v. The wedge is released, against the action of its locking spring q, by depressing the central two-part rod r, s and the lever can then be moved about the bottom pivot to pull all four cables and thus cause axial movement of the reflector. When the bottom pivot is allowed to remain locked however the only movement possible is a universal movement about the ball joint l, m, thus effecting a corresponding swivelling movement of the reflector.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1415330A GB350673A (en) | 1930-05-08 | 1930-05-08 | Improvements relating to aircraft lights |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1415330A GB350673A (en) | 1930-05-08 | 1930-05-08 | Improvements relating to aircraft lights |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB350673A true GB350673A (en) | 1931-06-18 |
Family
ID=10035969
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1415330A Expired GB350673A (en) | 1930-05-08 | 1930-05-08 | Improvements relating to aircraft lights |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB350673A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2843728A (en) * | 1954-10-07 | 1958-07-15 | Grant V W Roth | Aircraft lighting and signaling structure |
| GB2367118A (en) * | 1999-06-23 | 2002-03-27 | Bell Helicopter Textron Inc | Adjustable Position Light for Aircraft |
-
1930
- 1930-05-08 GB GB1415330A patent/GB350673A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2843728A (en) * | 1954-10-07 | 1958-07-15 | Grant V W Roth | Aircraft lighting and signaling structure |
| GB2367118A (en) * | 1999-06-23 | 2002-03-27 | Bell Helicopter Textron Inc | Adjustable Position Light for Aircraft |
| GB2367118B (en) * | 1999-06-23 | 2004-12-29 | Bell Helicopter Textron Inc | Position light for aircraft |
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