GB1251476A - - Google Patents

Info

Publication number
GB1251476A
GB1251476A GB2483470A GB1251476DA GB1251476A GB 1251476 A GB1251476 A GB 1251476A GB 2483470 A GB2483470 A GB 2483470A GB 1251476D A GB1251476D A GB 1251476DA GB 1251476 A GB1251476 A GB 1251476A
Authority
GB
United Kingdom
Prior art keywords
vanes
engine
cascade
efflux
struts
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
GB2483470A
Other languages
English (en)
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 filed Critical
Publication of GB1251476A publication Critical patent/GB1251476A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C23/00Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/005Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Turbines (AREA)
GB2483470A 1970-05-22 1970-05-22 Expired GB1251476A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2483470 1970-05-22

Publications (1)

Publication Number Publication Date
GB1251476A true GB1251476A (de) 1971-10-27

Family

ID=10217971

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2483470A Expired GB1251476A (de) 1970-05-22 1970-05-22

Country Status (1)

Country Link
GB (1) GB1251476A (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2402251A3 (de) * 2010-07-01 2015-08-05 Rolls-Royce plc Triebwerkeinbau

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2402251A3 (de) * 2010-07-01 2015-08-05 Rolls-Royce plc Triebwerkeinbau

Similar Documents

Publication Publication Date Title
US2846165A (en) Aircraft control system
US3920203A (en) Thrust control apparatus for obtaining maximum thrust reversal in minimum time upon landing of an aircraft
US4019696A (en) Method of and apparatus for enhancing Coanda flow attachment over a wing and flap surface
US2891740A (en) External-flow jet flap
US3090584A (en) Aircraft
US2839891A (en) Thrust reversers for jet engines
GB1294349A (en) Improvements in or relating to high speed aircraft
US3971534A (en) Method of and apparatus for controlling flow attachment to the wing and flap surfaces of an upper surface blowing type aircraft
GB1465125A (en) Wing leading-edge slat system
GB1212705A (en) An aircraft
US2995010A (en) Adjustable propulsion nozzles
US3083936A (en) Aircraft
US3977630A (en) STOL aircraft
GB1130268A (en) Improvements in or relating to gas turbine by-pass engines
US4436261A (en) V/STOL Aircraft
US2846164A (en) Vertical take-off and landing aircraft
US2960281A (en) Control device for the air intake of a jet propulsion unit
US2943816A (en) Vertical take-off high-speed aircraft
US3884433A (en) Wing mounted thrust reverser
US3041830A (en) Steering deflector for a turbo-fan engine
GB1381646A (en) Aircraft with short take-off and landing characteristics
GB1251476A (de)
US3025027A (en) Vertical airfoil
US2961198A (en) Aircraft power plant
GB953301A (en) Convertible helicopter

Legal Events

Date Code Title Description
PS Patent sealed
PLNP Patent lapsed through nonpayment of renewal fees