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
GB21881/54A
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.)
MAXIMILIAN CHARLES JANISCH
Original Assignee
MAXIMILIAN CHARLES JANISCH
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 MAXIMILIAN CHARLES JANISCHfiledCriticalMAXIMILIAN CHARLES JANISCH
Priority to GB21881/54ApriorityCriticalpatent/GB780074A/en
Publication of GB780074ApublicationCriticalpatent/GB780074A/en
B64C17/00—Aircraft stabilisation not otherwise provided for
Landscapes
Engineering & Computer Science
(AREA)
Aviation & Aerospace Engineering
(AREA)
Emergency Lowering Means
(AREA)
Abstract
780,074. Stabilizing aircraft. JANISCH, M. C. July 27, 1954, No. 21881/54. Class 4. An aeroplane comprising a fuselage 3 and wings 1, 2 is stabilized by a weight 4 which is suspended by cables 5, 6 mounted on pulleys 7, 8 and connected to a winch within the fuselage. The weight, housed in position 4<SP>1</SP> during landing and take-off is lowered during flight to lower the position of the overall centre of gravity G and thereby stabilize the aircraft in flight. The weight may be provided with contacts so that when it encounters on obstruction a warning will be shown or sounded in the cockpit.
A possibility for avoiding surface roughness caused by insects on aircraft(Use of elastic surfaces on wing leading edges and fuselage edges of aircraft with boundary layer control, to avoid surface roughness due to insects)
Results of flight tests on a slender wing low speed research aircraft/H. P. 115/(Flight tests on stability and handling qualities of slender wing low speed Handley Page H. P. 115 aircraft)
Investigation of jet transport aircraft vortex systems descending into and generated in ground effect(Flight tests of heavy jet transport aircraft to determine characteristics of vortex systems generated within ground effect and vortex systems descending into ground effect)[Data Report, 27 May- 6 Jun. 1970]