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US 4,088,287 AGranted
Dual-purpose ejector for aircraft load jettisoning mechanism
AssigneeR. Alkan & Cie
InventorsJean H. Hasquenoph, Pierre F. Coutin
Life of this patent
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Abstract
In a telescopic retractable ejector, the driving gas is allowed to flow freely with the maximum efficiency by compensating the pressure drop resulting from the gas expansion during the piston extension with a concomitant and automatic increment in the surface area of the pistons which is exposed to the gas pressure.
Claims8
A telescopic retractable ejector, for ejecting a load from an aircraft by gas thrust, comprising:
- (i) a cylinder body
- (ii) inlet means for feeding said cylinder body with gas under pressure
- (iii) an outer ejection piston slidably mounted within said cylinder body,
- (iv) an inner ejection piston telescopically slidable within said outer ejection piston
- (v) means located between said inner and outer pistons for releasably interconnecting said outer and inner ejection pistons during an extension stroke of the outer piston, said means automatically allowing the disconnection of said pistons at the end of the extension stroke of the outer piston to permit an extension stroke of the inner piston relative to the outer piston,
- (vi) means defining a gas storage chamber connected through a non-return valve to said inlet means for storing gas received therefrom under maximum pressure,
- (vii) means defining a path of flow from said inlet means for applying gases under maximum pressure against a reduced surface area of an inner part of the inner ejection piston to ensure a simultaneous extension stroke of the two ejection pistons together, a connection being provided between the inner part of the inner ejection piston and the inner space of the cylinder body, said connection being operative only at the end of the extension stroke of the outer ejection piston to apply gas under reduced pressure to an upper outer flange of the inner piston to cause said inner piston to extend at a speed similar to the extension speed of the outer piston,
- (viii) a spool valve on said inner piston for automatically venting to the atmosphere, at the end of the extension stroke of the inner piston, residual ejection gases remaining within the inner piston,
- (ix) means defining a passage automatically connecting said gas storage chamber to a chamber located between a wall of the outer piston and a wall of the cylinder body, when said spool valve vents to the atmosphere the inner space of the inner piston, to apply stored gas under maximum pressure under a head portion of said outer piston to return said outer piston to a retracted position, said outer ejection piston having an opening for connecting automatically, at the end of the retraction stroke of the outer piston, said chamber located between the walls of the outer piston and the cylinder body to a chamber located between a wall of the inner piston and said wall of the outer piston, to apply gas under maximum pressure under a head portion of said inner piston to return said inner piston to a retracted position.
6 more elements
A telescopic retractable ejector for ejecting a load from an aircraft by gas thrust, comprising:
- (i) a cylinder body
- (ii) inlet means for feeding gas under pressure to said cylinder body,
- (iii) an outer ejection piston slidably mounted within said cylinder body,
- (iv) an inner ejection piston telescopically mounted within said outer ejection piston,
- (v) means defining a gas storage chamber within said cylinder body connected through a non-return valve to said inlet means, for storing gas under maximum pressure, a connection being provided between said storage chamber and annular chambers located between a wall of the cylinder body and a wall of the outer piston and between a wall of the inner piston and said wall of said outer piston to provide said annular chambers with gas under maximum pressure,
- (vi) a head portion of said outer piston having an upper face of greatest surface area to which is applied the gas pressure from the inlet means and an opposite lower face of reduced surface area submitted to gas under maximum pressure from the storage chamber to reduce the outer piston extension speed,
- (vii) a head portion of said inner piston having an upper face of greatest area to which is applied the gas pressure from the inlet means and an opposite lower face of reduced surface area submitted to gas under maximum pressure from the storage chamber to reduce the inner piston extension speed,
- (viii) means providing a connection, between the inlet means and an inner part of the inner piston, operative at the end of an extension stroke of the outer and inner pistons together, to apply gas under reduced pressure to an inner surface area of the inner piston for allowing said inner piston to perform a further extension stroke at a speed similar to its speed of extension together with the outer piston,
- (ix) a spool valve on said inner piston for automatically venting to the atmosphere, at the end of the further extension stroke, residual ejection gases remaining within the inner piston, an automatic retraction of the outer piston and then of the inner piston being successively obtained by said connection, by the storage chamber, and by the annular chambers.
6 more elements
Dependencies are inferred from the claim text.