Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
283 words
An aircraft video system utilizing an aircraft and operation on board intended for air surveyance of ground activity comprising a technical container attached to the aircraft, a transparent radome forming a forward portion of said container, a pilot camera inclinable in angle of sight and azimuth located in said radome, a television monitor screen in the aircraft connected to said camera, a remotely controlled inclination means for controlling inclination and for controlling the object-lens of said camera in said radome connected to said camera, a television transmitter with its transmission aerial in a rearward portion of said container, said remotely controlled means including a structure secured to said container through damping means, a cradle connected to said structure, a first means for pivoting said camera in azimuth with respect to said cradle, a second means for pivoting in sight said cradle with respect to said structure, electric motors having pulleys with two directions of rotation connected to further pulleys linked to said camera, and said electric motors also connected through cables to said cradle, a remote-control box connected to said remotely controlled means located to be acted upon by instinctive reaction of the operator while observing said television monitor screen, said remote-control box including a pivoted axis shaft pivoted in an elastic block, four microswitches controlling said electric motors for controlling camera inclination, said shaft having a lower portion which acts upon said microswitches, a plate in said box having a psuedo-square opening therein, said lower portion of said shaft having protuberant parts on either side of a portion of said shaft itself included in said psuedo-square opening to prevent undesired action on said microswitches by allowing only limited deviations of said shaft.
Claim 2
Dependent Claim
283 words
An aircraft video system utilizing an aircraft and operation on board intended for air surveyance of ground activity comprising a technical container attached to the aircraft, a transparent radome forming a forward portion of said container, a pilot camera inclinable in angle of sight and azimuth located in said radome, a television monitor screen in the aircraft connected to said camera, a remotely controlled inclination means for controlling inclination and for controlling the object-lens of said camera in said radome connected to said camera, a television transmitter with its transmission aerial in a rearward portion of said container, said remotely controlled means including a structure secured to said container through damping means, a cradle connected to said structure, a first means for pivoting said camera in azimuth with respect to said cradle, a second means for pivoting in sight said cradle with respect to said structure, electric motors having pulleys with two directions of rotation connected to further pulleys linked to said camera, and said electric motors also connected through cables to said cradle, a remote-control box connected to said remotely controlled means located to be acted upon by instinctive reaction of the operator while observing said television monitor screen, said remote-control box including a pivoted axis shaft pivoted in an elastic block, four microswitches controlling said electric motors for controlling camera inclination, said shaft having a lower portion which acts upon said microswitches, a plate in said box having a psuedo-square opening therein, said lower portion of said shaft having protuberant parts on either side of a portion of said shaft itself included in said psuedo-square opening to prevent undesired action on said microswitches by allowing only limited deviations of said shaft.
Claim 3
Dependent Claim
80 words
An aircraft video system in accordance with claim 1, further characterized by a second radome formed in a rearward portion of said technical container, a slave camera in said second radome, connected to said television monitor screen, a second cradle pivotly supporting said slave camera, limit switches controlling reversing switches located for actuation by said pilot and slave cameras to permit selection of a pertinent video display from one of said cameras, and the switching off of the unused camera.
Claim 4
Dependent Claim
35 words
An aircraft video system as in claim 2 wherein at least said pulleys linked to said camera and said cradle are also connected to potentiometers providing electrical information relative to the position of the camera.
Claim 5
Dependent Claim
36 words
An aircraft video system in accordance with claim 1, further characterized by said remotely controlled means further including servo amplifiers controlling said electric motors, potentiometers mounted in said remote-control box and connected to said servo amplifiers.
Claim 6
Dependent Claim
239 words
An aircraft video system utilizing an aircraft and operation on board intended for air surveyance of ground activity comprising a technical container attached to the aircraft, a transparent radome forming a forward portion of said container, a pilot camera inclinable in angle of sight and azimuth located in said radome, a television monitor screen in the aircraft connected to said camera, a remotely controlled inclination means for controlling inclination and for controlling the object-lens of said camera in said radome connected to said camera, a television transmitter connected to said camera, said remotely controlled means including a cradle connected to said container, a first means for pivoting said camera in azimuth with respect to said cradle, a second means for pivoting in sight said cradle with respect to said container, electric motors connected to said camera, and to said cradle, a remote-control box connected to said remotely controlled means located to be acted upon by instinctive reaction of the operator while observing said television monitor screen, said remote-control box including a pivoted axis shaft, microswitches controlling said electric motors for controlling camera inclination, said shaft having a portion which acts upon said microswitches a plate in said box havng an opening therein, said portion of said shaft having protuberant parts on either side of a portion of said shaft itself included in said opening to prevent undesired action on said microswitches by allowing only limited deviations of said shaft.
Claim 7
Dependent Claim
239 words
An aircraft video system utilizing an aircraft and operation on board intended for air surveyance of ground activity comprising a technical container attached to the aircraft, a transparent radome forming a forward portion of said container, a pilot camera inclinable in angle of sight and azimuth located in said radome, a television monitor screen in the aircraft connected to said camera, a remotely controlled inclination means for controlling inclination and for controlling the object-lens of said camera in said radome connected to said camera, a television transmitter connected to said camera, said remotely controlled means including a cradle connected to said container, a first means for pivoting said camera in azimuth with respect to said cradle, a second means for pivoting in sight said cradle with respect to said container, electric motors connected to said camera, and to said cradle, a remote-control box connected to said remotely controlled means located to be acted upon by instinctive reaction of the operator while observing said television monitor screen, said remote-control box including a pivoted axis shaft, microswitches controlling said electric motors for controlling camera inclination, said shaft having a portion which acts upon said microswitches a plate in said box havng an opening therein, said portion of said shaft having protuberant parts on either side of a portion of said shaft itself included in said opening to prevent undesired action on said microswitches by allowing only limited deviations of said shaft.