US4787576A — Automatic multi-position G-protective ejection se…

Claim 1

Independent Claim 262 words

A G-protective ejection seat assembly for an occupant of the cockpit of an aircraft utilizing a separable ejection seat including propulsion means for separating the ejection seat from the cockpit and propelling the seat with the occupant therein free of the cockpit during ejection, comprising: a cradle having a non-articulated upper portion and a lower portion, said cradle upper portion being attachable to the aircraft for selective angular movement within the cockpit between an upright position and a reclined position, said cradle upper portion being selectively positionable during use in said upright and reclined positions, said cradle having control support means for supporting hand and foot flight controls of the aircraft for movement with said cradle, the ejection seat being releasably carried by and substantially stationary with respect to said cradle upper portion during non-ejection use, the seat being moved with said cradle upper portion as said cradle upper portion moves between said upright and reclined positions, said cradle being arranged to support the occupant in the seat in a normally upright position when said cradle upper portion is in said upright position and in a supine position when said cradle upper portion is in said reclined position, the ejection seat being movable upon ejection independent of said cradle and the hand and foot flight controls supported by said cradle, upon ejection said cradle and the hand and foot controls remaining in place within the aircraft while the seat is propelled out of the cockpit; and power means for selectively angularly moving said cradle upper portion between said upright and reclined positions.

Claim 2

Dependent Claim 262 words

A G-protective ejection seat assembly for an occupant of the cockpit of an aircraft utilizing a separable ejection seat including propulsion means for separating the ejection seat from the cockpit and propelling the seat with the occupant therein free of the cockpit during ejection, comprising: a cradle having a non-articulated upper portion and a lower portion, said cradle upper portion being attachable to the aircraft for selective angular movement within the cockpit between an upright position and a reclined position, said cradle upper portion being selectively positionable during use in said upright and reclined positions, said cradle having control support means for supporting hand and foot flight controls of the aircraft for movement with said cradle, the ejection seat being releasably carried by and substantially stationary with respect to said cradle upper portion during non-ejection use, the seat being moved with said cradle upper portion as said cradle upper portion moves between said upright and reclined positions, said cradle being arranged to support the occupant in the seat in a normally upright position when said cradle upper portion is in said upright position and in a supine position when said cradle upper portion is in said reclined position, the ejection seat being movable upon ejection independent of said cradle and the hand and foot flight controls supported by said cradle, upon ejection said cradle and the hand and foot controls remaining in place within the aircraft while the seat is propelled out of the cockpit; and power means for selectively angularly moving said cradle upper portion between said upright and reclined positions.

Claim 3

Dependent Claim 56 words

The ejection seat assembly of claim 1 wherein said cradle lower portion is movably attached to said cradle upper portion and the assembly further includes means for moving said cradle lower portion between a lowered position and a raised position in response to movement of said cradle upper portion between said upright and reclined positions, respectively.

Claim 4

Dependent Claim 32 words

The ejection seat assembly of claim 2 wherein said cradle lower portion includes a pair of spaced apart leg rests each separately pivoted to said cradle upper portion and to the aircraft.

Claim 5

Dependent Claim 26 words

The ejection seat assembly of claim 1 wherein said cradle upper portion is positionable in a plurality of angular positions between said upright and reclined positions.

Claim 6

Dependent Claim 40 words

The ejection seat assembly of claim 1 wherein said power means includes an actuator connected between said cradle and the aircraft for applying directed force on said cradle to move said cradle upper portion between said upright and reclined positions.

Claim 7

Dependent Claim 37 words

The ejection seat assembly of claim 1 further including upper cradle linkage arms pivotally attaching said cradle upper portion to the aircraft to provide pivotal movement of said cradle upper portion between said upright and reclined positions.

Claim 8

Dependent Claim 66 words

The ejection seat assembly of claim 6 further including lower cradle linkage arms pivotally attaching said cradle lower portion to the aircraft independently of said upper cradle linkage arms to pivotally move said cradle lower portion relative to said cradle upper portion between a lowered position and a raised position in response to movement of said cradle upper position between said upright and reclined positions, respectively.

Claim 9

Dependent Claim 33 words

The ejection seat assembly of claim 1 further including means for adjustably moving the ejection seat relative to said cradle upper portion to move the occupant to the design eyepoint of the aircraft.

Claim 10

Dependent Claim 48 words

The ejection seat assembly of claim 1 wherein said control support means includes upper support means for supporting said hand flight controls on said cradle upper portion for movement therewith, and lower support means for supporting said foot flight controls on said cradle lower portion for movement therewith.

