IP Library Granted Patent US 10,914,551
Granted Patent B2
US 10,914,551 · App. 16/217,766 · Granted Feb 9, 2021

Vehicle device separation system with telescoping piston springs

Inventors: Philip Wright (New Palestine, IN); Jayson Kahle Bopp (Fishers, IN); Stephen A. Streib (Greenwood, IN); Brian R. Kavalar (Indianapolis, IN)
Assignee: Raytheon Company
F41F3/06F41F5/00
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Quick Facts
Patent No.
US 10,914,551
App. No.
16/217,766
Granted
Feb 9, 2021
Kind
B2
Abstract

An ejector system for ejecting/separating a store, such as a weapon, from a launch platform includes a pair of spring assemblies that each include nested springs that are contained in a housing when the spring assemblies are in a compressed configuration. To separate the store from the aircraft the spring assemblies each move from the initial compressed configuration to an extended configuration, using the potential energy stored in the springs when compressed. The extension of the springs extends the springs mostly out of the spring assembly housings, extending telescoped sleeves of the spring assemblies. The extension of the spring assemblies provides a safe and steady way of separating the store from the launch platform, while having the advantages of being reusable, low cost and low weight, not producing any debris, and providing a softer push than may be produced by other separation mechanisms, such as the use of pyrotechnic devices.

Claims (52)

1. An ejector system for separating a store from a launch platform, the ejector system comprising:

spring assemblies that engage different portions of the store;

wherein the spring assemblies have a compressed position when the store is mechanically coupled to the launch platform;

wherein the spring assemblies extend from the compressed position to an extended position to separate the store from the launch platform; and

wherein each of the spring assemblies includes at least two nested springs, with spring forces from the at least two nested springs applied in series.

2. The system of claim 1 , wherein, for each of the spring assemblies, the at least two nested springs include a pair of nested springs including an inner spring and an outer spring.

3. The system of claim 2 , wherein the outer spring has a larger wire diameter than that of the inner spring.

4. The system of claim 2 , wherein the outer spring has a larger spring constant than that of the inner spring.

5. The system of claim 2 , wherein each of the spring assemblies further includes a nesting device between the inner spring and the outer spring, that mechanically engages both the inner spring and the outer spring.

6. The system of claim 5 , wherein for each of the spring assemblies the nesting device is a sleeve that changes position as the spring assembly extends from the compressed position to the extended position.

7. An ejector system for separating a store from a launch platform, the ejector system comprising:

spring assemblies that engage different portions of the store;

wherein the spring assemblies have a compressed position when the store is mechanically coupled to the launch platform;

wherein the spring assemblies extend from the compressed position to an extended position to separate the store from the launch platform;

wherein each of the spring assemblies includes at least two nested springs;

wherein, for each of the spring assemblies, the at least two nested springs include a pair of nested coil springs including an inner spring and an outer spring; and

wherein each of the spring assemblies further includes a nesting device between the inner spring and the outer spring, that mechanically engages both the inner spring and the outer spring.

8. An ejector system for separating a store from a launch platform, the ejector system comprising:

spring assemblies that engage different portions of the store;

wherein the spring assemblies have a compressed position when the store is mechanically coupled to the launch platform;

wherein the spring assemblies extend from the compressed position to an extended position to separate the store from the launch platform;

wherein each of the spring assemblies includes at least two nested springs;

wherein, for each of the spring assemblies, the at least two nested springs include a pair of nested coil springs including an inner spring and an outer spring;

wherein each of the spring assemblies further includes a nesting device that mechanically engages both the inner spring and the outer spring; and

wherein the nesting device includes a cylinder within which part of the inner spring is located, and a flange extending radially outward from an open end of the cylinder, with one end of the outer spring directly engaging the flange.

9. An ejector system for separating a store from a launch platform, the ejector system comprising:

spring assemblies that engage different portions of the store;

wherein the spring assemblies have a compressed position when the store is mechanically coupled to the launch platform;

wherein the spring assemblies extend from the compressed position to an extended position to separate the store from the launch platform;

wherein each of the spring assemblies includes at least an inner spring and an outer spring; and

wherein the spring assemblies each include telescoping sleeves, with the inner spring and the outer spring extending over different respective portions of the telescoping sleeves.

