Nose landing gear jump strut assembly

Claim 2

A jump strut assembly which is extendable on command for rotating the nose of an airplane upwardly during the take-off ground run comprising a main housing cylinder adapted to be affixed to the nose of the airplane, a jump cylinder axially movable within said main housing cylinder between a retracted position and an extended position relative to said main housing cylinder, lock means for releasably locking said jump cylinder against extension when in the retracted position, lock release means for releasing said lock means, fluid pressure means acting on said jump cylinder for moving said jump cylinder to the extended postion upon release of said lock means, a main strut piston axially movable within said jump cylinder, and means for preventing relative movement between said main strut piston and jump cylinder during movement of said jump cylinder to the extended position.

Claim 3

The assembly of claim 1 further comprising means for permitting relative movement of said main strut piston within said jump cylinder when said jump cylinder is in the retracted position.

Claim 4

The assembly of claim 2 wherein said main strut piston defines with said jump cylinder upper and lower piston chambers, and said means for permitting relative movement of said main strut piston within said jump cylinder comprises orifice means permitting restricted flow between said piston chambers during relative movement of said main strut piston within said jump cylinder.

Claim 5

The assembly of claim 3 wherein said means for preventing relative movement between said main strut piston and jump cylinder during extension of said jump cylinder comprises a support tube assembly axially slidably received in said jump strut piston, said support tube assembly comprising an outer tube fixed with respect to said jump cylinder for movement therewith, and an inner tube axially movable with respect to said outer tube for respectively closing and opening flow holes through said tubes through which the fluid flow through said orifice means must pass, and means for causing relative movement between said inner and outer tubes to block the flow holes therethrough for hydraulically locking said main strut piston against movement relative to said jump cylinder during extension of said jump cylinder.

Claim 6

The assembly of claim 4 wherein said last-mentioned means comprises spring means biasing said inner tube to a position blocking said flow holes.

Claim 7

The assembly of claim 5 further comprising means for overcoming the bias of said spring means to unblock said flow holes through said support tubes when said jump cylinder is in its fully retracted position.

Claim 8

The assembly of claim 6 wherein said means for overcoming the bias of said spring means comprises stop pin means affixed to said inner tube and engageable with a stop surface on said main housing cylinder to overcome the bias of said spring means when said jump cylinder is in the retracted position.

Claim 9

The assembly of claim 1 wherein said lock means comprises an expandable split lock ring, and means for expanding said lock ring radially outwardly into engagement with an internal shoulder in said main housing cylinder to lock said jump cylinder against extension relative to said main housing cylinder when said jump cylinder is in the retracted position.

Claim 10

The assembly of claim 8 wherein said means for expanding said lock ring comprises an annular trigger member mounted for axial movement relative to said lock ring, and a series of lock links having radial inner and outer edges captivated in respective annular grooves in said lock ring and trigger member, said trigger member being axially movable between a first position in which said lock links extend substantially radially between said lock ring and trigger member to expand said lock ring against said internal shoulder and a second position in which the radial inner edges of said lock links are moved to an overcenter position which allows said lock ring to contract so that said lock ring no longer engages said internal shoulder.

Claim 11

The assembly of claim 9 further comprising spring means for biasing said trigger member toward said first position.

Claim 12

The assembly of claim 10 further comprising an unlock piston which is movable upon command in a direction causing movement of said trigger member to said second position.

Claim 13

The assembly of claim 11 further comprising a manifold attached to said main housing cylinder for supplying hydraulic fluid to move said unlock piston in such direction causing movement of said trigger member to said second position.

Claim 14

The assembly of claim 1 wherein said fluid pressure means comprises a jump chamber within said main housing cylinder which is adapted to be charged with a high pressure gas that acts on said jump cylinder causing said jump cylinder to move to the extended position upon release of said lock means.

Claim 15

The assembly of claim 1 further comprising means for permitting said main strut piston to extend relative to said jump cylinder after said jump cylinder has been fully extended and there is no retracting load acting on said main strut piston.

