GB512105A - Means for obtaining relative movement of aircraft parts - Google Patents

Means for obtaining relative movement of aircraft parts

Info

Publication number
GB512105A
GB512105A GB35138/38A GB3513838A GB512105A GB 512105 A GB512105 A GB 512105A GB 35138/38 A GB35138/38 A GB 35138/38A GB 3513838 A GB3513838 A GB 3513838A GB 512105 A GB512105 A GB 512105A
Authority
GB
United Kingdom
Prior art keywords
rod
driven
motor shaft
screw thread
motor
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
GB35138/38A
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.)
Elektron-Co Mbh
Elektron Co mbH
Original Assignee
Elektron-Co Mbh
Elektron Co mbH
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 Elektron-Co Mbh, Elektron Co mbH filed Critical Elektron-Co Mbh
Publication of GB512105A publication Critical patent/GB512105A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/02Undercarriages
    • B64C25/08Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/18Operating mechanisms
    • B64C25/24Operating mechanisms electric

Abstract

512,105. Screw and nut actuators. ELEKTRON CO. Dec. 2, 1938, No. 35138. Convention date, Jan. 12. [Class 78 (iii)] [Also in Group XXXIII] Relative movement of aircraft parts, particularly retractable undercarriages, is obtained by means of a strut, variation of the length of which is obtained by longitudinal movement of one part of the strut produced by an electric motor which forms part of the strut. The casing of the motor 1 is connected by a part 5 to the aircraft body and the motor shaft 2 is adapted to extend by a screw thread 3, a rod 4 connected to a retractable undercarriage. Rotation of the rod 4 is prevented by a part 8. In a modification the motor shaft drives the screw thread by-means of a differential gear, the screw thread and the rod 4 being arranged in the hollow motor shaft. In further modifications different geared arrangements are shown, in one of which the rod. 4 is toothed and driven by a wheel having inclined teeth, which is driven by gearing from the motor shaft. In a further modification the toothed rod is driven by a pinion on a shaft driven by bevel gear from the motor shaft. In two further modifications the rod.4 is at the side of the motor and is driven by gearing and screw thread or a wheel with inclined teeth engaging teeth on the rod.
GB35138/38A 1938-01-12 1938-12-02 Means for obtaining relative movement of aircraft parts Expired GB512105A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE512105X 1938-01-12

Publications (1)

Publication Number Publication Date
GB512105A true GB512105A (en) 1939-08-29

Family

ID=6548028

Family Applications (1)

Application Number Title Priority Date Filing Date
GB35138/38A Expired GB512105A (en) 1938-01-12 1938-12-02 Means for obtaining relative movement of aircraft parts

Country Status (1)

Country Link
GB (1) GB512105A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2486242A (en) * 1944-01-17 1949-10-25 Electrol Inc Actuating mechanism for retractable landing gear, doors, flaps, and the like of airplanes

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2486242A (en) * 1944-01-17 1949-10-25 Electrol Inc Actuating mechanism for retractable landing gear, doors, flaps, and the like of airplanes

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