Roll drum sensor housing having sliding window

Claim 2

An improved roll drum housing for use on board an aircraft, said housing having a hollow cavity in which is received a sensor apparatus, said housing being rotatable about a roll axis that is generally parallel to the flight path of said aircraft, wherein said sensor apparatus rolls about said axis correspondingly with drum housing rotation, said sensor apparatus further being independently pivotable in said housing about a separate azimuthal axis, the improvement comprising: a window frame opening in a sidewall of said housing; a window frame member slidably positioned across said opening, said frame member having a window aperture which provides said sensor apparatus with a view from inside to outside said housing; means for sliding said window frame member back and forth in a direction generally parallel to said roll axis, said sliding means being operatively connected to said sensor apparatus in a manner so that said window sliding occurs correspondingly with azimuthal pivoting of said sensor apparatus, so that said window aperture is continually positioned to permit said sensor apparatus with a view outside said housing as said apparatus changes azimuthal positions in said housing.

Claim 3

The improvement of claim 1, wherein said roll drum housing is cylindrical, and wherein said aircraft includes a fuselage roof portion shaped to cradle a lower circumferential portion of said drum housing, for supporting said housing on top of said fuselage, and wherein an upper circumferential portion of said housing is normally exposed to the atmosphere, said window frame opening being normally positioned in said upper circumferential portion when it is desired to operate said sensor apparatus, so that a boundary layer airflow develops on said upper circumferential portion and across said window aperture, and including said window aperture in said window frame member having an upstream edge and a downstream edge, said downstream edge extending inwardly into said housing cavity with respect to said upstream edge, and further including first blower means, positioned adjacent said upstream edge, for blowing high pressure air across said window aperture and into said boundary layer airflow, and still further including, second blower means for blowing high pressure air into said housing cavity, for pressurizing said cavity in a manner so that pressurized air moves outwardly from said cavity through said window aperture, wherein said inwardly extending downstream edge and said first and second blower means cooperate with each other to create uniformity in said boundary layer airflow.

Claim 4

The improvement of claim 2, wherein said first blower means includes a telescopic conduit having an air blowing port positioned adjacent said upstream edge of said window aperture, said conduit being extendible and retractable correspondingly with back and forth movement of said window frame member, in a manner so that said air blowing port remains adjacent said upstream edge as said window frame member moves.

Claim 5

The improvement of claim 3, wherein said second blower means is adjustable to control the amount of high pressure air blown into said cavity.

Claim 6

The improvement of claim 1, wherein said sliding means includes a cable cradle portion fixedly connected to said sensor apparatus in a manner so that said cradle portion pivots correspondingly with pivoting movement of said sensor apparatus, said cradle portion having a curved portion, a first line operatively connected to an upstream end of said window frame member, in a manner so that a pulling force can be transmitted through said line to slide said frame member in one direction, a second line operatively connected to a downstream end of said window frame member, in a manner so that a pulling force can be transmitted through said second line to slide said frame member in another direction, cable loop means operatively connecting said first and second lines to said curved portion of said cradle portion, for causing a pulling force to be transmitted through said lines in response to cradle portion pivoting, wherein cradle portion pivoting in one rotational direction causes said window frame member to slide in one direction, and vice versa when said cradle portion pivots in the opposite direction.

Claim 7

The improvement of claim 1, wherein said window aperture in said window frame member has an upstream edge and a downstream edge, said downstream edge extending inwardly into said housing cavity with respect to said upstream edge.

Claim 8

The improvement of claim 1, including first blower means, positioned adjacent an upstream edge of said window frame member, for blowing high pressure air across said window aperture.

Claim 9

The improvement of claim 1, including second blower means for blowing high pressure air into said housing cavity, for pressurizing said cavity in a manner so that pressurized air moves outwardly from said cavity through said window aperture.

Claim 10

For a sensor positioned in a cavity within a housing which is mounted onboard an aircraft, said housing having a window aperture for providing said sensor with a line-of-sight view from said cavity outside said housing, said sensor being pivotably mounted in said housing cavity, said window aperture normally being exposed to airflow outside said aircraft during operation of said sensor such that a boundary layer airflow develops across said aperture, an apparatus for controlling said boundary layer airflow, comprising: means defining an upstream edge of said window aperture; means defining a downstream edge of said window aperture, wherein said downstream edge extends inwardly into said housing with respect to said upstream edge; first blower mans, positioned adjacent said upstream edge, for blowing high pressure air across said window aperture and into said boundary layer airflow; second blower means for blowing high pressure air into said housing cavity, for pressurizing said cavity in a manner so that such air moves outwardly from said cavity through said window aperture; and means for sliding said window aperture back and forth in response to pivoting movement of said sensor in said housing, so that said window aperture is continually positioned to provide said sensor with said line-to-sight view as said sensor pivots.