Claim 11

Dependent Claim 26 words

The ejection seat assembly of claim 9 wherein said upper support means includes at least one arm rest to which said hand flight controls are mounted.

Claim 12

Dependent Claim 81 words

The ejection seat assembly of claim 1 for use with a display console positionable between the legs of the cockpit occupant, wherein said cradle lower portion includes a pair of leg rests, one leg rest being positioned to each side of the display console, whereby during ejection free upward travel of the occupant's legs is permitted uninhibited by the display console as the occupant is carried in the seat even upon ejection with said cradle upper portion in said reclined position.

Claim 13

Dependent Claim 27 words

The ejection seat assembly of claim 1 further including control means for controlling operation of said power means in response to sensed aircraft G-loading and anticipated G-loading.

Claim 14

Dependent Claim 41 words

The ejection seat assembly of claim 12 wherein said control means causes said power means to recline said cradle upper portion from said upright position when the greater of said sensed G-loading or said anticipated G-loading exceeds a preselected G-loading force.

Claim 15

Dependent Claim 85 words

The ejection seat assembly of claim 13 wherein said control means controls operation of said power means to adjust the angular position of said cradle upper portion as a hysteretic function dependent on the value of the greater of said sensed G-loading or said anticipated G-loading, said function providing an offset between the maximum G-loading necessary to cause said cradle upper portion to be in said reclined position and the maximum G-loading which will cause said cradle upper portion to move toward said upright position.

Claim 16

Dependent Claim 44 words

The ejection seat assembly of claim 14 wherein said hysteretic function has a slope to provide continuous angular adjustment of said cradle upper portion at angular positions between said upright and reclined positions as said cradle upper portion is moved toward said reclined position.

Claim 17

Dependent Claim 31 words

The ejection seat assembly of claim 12 wherein said control means further includes anticipatory means for anticipating aircraft G-force related performance and controlling operation of said power means in response thereto.

Claim 18

Dependent Claim 19 words

The ejection seat assembly of claim 16 wherein said anticipatory means is responsive to sensed aircraft G-force related parameters.

Claim 19

Dependent Claim 66 words

The ejection seat assembly of claim 12 further including: first sensor means for sensing G-loading at the cockpit and generating a sensed aircraft G-loading signal in response thereto; means for determining selected sensed anticipatory aircraft parameters and generating an anticipatory G-loading signal in response thereto; and control means for controlling operation of said power means in response to said G-loading signal and said anticipatory G-loading signal.

Claim 20

Dependent Claim 220 words

A G-protective ejection seat assembly for an occupant of the cockpit of an aircraft, comprising: a non-articulated, rigid ejection seat cradle, said cradle having control support means for supporting hand flight controls of the aircraft for movement with said cradle; means attachable to the aircraft for supporting said cradle for selective angular movement within the cockpit between an upright position and a reclined position, said cradle being selectively positionable during use in said upright and reclined positions; a separable, non-articulated ejection seat releasably carried by and substantially stationary with respect to said cradle during non-ejection use, said seat being moveable with said cradle as said cradle moves between said upright and reclined positions, said seat supporting the occupant in a normally upright position when said cradle is in said upright position and in a supine position when said cradle is in said reclined position, said ejection seat being movable upon ejection independent of said cradle and the hand flight controls supported by said cradle, said ejection seat including propulsion means for separating said ejection seat from said cradle and propelling said seat with the occupant therein free of the cockpit during ejection with said cradle and the hand controls remaining in place within the aircraft; and power means for selectively angularly moving said cradle between said upright and reclined positions.

Claim 21

Dependent Claim 220 words

A G-protective ejection seat assembly for an occupant of the cockpit of an aircraft, comprising: a non-articulated, rigid ejection seat cradle, said cradle having control support means for supporting hand flight controls of the aircraft for movement with said cradle; means attachable to the aircraft for supporting said cradle for selective angular movement within the cockpit between an upright position and a reclined position, said cradle being selectively positionable during use in said upright and reclined positions; a separable, non-articulated ejection seat releasably carried by and substantially stationary with respect to said cradle during non-ejection use, said seat being moveable with said cradle as said cradle moves between said upright and reclined positions, said seat supporting the occupant in a normally upright position when said cradle is in said upright position and in a supine position when said cradle is in said reclined position, said ejection seat being movable upon ejection independent of said cradle and the hand flight controls supported by said cradle, said ejection seat including propulsion means for separating said ejection seat from said cradle and propelling said seat with the occupant therein free of the cockpit during ejection with said cradle and the hand controls remaining in place within the aircraft; and power means for selectively angularly moving said cradle between said upright and reclined positions.

