GB932070A - Improvements in and relating to aircraft landing lamps - Google Patents

Improvements in and relating to aircraft landing lamps

Info

Publication number
GB932070A
GB932070A GB1112061A GB1112061A GB932070A GB 932070 A GB932070 A GB 932070A GB 1112061 A GB1112061 A GB 1112061A GB 1112061 A GB1112061 A GB 1112061A GB 932070 A GB932070 A GB 932070A
Authority
GB
United Kingdom
Prior art keywords
lamp
rod
plunger
sleeve
fuselage
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
Application number
GB1112061A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
MALDON CAVENDISH HARLEY
Original Assignee
MALDON CAVENDISH HARLEY
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by MALDON CAVENDISH HARLEY filed Critical MALDON CAVENDISH HARLEY
Priority to GB1112061A priority Critical patent/GB932070A/en
Publication of GB932070A publication Critical patent/GB932070A/en
Expired legal-status Critical Current

Links

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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60Q—ARRANGEMENT OF SIGNALLING OR LIGHTING DEVICES, THE MOUNTING OR SUPPORTING THEREOF OR CIRCUITS THEREFOR, FOR VEHICLES IN GENERAL
    • B60Q1/00—Arrangement of optical signalling or lighting devices, the mounting or supporting thereof or circuits therefor
    • B60Q1/02—Arrangement of optical signalling or lighting devices, the mounting or supporting thereof or circuits therefor the devices being primarily intended to illuminate the way ahead or to illuminate other areas of way or environments
    • B60Q1/04—Arrangement of optical signalling or lighting devices, the mounting or supporting thereof or circuits therefor the devices being primarily intended to illuminate the way ahead or to illuminate other areas of way or environments the devices being headlights
    • B60Q1/05—Arrangement of optical signalling or lighting devices, the mounting or supporting thereof or circuits therefor the devices being primarily intended to illuminate the way ahead or to illuminate other areas of way or environments the devices being headlights retractable

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Lighting Device Outwards From Vehicle And Optical Signal (AREA)

Abstract

932,070. Aircraft landing lamps. M. C. HARLEY. March 27, 1962 [March 27, 1961], No. 11120/61. Class 75 (3). A lamp of the type having a support hinged to a mounting in a space in the wing or fuselage of an aircraft and in which mechanism is provided for moving the lamp into and out of operative position and embodies limit switches determining the operative and inoperative positions of the lamp, means are provided for adjusting the position of the lamp at which the actuating mechanism is arrested during outward movement of the lamp, the means being disposed within a lamp housing support so as to be freely accessible from below. In the form shown, the lamp and reflector are carried in a casing c pivoted at e to a housing a in the wing or fuselage and moved by an arm f pivoted to the rod g of an electric actuator (not shown). The arm f carries a pin h engaging a plate i on a plunger consisting of a screw-threaded sleeve j and a threaded rod k carrying a plate t at the opposite end, which actuates the plunger r of a micro-switch s after the lamp has moved a distance determined by the extent to which the rod k is screwed into the sleeve j, this adjustment being indicated by a pointer o on the sleeve j moving over a fixed scale p. A spring m on the rod k keeps the head i of the plunger in contact with the pin h.
GB1112061A 1961-03-27 1961-03-27 Improvements in and relating to aircraft landing lamps Expired GB932070A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1112061A GB932070A (en) 1961-03-27 1961-03-27 Improvements in and relating to aircraft landing lamps

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1112061A GB932070A (en) 1961-03-27 1961-03-27 Improvements in and relating to aircraft landing lamps

Publications (1)

Publication Number Publication Date
GB932070A true GB932070A (en) 1963-07-24

Family

ID=9980406

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1112061A Expired GB932070A (en) 1961-03-27 1961-03-27 Improvements in and relating to aircraft landing lamps

Country Status (1)

Country Link
GB (1) GB932070A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2499916A1 (en) * 1981-02-17 1982-08-20 Manzoni Bouchot Sa Headlamp aim compensator for motor vehicles - uses electric motor mounted behind grille between headlamps actuate cable which tilts headlamp against spring compensating for load

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2499916A1 (en) * 1981-02-17 1982-08-20 Manzoni Bouchot Sa Headlamp aim compensator for motor vehicles - uses electric motor mounted behind grille between headlamps actuate cable which tilts headlamp against spring compensating for load

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