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.)
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Safran Aerosystems SAS
Original Assignee
Aerazur Constructions Aeronautiques SA
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Filing date
Publication date
Application filed by Aerazur Constructions Aeronautiques SAfiledCriticalAerazur Constructions Aeronautiques SA
Publication of GB1207136ApublicationCriticalpatent/GB1207136A/en
B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
B64F1/00—Ground or aircraft-carrier-deck installations
B64F1/02—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables
B64F1/027—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables using net or mesh
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Engineering & Computer Science
(AREA)
Mechanical Engineering
(AREA)
Aviation & Aerospace Engineering
(AREA)
Packages
(AREA)
GB49973/67A1966-11-031967-11-03Improvements to aircraft stopping or arresting barriers
ExpiredGB1207136A
(en)
Experimental study of wind-tunnel wall effects and wall corrections for a general-research v/stol tilt-wing model with flap(Wind tunnel wall effects and wall corrections for vertical short takeoff and landing tilt-wing model with flap)
An approach to the evaluation of propulsion systems in v/stol aircraft(Propulsion systems evaluation of vertical and short takeoff and landing aircraft)
The wall jet beneath a counter-flowing stream Final technical report, Sep. 1966- Mar. 1968(Wall jet wind tunnel tests in two dimensional flow used to simulate ground effect of vertical takeoff aircraft)
Longitudinal flight control of tilt-wing v/stol aircraft during hovering and transition, considering flow separation, pitching moment and control system
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)
Flow field survey and decelerator drag characteristics in the wake of a model of the X-15 airplane at Mach 2. 30 and 4. 65(Flow field survey and decelerator drag characteristics in wake of model X-15 airplane at Mach 2. 30 and 4. 65)
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]