Claim 22

Dependent Claim 66 words

The ejection seat assembly of claim 19 further including leg supports movably attached to said cradle and having control support means for supporting foot flight controls of the aircraft for movement with the leg supports, and further including means for moving said leg supports between a lowered position and a raised position in response to movement of said cradle between said upright and reclined positions, respectively.

Claim 23

Dependent Claim 31 words

The ejection seat assembly of claim 20 wherein said leg supports include a pair of spaced apart leg rests each separately pivoted to said cradle upper portion and to the aircraft.

Claim 24

Dependent Claim 24 words

The ejection seat assembly of claim 19 wherein said cradle is positionable in a plurality of angular positions between said upright and reclined positions.

Claim 25

Dependent Claim 31 words

The ejection seat assembly of claim 19 further including means for adjustably moving said ejection seat relative to said cradle to move the occupant to the design eyepoint of the aircraft.

Claim 26

Dependent Claim 27 words

The ejection seat assembly of claim 19 further including control means for controlling operation of said power means in response to sensed aircraft G-loading and anticipated G-loading.

Claim 27

Dependent Claim 39 words

The ejection seat assembly of claim 24 wherein said control means causes said power means to recline said cradle from said upright position when the greater of said sensed G-loading or said anticipated G-loading exceeds a preselected G-loading force.

Claim 28

Dependent Claim 79 words

The ejection seat assembly of claim 25 wherein said control means controls operation of said power means to adjust the angular position of said cradle as a hysteretic function dependent on the value of the greater of said sensed G-loading or said anticipated G-loading, said function providing an offset between the maximum G-loading necessary to cause said cradle to be in said reclined position and the maximum G-loading which will cause said cradle to move toward said upright position.

Claim 29

Dependent Claim 40 words

The ejection seat assembly of claim 26 wherein said hysteretic function has a slope to provide continuous angular adjustment of said cradle at angular positions between said upright and reclined positions as said cradle is moved toward said reclined position.

Claim 30

Dependent Claim 31 words

The ejection seat assembly of claim 24 wherein said control means further includes anticipatory means for anticipating aircraft G-force related performance and controlling operation of said power means in response thereto.

Claim 31

Dependent Claim 19 words

The ejection seat assembly of claim 28 wherein said anticipatory means is responsive to sensed aircraft G-force related parameters.

Claim 32

Dependent Claim 68 words

A G-protective ejection seat assembly for an occupant of an aircraft comprising: an ejection seat attachable to the aircraft for selective angular movement with the aircraft between an upright position and a reclined position; power means for selectively angularly moving said ejection seat between said upright and reclined positions; and control means for controlling operation of said power means in response to sensed aircraft G-loading and anticipated G-loading.

Claim 33

Dependent Claim 68 words

A G-protective ejection seat assembly for an occupant of an aircraft comprising: an ejection seat attachable to the aircraft for selective angular movement with the aircraft between an upright position and a reclined position; power means for selectively angularly moving said ejection seat between said upright and reclined positions; and control means for controlling operation of said power means in response to sensed aircraft G-loading and anticipated G-loading.

Claim 34

Dependent Claim 47 words

The ejection seat assembly of claim 30 wherein said control means is responsive to G-loading, said control means causes said power means to recline said ejection seat from said upright position when the greater of said sensed G-loading or said anticipated G-loading exceeds a preselected G-loading force.

Claim 35

Dependent Claim 82 words

The ejection seat assembly of claim 31 wherein said control means controls operation of said power means to adjust the angular position of said ejection seat as a hysteretic function dependent on the value of the greater of said sensed G-loading or said anticipated G-loading, said function providing an offset between the maximum G-loading necessary to cause said ejection seat to be in said reclined position and the maximum G-loading which will cause said ejection seat to move toward said upright position.

Claim 36

Dependent Claim 42 words

The ejection seat assembly of claim 32 wherein said hysteretic function has a slope to provide continuous angular adjustment of said ejection seat at angular positions between said upright and reclined positions as said ejection seat is moved toward said reclined position.

Annuity Stage	Window Opens	Payment Deadline	Surcharge Period Until	Estimated Fee	Status
3.5 Years (Year 4)	1991-11-29	1992-05-30	1992-11-29	$2000.00	Window Closed / Lapsed
7.5 Years (Year 8)	1995-11-29	1996-05-30	1996-11-29	$3760.00	Window Closed / Lapsed
11.5 Years (Year 12)	1999-11-29	2000-05-30	2000-11-29	$7700.00	Window Closed / Lapsed

Automatic multi-position G-protective ejection seat assembly

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