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US4901952A Expired / Lapsed US ⏱️ 0.0 years remaining

Control apparatus

Assignee: BAE Systems PLC
•
Filing: 1988-06-23
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Granted: 1990-02-20
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Expires: 2008-06-23
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Abstract

Abstract Control apparatus for effecting control of thrust magnitude and thrust vector angle for aircraft of the short take-off and vertical landing type known by the acronym STOVL comprises a fixed housing (10), a manually movable stick member (7) supported with respect to the fixed housing (10) and arranged to provide a throttle input, the stick member (7) including a grip (8) to enable it to be gripped and moved manually relative to the fixed housing (10), and a rotatable collar (9) arranged to provide the thrust vector angle input. Preferably the grip includes an upright hand-datum flange (13) for positively laterally locating a controlling hand and the hand-datum flange (13) is located at one extremity of the grip (8) and the collar (9) is located at the other extremity of the grip (8).

Inventors

  • 👤 Neil J. Curtis

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-24 18:40
CPC Classifications
B; B64; B64D; B64D31/00; B64D31/02; B64D31/04; G; G05; G05G; G05G13/00; Y; Y10; Y10T; Y10T74/00; Y10T74/20; Y10T74/20012; Y10T74/20201

Claims Analysis

Total Claims: 18
Claim 1
Independent Claim 133 words
A control apparatus for an aircraft of the vectored thrust type arranged to produce control signals in response to control movements, including: a fixed housing; a manually movable stick member supported with respect to said fixed housing and arranged to provide a first control signal corresponding to thrust magnitude demand, said thrust magnitude demand being determined by the location of said stick member with respect to said housing; said stick member including a grip to enable it to be gripped and moved manually with respect to said fixed housing so as to vary said thrust magnitude demand; and a rotatable collar mounted on said grip and arranged to provide a second control signal corresponding to thrust vector angle demand, said thrust vector angle demand being determined by an angular orientation of said collar.
Claim 2
Dependent Claim 133 words
A control apparatus for an aircraft of the vectored thrust type arranged to produce control signals in response to control movements, including: a fixed housing; a manually movable stick member supported with respect to said fixed housing and arranged to provide a first control signal corresponding to thrust magnitude demand, said thrust magnitude demand being determined by the location of said stick member with respect to said housing; said stick member including a grip to enable it to be gripped and moved manually with respect to said fixed housing so as to vary said thrust magnitude demand; and a rotatable collar mounted on said grip and arranged to provide a second control signal corresponding to thrust vector angle demand, said thrust vector angle demand being determined by an angular orientation of said collar.
Claim 3
Dependent Claim 29 words
A control apparatus according to claim 1, in which said grip includes an upright hand-datum flange for positively laterally locating a controlling hand with respect to said rotatable collar.
Claim 4
Dependent Claim 32 words
A control apparatus according to claim 2, in which said hand-datum flange is located at one extremity of said grip and said collar is located at the other extremity of said grip.
Claim 5
Dependent Claim 30 words
A control apparatus according to claim 1, in which the attitude of said manually movable stick member, with respect to a pilot, remains substantially constant throughout its range of movement.
Claim 6
Dependent Claim 17 words
A control apparatus according to claim 1, in which said collar includes a manually releasable friction lock.
Claim 7
Dependent Claim 17 words
A control apparatus according to claim 4, in which said collar includes a manually releasable friction lock.
Claim 8
Dependent Claim 29 words
A control apparatus according to claim 1, in which said control apparatus also includes a selectable stop mechanism selectively to limit the range of angular movement of said collar.
Claim 9
Dependent Claim 25 words
A control apparatus according to claim 1, in which said collar includes a number of preset angular detents at locations corresponding to predetermined angular orientations.
Claim 10
Dependent Claim 13 words
A control apparatus according to claim 1, which also includes ancillary control switches.
Claim 11
Dependent Claim 174 words
A control apparatus for a vectored thrust aircraft arranged to produce a thrust magnitude demand signal and a thrust vector angle demand signal in response to control movements, said apparatus including: a fixed housing; a manually movable stick member supported with respect to said fixed housing, the attitude of said manually movable stick member remaining substantially constant with respect to a pilot throughout its range of movement, said thrust magnitude demand signal being provided by the location of said stick member with respect to said fixed housing; said stick member including a grip to enable it to be gripped and moved manually relative to said fixed housing; a rotatable collar mounted on said grip, said thrust vector angle demand signal being provided by the angular orientation of said collar; and an upright hand-datum flange located on said grip for positively laterally locating a controlling hand with respect to said rotatable collar, said hand-datum flange being located at one extremity of said grip and said collar being located at the other extremity of said grip.
Claim 12
Dependent Claim 174 words
A control apparatus for a vectored thrust aircraft arranged to produce a thrust magnitude demand signal and a thrust vector angle demand signal in response to control movements, said apparatus including: a fixed housing; a manually movable stick member supported with respect to said fixed housing, the attitude of said manually movable stick member remaining substantially constant with respect to a pilot throughout its range of movement, said thrust magnitude demand signal being provided by the location of said stick member with respect to said fixed housing; said stick member including a grip to enable it to be gripped and moved manually relative to said fixed housing; a rotatable collar mounted on said grip, said thrust vector angle demand signal being provided by the angular orientation of said collar; and an upright hand-datum flange located on said grip for positively laterally locating a controlling hand with respect to said rotatable collar, said hand-datum flange being located at one extremity of said grip and said collar being located at the other extremity of said grip.
Claim 13
Dependent Claim 17 words
A control apparatus according to claim 10, in which said collar includes a manually releasable friction lock.
Claim 14
Dependent Claim 29 words
A control apparatus according to claim 10, in which said control apparatus also includes a selectable stop mechanism selectively to limit the range of angular movement of said collar.
Claim 15
Dependent Claim 29 words
A control apparatus according to claim 11, in which said control apparatus also includes a selectable stop mechanism selectively to limit the range of angular movement of said collar.
Claim 16
Dependent Claim 25 words
A control apparatus according to claim 10, in which said collar includes a number of preset angular detents at locations corresponding to predetermined angular orientations.
Claim 17
Dependent Claim 25 words
A control apparatus according to claim 12, in which said collar includes a number of preset angular detents at locations corresponding to predetermined angular orientations.
Claim 18
Dependent Claim 13 words
A control apparatus according to claim 10, which also includes ancillary control switches.

References Cited (Backward Citations)

US2923502A Cited
US2787746A Cited
US3098628A Cited
US3599510A Cited
US3726497A Cited
US4130259A Cited
US4134560A Cited
US4280371A Cited
US4574651A Cited
US4567786A Cited
US4667909A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1993-02-19 1993-08-21 1994-02-20 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1997-02-19 1997-08-21 1998-02-20 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2001-02-19 2001-08-21 2002-02-20 $7700.00 Window Closed / Lapsed

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