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
GB1333/41A
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.)
ARTHUR WALTER BANFIELD
Original Assignee
ARTHUR WALTER BANFIELD
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 ARTHUR WALTER BANFIELDfiledCriticalARTHUR WALTER BANFIELD
Priority to GB1333/41ApriorityCriticalpatent/GB544697A/en
Publication of GB544697ApublicationCriticalpatent/GB544697A/en
B64C17/00—Aircraft stabilisation not otherwise provided for
B—PERFORMING OPERATIONS; TRANSPORTING
B64—AIRCRAFT; AVIATION; COSMONAUTICS
B64C—AEROPLANES; HELICOPTERS
B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
B64C2001/0045—Fuselages characterised by special shapes
Landscapes
Engineering & Computer Science
(AREA)
Aviation & Aerospace Engineering
(AREA)
Soundproofing, Sound Blocking, And Sound Damping
(AREA)
Exhaust Silencers
(AREA)
Abstract
544,697. Exhaust silencers. BANFIELD, A. W. Jan. 31, 1941, No. 1333. [Class 7 (ii)] [Also in Group XXXIII] To reduce the noise of aircraft engines while sound observations are being taken, a silencer L is provided for each engine, a swivelling connection M being movable opposite to or away from the engine exhaust.
GB1333/41A1941-01-311941-01-31Improvements in or relating to aircraft
ExpiredGB544697A
(en)