Claim 16

The assembly of claim 14 wherein said main strut piston defines with said jump cylinder upper and lower piston chambers, and orifice means permit restricted flow between said piston chambers during relative movement of said main strut piston within said jump cylinder, said means for preventing relative movement between said main strut piston and jump cylinder comprising a support tube assembly axially slidably received in said main strut piston, said support tube assembly comprising an outer tube fixed with respect to said jump cylinder for movement therewith, and an inner tube axially movable with respect to said outer tube for respectively closing and opening flow holes through said tubes through which the fluid flow through said orifice means must pass, and means for causing relative movement between said inner and outer tubes to block said flow holes for hydraulically locking said main strut piston against movement relative to said jump cylinder during extension of said jump cylinder, said means for permitting said main strut piston to extend comprising additional flow holes through said tubes, and flapper valve means for blocking fluid flow through said additional flow holes from said lower piston chamber to said upper piston chamber while permitting fluid flow through said additional flow holes from said upper piston chamber to said lower piston chamber whenever the pressure in said lower piston chamber is less than the pressure in said upper piston chamber.

Claim 17

The assembly of claim 14 further comprising means for retracting said jump cylinder within said main housing cylinder after said main strut piston has been extended relative to said jump cylinder.

Claim 18

The assembly of claim 16 wherein said means for retracting said jump cylinder comprises valve means for venting said fluid pressure means, and means for applying a retract force to said jump cylinder.

Claim 19

The assembly of claim 17 wherein said fluid pressure means comprises a jump chamber within said main housing cylinder which is charged with a high pressure gas that acts on said jump cylinder to extend said jump cylinder upon release of said lock means, and said valve means is operative to vent said jump chamber to the atmosphere on command.

Claim 20

The assembly of claim 18 further comprising a recoil chamber within said main housing cylinder which is pressurized to apply a force on said jump cylinder urging said jump cylinder toward the retracted position.

Claim 21

The assembly of claim 19 further comprising accumulator means containing pressurized gas, and valve means for connecting said accumulator means to said recoil chamber upon venting of said jump chamber to pressurize said recoil chamber to cause said jump cylinder to retract.

Claim 22

The assembly of claim 19 further comprising accumulator means containing pressurized gas which is continuously connected to said recoil chamber whereby there is a build-up of pressure in said accumulator means during extension of said jump cylinder which causes said jump cylinder to retract upon venting said jump chamber.

Claim 23

The assembly of claim 1 wherein said main strut piston defines with said jump cylinder upper and lower piston chambers, and orifice means provide restricted flow between said piston chambers during relative movement of said main strut piston within said jump cylinder, and bypass means provide for additional flow from said lower piston chamber to said upper piston chamber whenever said jump strut assembly engages a bump during movement of the airplane along the ground except during extension of said jump cylinder.

Claim 24

The assembly of claim 22 wherein said bypass means comprises a bypass passage around said orifice means, a bypass sleeve axially movable with respect to said bypass passage between open and closed positions for respectively opening and closing said bypass passage, spring means for biasing said bypass sleeve toward the open position, and means for retaining said bypass sleeve in the closed position until after landing has taken place.

Claim 25

The assembly of claim 23 further comprising a support tube axially slidably received in said main strut piston, said support tube being fixed with respect to said jump cylinder for movement therewith, said orifice means being formed by a metering pin fixed with respect to said main strut piston for movement therewith, and an opening in said support tube through which said metering pin extends, said bypass passage extending through said support tube around said orifice means, and said bypass sleeve being axially slidable within said support tube for respectively opening and closing said bypass passage.

Claim 26

The assembly of claim 24 wherein said means for retaining said bypass sleeve in the closed position comprises a stop member on said metering pin engageable with said bypass sleeve to move said bypass sleeve to the closed position when said main strut piston is substantially fully extended relative to said jump cylinder.