Claim 11

For a sensor positioned in a cavity within a housing which is mounted onboard an aircraft, said housing having a window aperture for providing said sensor with a line-of-sight view from said cavity outside said housing, said sensor being pivotably mounted in said housing cavity, said window aperture normally being exposed to airflow outside said aircraft during operation of said sensor such that a boundary layer airflow develops across said aperture, an apparatus for controlling said boundary layer airflow, comprising: means defining an upstream edge of said window aperture; means defining a downstream edge of said window aperture, wherein said downstream edge extends inwardly into said housing with respect to said upstream edge; first blower mans, positioned adjacent said upstream edge, for blowing high pressure air across said window aperture and into said boundary layer airflow; second blower means for blowing high pressure air into said housing cavity, for pressurizing said cavity in a manner so that such air moves outwardly from said cavity through said window aperture; and means for sliding said window aperture back and forth in response to pivoting movement of said sensor in said housing, so that said window aperture is continually positioned to provide said sensor with said line-to-sight view as said sensor pivots.

Claim 12

The apparatus of claim 9, wherein said sliding means includes a cradle portion fixedly connected to said sensor in a manner so that said cradle portion pivots correspondingly with pivoting movement of said sensor, said cradle portion having a curved portion, a first line operatively connected to an upstream end of said window aperture, in a manner so that a pulling force can be transmitted through said like to slide said window aperture in one direction, a second line operatively connected to a downstream end of said window aperture, in a manner so that a pulling force can be transmitted through said second line to slide window aperture in another direction, cable loop means operatively connecting said first and second lines to said curved portion of said cradle portion, for causing a pulling force to be transmitted through said lines in response to cradle portion pivoting, wherein cradle portion pivoting in one rotational direction causes said window aperture to slide in one direction, and vice versa when said cradle portion pivots in the opposite direction.

Claim 13

The apparatus of claim 9, including means defining an upper and a lower transverse edge of said window aperture, said transverse edges connecting said aperture's upstream edge to its downstream edge, said transverse edges also extending inwardly into said housing cavity with respect to said upstream edge.

Claim 14

For a sensor positioned in a cavity within a housing mounted onboard an aircraft, said housing having a window aperture for providing said sensor with a line-of-sight view from said cavity outside said housing, said sensor being pivotably mounted in said housing cavity, said window aperture normally being exposed to airflow outside said aircraft during operation of said sensor such that a boundary layer airflow develops across said aperture, an apparatus for controlling said boundary layer airflow, including: means for sliding said window aperture back and forth in response to pivoting movement of said sensor in said housing, so that said window aperture is continually positioned to provide said sensor with said line-of-sight view as said sensor pivots; a telescopic conduit having an air blowing port positioned adjacent said upstream edge of said window aperture for blowing high pressure air across said window aperture and into said boundary layer airflow, said conduit being extendible and retractable correspondingly with back and forth movement of said aperture in a manner so that said air blowing port remains adjacent said upstream edge as said aperture moves.

Claim 15

For a sensor positioned in a cavity within a housing mounted onboard an aircraft, said housing having a window aperture for providing said sensor with a line-of-sight view from said cavity outside said housing, said sensor being pivotably mounted in said housing cavity, said window aperture normally being exposed to airflow outside said aircraft during operation of said sensor such that a boundary layer airflow develops across said aperture, an apparatus for controlling said boundary layer airflow, including: means for sliding said window aperture back and forth in response to pivoting movement of said sensor in said housing, so that said window aperture is continually positioned to provide said sensor with said line-of-sight view as said sensor pivots; a telescopic conduit having an air blowing port positioned adjacent said upstream edge of said window aperture for blowing high pressure air across said window aperture and into said boundary layer airflow, said conduit being extendible and retractable correspondingly with back and forth movement of said aperture in a manner so that said air blowing port remains adjacent said upstream edge as said aperture moves.

Claim 16

The apparatus of claim 12, wherein said aperture further includes a downstream edge which extends inwardly into said housing cavity with respect to said upstream edge.

Claim 17

The apparatus of claim 3, including means defining an upper and lower transverse edge of said window aperture, said transverse edges connecting said aperture's upstream edge to its downstream edge, said transverse edges also extending inwardly into said housing cavity with respect to said upstream edge.