Towplate units for aerial cargo delivery and assemblies including the same

Patent metadata

Field	Value
Publication number	US-11987358-B2
Application number	US-202217719999-A
Country	US
Kind code	B2
Filing date	Apr 13, 2022
Priority date	Apr 13, 2022
Publication date	May 21, 2024
Grant date	May 21, 2024

Abstract

Towplate units and assemblies are disclosed for airborne extraction of a cargo load. The towplate unit includes an extraction and jettison links having a pair of spaced-apart parallel extraction and jettison link arms and an extraction and jettison cross-connector extending between and rigidly joining the extraction and jettison link arms, respectively. A locking system removably locks the jettison link to the extraction link to thereby allow the jettison link to be removed from the extraction link when unlocked. A towplate assembly is also provided which includes a towplate unit removably assembled with a deck plate and an actuator control assembly operatively interconnected to the towplate unit so as to cause the towplate unit to separate from the deck plate during a normal cargo deployment condition or to cause the jettison link to separate from the extraction link of the towplate unit during an aborted cargo deployment condition.

First claim

What is claimed is:

1. A towplate unit to assist in aerial extraction of a cargo load from an airborne aircraft, the towplate unit comprising:
an extraction link which includes a pair of spaced-apart parallel extraction link arms and an extraction cross-connector extending between and rigidly joining the extraction link arms, the extraction cross-connector being adapted for connection with a cargo extraction line attached to a cargo load to be extracted from the airborne aircraft;
a jettison link which includes a pair of spaced-apart parallel jettison link arms each nested within a respective one of the extraction link arms, and a jettison cross-connector extending between and rigidly joining the jettison link arms rearwardly of the extraction cross-connector, the jettison cross-connector being adapted for connection with a drogue parachute line associated with a drogue parachute being towed by the airborne aircraft; and
a locking system adapted to removably lock the jettison link to the extraction link and to allow the jettison link to be removed from the extraction link when unlocked, wherein the locking system comprises:
(i) at least one locking link pivotally connected to a respective jettison link arm; and
(ii) at least one locking pin rigidly associated with a respective extraction link arm, wherein

the at least one locking link is pivotally moveable between a locked condition such that the at least one locking link is lockably engaged with the at least one locking pin so that the extraction and jettison links are connected to one another, and an unlocked condition such that the at least one locking link is disengaged with the at least one locking pin to thereby allow separation of the jettison link from the extraction link.

2. The towplate unit according to claim 1 , wherein
the extraction link arms include an aft-facing end which defines an inner convexly conically curved surface, and wherein
the jettison link arms include an aft facing end which defines an outer concavely conically curved surface which is engaged with the inner convexly conically curved surface of a respective one of the jettison link arms.

3. The towplate unit according to claim 2 , wherein the aft-facing end of the extraction link arms further defines an outer concavely curved surface.

4. The towplate unit according to claim 1 , wherein the locking system comprises:
(i) a pair of locking links each pivotally connected to a respective one of the jettison link arms; and
(ii) a pair of locking pins each being rigidly associated with a respective one of the extraction link arms, wherein
each locking link is pivotally moveable between the locked condition such that the locking link is lockably engaged with a respective one of the locking pins so that the extraction and jettison links are connected to one another, and the unlocked condition such that each the locking link is disengaged with the respective one of the locking pins to thereby allow separation of the jettison link from the extraction link.

5. The towplate unit according to claim 4 , wherein
each of the jettison link arms includes an indicator window, and wherein
each of the locking links includes an indicator boss extending into a respective one of the indicator windows so as to provide a visual verification that the locking link is in the locked condition thereof.

6. The towplate unit according to claim 1 , wherein
the at least one locking link includes a J-shaped hook latch end lockably engaged with the at least one locking pin, and wherein
the locking system further comprises a spring element for exerting a bias force on the J-shaped hook latch end in a direction to pivot the J-shaped hook latch end into the engaged position thereof with the locking pin.

7. The towplate unit according to claim 6 , wherein the spring element is a torsion spring.

8. The towplate unit according to claim 1 , wherein
at least one of the jettison link arms includes an indicator window, and wherein
the at least one locking link includes an indicator boss extending into the indicator window of the at least one of the jettison link arms so as to provide a visual verification that the at least one locking link is in the locked condition thereof.

9. The towplate unit according to claim 1 , wherein the extraction link arms include forwardly protruding latch surfaces.

10. A towplate assembly for aerial extraction of cargo from an airborne aircraft comprising:
a deck plate adapted to being immovably mounted to a cargo deck of the aircraft;
the towplate unit according to claim 1 operatively associated with the deck plate;
an actuator control assembly removably locking the towplate unit to the deck plate, wherein the actuator control assembly is interconnected to the towplate unit so as to be operatively movable between (i) a cargo extraction state which causes the towplate unit to separate from the deck plate during a normal cargo deployment condition or (ii) a jettison state wherein the at least one locking link is pivotally moved from the locked condition and into the unlocked condition thereof to thereby cause the jettison link to separate from the extraction link of the towplate unit.

11. The towplate assembly according to claim 10 , wherein the actuator control system comprises:
an actuator cylinder which includes an actuator shaft that is reciprocally rectilinearly moveable from an intermediate position and into retracted and extended positions;
a bell crank operatively connected to a terminal end of the actuator shaft so as to be pivotally moveable between a towplate unit release position and a jettison link release position in response to movement of the actuator shaft between its retracted and extended positions, respectively;
a pivotal extraction link trigger operatively engaged with the extraction link of the towplate unit so as to removably lock the towplate unit to the deck plate; and
a jettison link trigger adapted to being pivotally moved into contact with the locking system associated with the jettison link of the towplate unit to unlock the jettison link from the extraction link, wherein
movement of the actuator shaft into the retracted position responsively causes the bell crank to pivot into the towplate unit release position and engage with the extraction link trigger so as to pivotally move the extraction link trigger to unlock the towplate unit from the deck plate and thereby allow the towplate unit to be separated therefrom, and wherein
movement of the actuator shaft into the extended position responsively caused the bell crank to pivot into the jettison link release position and engage with the jettison link trigger so as to pivotally move the jettison link trigger into contact with the locking system to thereby unlock the jettison link from the extraction link to allow the jettison link to be separated therefrom.

12. The towplate assembly according to claim 11 , wherein the extraction link trigger includes:
an extraction trigger link shaft for mounting the extraction link trigger for pivotal movements between engaged and disengaged positions relative to the extraction link, and
a torsion spring operatively associated with the trigger link shaft for exerting a bias force to move the extraction link trigger into the engaged position thereof.

13. The towplate assembly according to claim 12 , wherein
the extraction trigger link shaft includes a handle to allow manual rotation of the trigger link shaft and thereby cause the extraction trigger link to be manually pivoted between the engaged and disengaged positions thereof, and wherein
the deck plate includes an access window to allow manual ac

Assignees

• Embraer Sa

Inventors

• De Souza Heron Medeiros
• Trisotto Saint Clair
• Goncalves Marcos Antônio Batista
• Borges Guilherme Augusto Garcia
• Santos Vinicius Mira
• Allert Torben

Classifications

• B64D1/12 Primary

  Releasing · CPC title

• B64D17/38

  Releasable fastening devices between parachute and load or pack · CPC title

• B64D1/10 Primary

  Stowage arrangements for the devices in aircraft · CPC title