Aircraft control yoke
First Claim
1. In an aircraft having a control yoke and having an airbag associated therewith, said airbag being subject to inflation as a function of forces exerted upon the aircraft, the improvement comprising;
- said control yoke having first and second portions that are movable from a normal position to an extended position, to thereby form a control yoke of extended length, andforce means operable as a function of airbag inflation to effect movement of said control yoke to said extended position.
2 Assignments
0 Petitions
Accused Products
Abstract
An airbag module is positioned relative to an aircraft control yoke or shaft, the airbag being actuated by majority voting sensors that are responsive to acceleration forces upon the aircraft. The aircraft control yoke or control yoke post is constructed to telescope, extend, or move a limited distance toward the pilot as the airbag inflates. The yoke carries telescoping, extendable, or movable handle portions that allow left and right hand pilot grip handles to move, if necessary, under the force of the expanding airbag. Hand sleeves may be provided to help maintain the pilot'"'"'s hands on the grip handles during airbag expansion. The movable yoke and handle portions may be manually or automatically restored to normal operative positions after airbag deflation. The yoke may be formed so as to provide a U shaped section that accommodates a horizontal support or table for holding the airbag module, a map, or a like device. The U shaped yoke and table support members are structured such that the table remains horizontal during pivoting movement of the yoke to control aircraft roll, and during generally horizontal movement of the yoke to control aircraft pitch.
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Citations
46 Claims
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1. In an aircraft having a control yoke and having an airbag associated therewith, said airbag being subject to inflation as a function of forces exerted upon the aircraft, the improvement comprising;
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said control yoke having first and second portions that are movable from a normal position to an extended position, to thereby form a control yoke of extended length, and force means operable as a function of airbag inflation to effect movement of said control yoke to said extended position. - View Dependent Claims (2, 3)
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4. In combination;
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a two-piece elongated aircraft control yoke, said two pieces of said control yoke having a normal relative position whereby said control yoke is operable to effect two modes of aircraft control, an airbag associated with said control yoke, said airbag being subject to inflation as a function of an aircraft force, and force means operable as a function of airbag inflation to effect movement of said two pieces of said control yoke to an extended length relative position, whereat said control yoke is operable to effect only one of said two modes of aircraft control. - View Dependent Claims (5, 6)
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7. In combination;
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an elongated aircraft control yoke comprising a two-piece tubular member having a central axis, said control yoke having a first piece extending from a control panel, and a second piece extending from said first piece and terminating at a T-shaped portion that includes a left-hand grip and a right-hand grip, said first piece of said control yoke being rotatable about said axis to control aircraft roll, and said first piece of said control yoke being movable along said axis to control aircraft angle of attack, said two pieces of said control yoke having a normal relative position, whereby said hand grips are operable to effect control of both aircraft roll and aircraft angle of attack, an airbag associated with said control yoke, said airbag being subject to inflation as a function of an aircraft force, force means operable as a function of airbag inflation to effect relative movement of said two pieces of said control yoke to an extended length relative position, and said control yoke being constructed to accommodate only rotation of said control yoke when in said extended length relative position, whereby said hand grips are operable to effect control of only aircraft roll. - View Dependent Claims (8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19)
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20. An aircraft control yoke extending outward from a generally vertical aircraft instrument panel, comprising;
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a first rigid, elongated, and generally horizontal yoke member rotatable about a generally horizontal axis to control aircraft roll and movable toward and away from said instrument panel to control aircraft pitch, said first horizontal yoke member having a first end extending toward said instrument panel and having a second end, a rigid, upward facing, U-shaped yoke post member having two horizontally spaced and vertically extending side legs whose bottom ends are joined together by a bottom leg, a top end of a first of said side legs being connected to said second end of said first horizontal yoke member, first and a second elongated guide slots formed in said side legs so as to place said guide slots in parallel facing relation to each other, a generally horizontal support member located within said U-shaped yoke post portion, a rigid, elongated, guide rod carried by said support member, said guide rod having opposite ends thereof freely slidable in said first and second guide slots, and extendable support means mounting said support member to be supported by said instrument panel. - View Dependent Claims (21, 22, 23, 24, 25)
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26. An aircraft control yoke extending outward from a generally vertical aircraft instrument panel, comprising;
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a first rigid, elongated, and generally horizontal yoke member rotatable about a generally horizontal axis to control aircraft roll and movable toward and away from said instrument panel to control aircraft pitch, said first horizontal yoke member having a first end extending toward said instrument panel and having a second end, a rigid, upward facing, U-shaped yoke member having two horizontally spaced and vertically extending side legs, whose bottom ends are joined together by a bottom leg, a top end of a first of said side legs being connected to said second end of said first horizontal yoke member, first and a second elongated guide slots formed in said side legs so as to place said guide slots in parallel facing relation to each other, a generally horizontal support member located within said U-shaped yoke portion, said support member having an upper surface, a rigid, elongated, guide rod carried by said support member, said guide rod having opposite ends thereof freely slidable in said first and second guide slots, extendable support means mounting said support member to be supported by said instrument panel, an airbag mounted on said upper surface of said support member, said airbag being subject to inflation as a function of forces exerted upon the aircraft, said first yoke member having first and second portions that are movable from a normal position to an extended position, to thereby form a control yoke of extended length, and force means operable as a function of airbag inflation to effect movement of said control yoke to said extended position. - View Dependent Claims (27, 28, 29, 30, 31, 32, 33)
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34. An aircraft control yoke extending outward from a generally vertical aircraft instrument panel, comprising;
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an upward facing U-shaped yoke member having two horizontally spaced and vertically extending side legs having top ends and having bottom ends that are joined together by a bottom leg, first and second elongated guide slots formed in said side legs so as to place said guide slots in parallel facing relation to each other, a generally horizontal support table located within said U-shaped yoke portion, a guide rod carried by said support table, said guide rod having opposite ends thereof freely slidable in said first and second guide slots, extendable support means mounting said table to be supported by said instrument panel, an airbag mounted on said table, said airbag being subject to inflation as a function of an aircraft force, a two piece, horizontally extending yoke member rotatable about a generally horizontal axis to control aircraft roll and movable toward and away from said instrument panel to control aircraft pitch, a first piece of said two piece yoke member extending from said instrument panel, and a second piece of said two piece yoke member extending from said first piece to a top end of a first of said side members, said two piece yoke member having a normal relative position whereby said two piece yoke member is operable to effect control of both aircraft roll and aircraft angle of attack, force means operable as a function of airbag inflation to effect relative movement of said two pieces of said two piece yoke member to an extended length relative position, and said two piece yoke member being constructed to accommodate only aircraft roll control when in said extended position. - View Dependent Claims (35, 36, 37, 38, 39, 40, 41, 42, 43, 44, 45, 46)
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Specification