GB448827A - Improvements in or relating to control surfaces for aircraft - Google Patents

Improvements in or relating to control surfaces for aircraft

Info

Publication number
GB448827A
GB448827A GB35188/35A GB3518835A GB448827A GB 448827 A GB448827 A GB 448827A GB 35188/35 A GB35188/35 A GB 35188/35A GB 3518835 A GB3518835 A GB 3518835A GB 448827 A GB448827 A GB 448827A
Authority
GB
United Kingdom
Prior art keywords
aircraft
elevators
relating
control surfaces
hellington
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
GB35188/35A
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.)
ALEXANDER MCMAHON
Original Assignee
ALEXANDER MCMAHON
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 ALEXANDER MCMAHON filed Critical ALEXANDER MCMAHON
Priority to GB35188/35A priority Critical patent/GB448827A/en
Publication of GB448827A publication Critical patent/GB448827A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Elevator Control (AREA)

Abstract

448,827. Controlling aircraft. McMAHON, A., 28, Hellington Street, Edinburgh. Dec. 19, 1935, No. 35188. [Class 4] Aircraft controls comprise a right circular conical member 3 carrying tail planes 1 and elevators 4 set at a transverse dihedral angle and rotatably connected to the rear of the fuselage by ball bearings 9. As shown, the elevators 4 are adjustable through known linkage, the member 3 is provided with a sleeve 14 having friction rollers 10 and stops are provided to limit its movement. The member 3 is rotated by cables 13.
GB35188/35A 1935-12-19 1935-12-19 Improvements in or relating to control surfaces for aircraft Expired GB448827A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB35188/35A GB448827A (en) 1935-12-19 1935-12-19 Improvements in or relating to control surfaces for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB35188/35A GB448827A (en) 1935-12-19 1935-12-19 Improvements in or relating to control surfaces for aircraft

Publications (1)

Publication Number Publication Date
GB448827A true GB448827A (en) 1936-06-16

Family

ID=10374867

Family Applications (1)

Application Number Title Priority Date Filing Date
GB35188/35A Expired GB448827A (en) 1935-12-19 1935-12-19 Improvements in or relating to control surfaces for aircraft

Country Status (1)

Country Link
GB (1) GB448827A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2424889A (en) * 1943-08-20 1947-07-29 Tracy S Holmes Airplane control system
US2480040A (en) * 1943-12-06 1949-08-23 Wilbur A E Mitchell Aircraft control surfaces
US2500689A (en) * 1945-02-05 1950-03-14 Lockheed Aircraft Corp Coupled control surface for aircraft

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2424889A (en) * 1943-08-20 1947-07-29 Tracy S Holmes Airplane control system
US2480040A (en) * 1943-12-06 1949-08-23 Wilbur A E Mitchell Aircraft control surfaces
US2500689A (en) * 1945-02-05 1950-03-14 Lockheed Aircraft Corp Coupled control surface for aircraft

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