GB667912A - Improvements in aircraft - Google Patents

Improvements in aircraft

Info

Publication number
GB667912A
GB667912A GB10722/50A GB1072250A GB667912A GB 667912 A GB667912 A GB 667912A GB 10722/50 A GB10722/50 A GB 10722/50A GB 1072250 A GB1072250 A GB 1072250A GB 667912 A GB667912 A GB 667912A
Authority
GB
United Kingdom
Prior art keywords
control
aircraft
pilot
actuation
speed
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
GB10722/50A
Inventor
Frederick Francis Crocombe
Geoffrey Terence Roland Hill
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.)
Blackburn and General Aircraft Ltd
Original Assignee
Blackburn and General Aircraft Ltd
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 Blackburn and General Aircraft Ltd filed Critical Blackburn and General Aircraft Ltd
Priority to GB10722/50A priority Critical patent/GB667912A/en
Publication of GB667912A publication Critical patent/GB667912A/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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/08—Stabilising surfaces mounted on, or supported by, wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C2009/005—Ailerons

Abstract

667,912. Aircraft control surfaces. BLACKBURN & GENERAL AIRCRAFT, Ltd. May 1, 1950, No. 10723/50. Drawings to Specification. Class 4. In an aircraft having fixed swept-back wings each wing has a movable tip for lateral control at high speed and a normal trailing edge aileron for lateral control at low speed, which are operated through a mechanism connected to a selecting device under the pilot's control such that the mechanism is conditioned to actuate the appropriate control surface simply by actuation of such device appropriately to the speed of the aircraft. The arrangement of the control transmission and control surfaces described. is similar to that for an aircraft with variable stveep-back wings as described in Specification 667,911, except that the inboard end of the rod 24 is connected by a linkage to a pilot's control member instead of being pivotally connected to the fuselage. The appropriate control surface is brought into operation by actuation of the pilot's control member.
GB10722/50A 1950-05-01 1950-05-01 Improvements in aircraft Expired GB667912A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB10722/50A GB667912A (en) 1950-05-01 1950-05-01 Improvements in aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB10722/50A GB667912A (en) 1950-05-01 1950-05-01 Improvements in aircraft

Publications (1)

Publication Number Publication Date
GB667912A true GB667912A (en) 1952-03-12

Family

ID=9973086

Family Applications (1)

Application Number Title Priority Date Filing Date
GB10722/50A Expired GB667912A (en) 1950-05-01 1950-05-01 Improvements in aircraft

Country Status (1)

Country Link
GB (1) GB667912A (en)

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