Claim 27

The assembly of claim 25 wherein said means for retaining said bypass sleeve in the closed position further comprises slot means in said bypass sleeve, and pin means on said support tube movable into engagement with said slot means to retain said bypass sleeve in the closed position.

Claim 28

The assembly of claim 26 further comprising means responsive to a relatively high pressure within said lower piston chamber which occurs during landing of the aircraft for moving said pin means into engagement with said slot means to retain said bypass sleeve in the closed position.

Claim 29

The assembly of claim 27 further comprising means for moving said pin means out of engagement with said slot means in response to a substantial drop in the pressure in said lower piston chamber which occurs after landing has taken place.

Claim 30

The assembly of claim 28 wherein said means for moving said pin means into engagement with said slot means comprises an external surface on said pin means exposed to the fluid pressure in said lower piston chamber, and said means for moving said pin means out of engagement with said slot means comprises leaf spring means providing a biasing force urging said pin means out of engagement with said slot means.

Claim 31

The assembly of claim 24 further comprising flapper valve means for permitting unobstructed flow through said bypass passage when said bypass sleeve is in the open position during retraction of said main strut piston within said jump cylinder and for blocking return flow through said bypass passage during extension of said main strut piston relative to said jump cylinder.

Claim 32

The assembly of claim 30 further comprising a delivery tube concentrically mounted within said support tube, said delivery tube containing said opening for said metering pin, and said flapper valve means being mounted for limited axial movement into and out of engagement with one end of said delivery tube to respectively block and permit fluid flow through said bypass passage while said bypass sleeve is in the open position.

Claim 33

The assembly of claim 31 wherein said flapper valve means includes flow slots for flow of fluid through said flapper valve means when said flapper valve means has moved out of engagement with said delivery tube.

Claim 34

A jump strut assembly which is extendable on command for rotating the nose of an airplane upwardly during the take-off ground run comprising a main housing cylinder, a jump cylinder axially movable within said main housing cylinder, lock means for releasably locking said jump cylinder against extension when in a retracted position within said main housing cylinder, lock release means for releasing said lock means, means for moving said jump cylinder to an extended position relative to said main strut piston upon release of said lock means, a main strut piston axially movable within said jump cylinder to dissipate energy, and means for locking said jump strut against movement relative to said jump cylinder only during extension of said jump cylinder.

Claim 35

A jump strut assembly which is extendable on command for rotating the nose of an airplane upwardly during the take-off ground run comprising a main housing cylinder, a jump cylinder axially movable within said main housing cylinder, lock means for releasably locking said jump cylinder against extension when in a retracted position within said main housing cylinder, lock release means for releasing said lock means, means for moving said jump cylinder to an extended position relative to said main strut piston upon release of said lock means, a main strut piston axially movable within said jump cylinder to dissipate energy, and means for locking said jump strut against movement relative to said jump cylinder only during extension of said jump cylinder.

Claim 36

The assembly of claim 33 further comprising means for permitting said main strut piston to extend relative to said jump cylinder after such extension of said jump cylinder.

Claim 37

The assembly of claim 34 further comprising means for retracting said jump cylinder within said main housing cylinder following extension of said main strut piston relative to said jump cylinder.

Claim 38

The assembly of claim 35 wherein said means for moving said jump cylinder to an extended position comprises a jump chamber within said main housing cylinder which is chargeable with a high pressure gas that acts on said jump cylinder causing said jump cylinder to extend upon release of said lock means, and said means for retracting said jump cylinder comprises vent means for venting said jump chamber on command, and means for applying a retract force to said jump cylinder.

Claim 39

The assembly of claim 36 wherein said means for applying a retract force to said jump cylinder comprises an accumulator containing pressurized gas, a recoil chamber within said main housing cylinder which when pressurized applies a retraction force to said jump cylinder, and means providing fluid communication between said accumulator and recoil chamber for pressurizing said recoil chamber.