US3936019A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Ejector release unit for use in aircraft
Assignee: ML Aviation Ltd
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Filing: 1974-02-19
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Granted: 1976-02-03
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Expires: 1994-02-19
Abstract
Abstract This invention is concerned with an ejection release unit for releasing and projecting a store from an aircraft. The unit comprises a releasable latching mechanism for supporting the store, a pair of telescopic ejection guns for projecting the store from the aircraft, a breech for one or more cartridges which, on ignition, produce pressure gas which causes the latching mechanism to release the store and also acts on a piston which indirectly transmits the resultant force to a body of hydraulic fluid, which, in its turn, operates the ejection gun at each side. Preferably, there are two oppositely acting pistons, each of which pistons transmits pressure to a separate body of hydraulic fluid for operating a respective ejection gun. The breeches may be formed in a removable unit which also defines the cylinders within which the pistons work.
Inventors
- 👤 Samuel W. Craigie
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 23:20
CPC Classifications
B; B64; B64D; B64D1/00; B64D1/02; B64D1/04; B64D1/06
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
136 words
In an ejector release unit for releasing and projecting a store from an aircraft, a latching mechanism for projecting and releasing said store; a pair of ejection guns for projecting said store from said aircraft; a breech and firing contact for at least one cartridge, ignition of said at least one cartridge producing pressure gas; the improvement comprising a cylinder and a piston mounted for reciprocatory movement within said cylinder, said cylinder being connected to said breech; and a chamber having fluid connections to each said ejection gun, a body of hydraulic fluid being contained within said chamber; and means capable of operation by said piston when said gas acts thereon to transmit the resultant force to said body of fluid whereby said fluid is caused to flow through said connections to operate said ejection guns.
Claim 2
Dependent Claim
136 words
In an ejector release unit for releasing and projecting a store from an aircraft, a latching mechanism for projecting and releasing said store; a pair of ejection guns for projecting said store from said aircraft; a breech and firing contact for at least one cartridge, ignition of said at least one cartridge producing pressure gas; the improvement comprising a cylinder and a piston mounted for reciprocatory movement within said cylinder, said cylinder being connected to said breech; and a chamber having fluid connections to each said ejection gun, a body of hydraulic fluid being contained within said chamber; and means capable of operation by said piston when said gas acts thereon to transmit the resultant force to said body of fluid whereby said fluid is caused to flow through said connections to operate said ejection guns.
Claim 3
Dependent Claim
35 words
An ejection release unit according to claim 1, in which there are two oppositely acting pistons, each of which pistons transmits pressure to a separate body of hydraulic fluid for operating a respective ejection gun.
Claim 4
Dependent Claim
28 words
An ejection release unit according to claim 2, in which the breeches are formed in a removable unit which also defines the cylinders within which the pistons work.
Claim 5
Dependent Claim
31 words
An ejection release unit according to claim 3, in which the removable unit is arranged to terminate at each side along a line defined by the end face of each piston.
Claim 6
Dependent Claim
29 words
An ejection release unit according to claim 1, in which throttling devices are fitted in order to regulate the pressure of the hydraulic fluid for operating the ejection guns.
Claim 7
Dependent Claim
151 words
An ejection release unit according to claim 1, in which a spring loaded piston is fitted, the piston being located in a short extension of the unit, the extension defining a cylinder within which the piston slides and a compression spring being mounted between the rear of the piston and the end of the extension to force the piston inwardly to compensate for any small leakage of hydraulic fluid and to yield in the event of expansion due to rise of temperature, there being a small passage extending from the extension to a point just beyond the free end of the piston so that prior to firing, hydraulic fluid can flow freely along this passage in either direction, but immediately after firing movement of the piston closes the end of the passage so that fluid in the extension is automatically shut off from the sudden rise in pressure in the fluid.
References Cited (Backward Citations)
US3610094A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1979-02-02 | 1979-08-04 | 1980-02-03 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1983-02-02 | 1983-08-04 | 1984-02-03 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1987-02-02 | 1987-08-04 | 1988-02-03 | $7700.00 | Window Closed / Lapsed |