Patent US3930628A successfully refreshed from Google Patents.
US3930628A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Depoly/release system
Assignee: National Aeronautics and Space Administration
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Filing: 1974-11-27
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Granted: 1976-01-06
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Expires: 1994-11-27
Abstract
Abstract An apparatus is disclosed for arresting uncontrollable motions of model araft. A signal is used to deploy a parachute when a model aircraft is in a motion, such as a tailspin, from which the operator cannot recover by manipulating the flight surfaces. After the model aircraft has been stabilized to a point where the operator can arrest the uncontrollable motion the parachute is jettisoned and normal flight resumed. The deploy and jettison signals may be sent using a single channel of a multi-channel transmitter and are completely independent of each other.
Inventors
- 👤 David B. Robelen
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-07 10:03
CPC Classifications
B; B64; B64D; B64D17/00; B64D17/80
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
178 words
Apparatus for arresting uncontrollable motions of a model aircraft comprising in combination: a model aircraft; a parachute having shrouds connected to one end of a riser; said riser having a closed loop at the other end thereof; a platform firmly attached to said model aircraft for supporting said parachute during normal aircraft flight; and parachute being releasably held in a suitably folded position on said platform by an elastic band having one end thereof securely fastened to said platform and having a metal loop at the other end thereof; said metal loop being releasably fastened to said platform by a release pin; a frame means for firmly attaching said platform to said aircraft; said frame means having a plunger slidably mounted thereon; said plunger being inserted through said loop of said riser for holding said parachute after said parachute has been deployed; a deploy means for releasing said release pin in response to a deploy signal thereby deploying said parachute; and jettison means for slidably moving said plunger in response to a jettison signal thereby jettisoning said parachute.
Claim 2
Dependent Claim
178 words
Apparatus for arresting uncontrollable motions of a model aircraft comprising in combination: a model aircraft; a parachute having shrouds connected to one end of a riser; said riser having a closed loop at the other end thereof; a platform firmly attached to said model aircraft for supporting said parachute during normal aircraft flight; and parachute being releasably held in a suitably folded position on said platform by an elastic band having one end thereof securely fastened to said platform and having a metal loop at the other end thereof; said metal loop being releasably fastened to said platform by a release pin; a frame means for firmly attaching said platform to said aircraft; said frame means having a plunger slidably mounted thereon; said plunger being inserted through said loop of said riser for holding said parachute after said parachute has been deployed; a deploy means for releasing said release pin in response to a deploy signal thereby deploying said parachute; and jettison means for slidably moving said plunger in response to a jettison signal thereby jettisoning said parachute.
Claim 3
Dependent Claim
85 words
An apparatus as set forth in claim 1 wherein said stowing means includes: a platform for supporting said parachute during normal aircraft flight; said parachute being suitably folded and placed on said platform; an elastic band having one end thereof rigidly secured to said platform and the other end thereof secured to a metal loop; said elastic band being stretched over said parachute and said metal loop being releasably connected to said platform thereby securely holding said parachute against said platform during normal aircraft flight.
Claim 4
Dependent Claim
99 words
An apparatus as set forth in claim 2 wherein said deploy means includes two eyelets rigidly fastened to said platform; a release pin for holding said elastic band across said parachute; said elastic band being stretched over said parachute and said metal loop being received between said eyelets and releasably held therein by said release pin, said release pin being slidably positioned through said eyelets and said metal loop; said release pin being slidably removable from said eyelets and said metal loop in response to said deploy signal thereby releasing said elastic band and permitting said parachute to deploy.
Claim 5
Dependent Claim
41 words
An apparatus as set forth in claim 3 wherein said deploy means includes a tension means for applying a rearward acting tensile force to said release pin to thereby maintain said release pin positioned through said eyelets and said metal loop.
Claim 6
Dependent Claim
76 words
An apparatus as set forth in claim 1 wherein said jettison means includes a plunger slidably mounted on said frame means for holding said parachute after said parachute has been deployed; said plunger being inserted through said closed loop of said riser; and spring means for initially maintaining said plunger in position; said jettison signal serving to slidably move said plunger to thereby remove said plunger from said closed loop and cause jettisoning of said parachute.
Claim 7
Dependent Claim
30 words
An apparatus as set forth in claim 1 wherein said deploy means and said jettison means are operated by a linkage means in response to said deploy and jettison signals.
Claim 8
Dependent Claim
149 words
An apparatus as set forth in claim 1 wherein said deploy means and said jettison means are actuated by a linkage means comprising: a single radio channel; a radio receiver rigidly mounted in said aircraft for receiving said deploy and jettison signals; a single digital proportional servo rigidly mounted in said aircraft for releasing said release pin and for slidably moving said plunger; said digital proportional servo communicating with said deploy means by way of a deploy cable having one end thereof attached to said servo and the other end thereof attached to said release pin; said digital proportional servo also communicating with said jettison means by way of a jettison cable having one end thereof attached to said servo and the other end thereof attached to said plunger; and power source rigidly mounted in said aircraft for supplying power to said radio receiver and said digital proportional servo.
Claim 9
Dependent Claim
17 words
An apparatus as set forth in claim 7 wherein said receiver means receives remotely transmitted radio signals.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1979-01-05 | 1979-07-07 | 1980-01-06 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1983-01-05 | 1983-07-07 | 1984-01-06 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1987-01-05 | 1987-07-07 | 1988-01-06 | $7700.00 | Window Closed / Lapsed |