10. The system of claim 9 , further comprising feet at free ends of the spring assemblies, with the feet mechanically engaging the store prior to separation of the store from the launch platform.

11. The system of claim 10 , wherein the feet include respective pairs of arms extending outward and downward, the arms of each of the feet defining respective store-receiving recesses.

12. The system of claim 9 ,

wherein the spring assemblies include respective housings that are mechanically coupled to a rack of the launch platform; and

wherein the spring assemblies are mechanically coupled to the rack at respective forward and aft locations.

13. The system of claim 12 , wherein the rack includes retractable hooks for mechanically securing the store while the spring assemblies are in the compressed position.

14. The system of claim 9 , wherein the spring assemblies each have a stroke of at least 25 cm from the compressed position to the extended position.

15. A method of separating a store from a launch platform, the method comprising:

releasing hooks coupling the store to a rack of the launch platform; and

pushing the store away from the launch platform by extending spring assemblies that are coupled to the rack, wherein the extending includes, for each of the spring assemblies, extending nested coil springs;

wherein the spring assemblies engage different portions of the store;

wherein the spring assemblies have a compressed position when the store is mechanically coupled to the launch platform;

wherein the pushing includes the spring assemblies extending from the compressed position to an extended position to separate the store from the launch platform;

wherein for each of the spring assemblies, the nested coil springs include at least an inner spring and an outer spring; and

wherein the spring assemblies each include telescoping sleeves, with the pushing including extending the telescoping sleeves, and extending the inner spring and the outer spring over different respective portions of the telescoping sleeves.

16. The method of claim 15 , wherein the pushing includes maintaining contact between the spring assemblies and the store throughout a stroke of the spring assemblies, as the spring assemblies extend from the compressed position to the extended position.

17. The method of claim 15 , wherein the stroke is at least 25 cm.

18. The method of claim 14 , wherein the pushing includes pushing with a force that does not exceed 8900 N (2000 pounds).

19. The method of claim 15 , wherein the pushing includes pushing with feet of the spring assemblies that maintain an orientation of the store during the pushing.

20. The method of claim 14 , wherein the pushing includes pushing on forward and aft parts of the store.

21. The method of claim 15 , wherein the extending of the spring assemblies includes extending the telescoping sleeves of the spring assemblies, with the inner spring and the outer spring of each of the spring assemblies extending simultaneously.

Assignments (9)
RELEASE OF SECURITY INTEREST Recorded Mar 2, 2023
From: ALLY BANK, AS COLLATERAL AGENT
To: VERTEX AEROSPACE LLC; VECTRUS SYSTEMS CORPORATION; ADVANTOR SYSTEMS, LLC
Reel/Frame 062927/0061 →
RELEASE OF SECURITY INTEREST Recorded Mar 2, 2023
From: ROYAL BANK OF CANADA
To: VERTEX AEROSPACE LLC; VECTRUS SYSTEMS CORPORATION; ADVANTOR SYSTEMS, LLC
Reel/Frame 062927/0079 →
RELEASE OF SECOND LIEN INTELLECTUAL PROPERTY SECURITY AGREEMENTS Recorded Mar 1, 2023
From: ROYAL BANK OF CANADA
To: VERTEX AEROSPACE LLC; VECTRUS SYSTEMS CORPORATION; ADVANTOR SYSTEMS, LLC
Reel/Frame 062903/0736 →
INTELLECTUAL PROPERTY SECURITY AGREEMENT Recorded Feb 28, 2023
From: VERTEX AEROSPACE LLC; VECTRUS SYSTEMS CORPORATION; ADVANTOR SYSTEMS, LLC; DELEX SYSTEMS, INCORPORATED; HIGGINS, HERMANSEN, BANIKAS, LLC
To: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
Reel/Frame 062886/0877 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 18, 2022
From: RAYTHEON COMPANY
To: VERTEX AEROSPACE LLC
Reel/Frame 059436/0396 →
SECURITY AGREEMENT Recorded Dec 10, 2021
From: VERTEX AEROSPACE, LLC
To: ALLY BANK, AS COLLATERAL AGENT
Reel/Frame 058957/0428 →
SECOND LIEN SECURITY AGREEMENT Recorded Dec 7, 2021
From: VERTEX AEROSPACE LLC
To: ROYAL BANK OF CANADA
Reel/Frame 058342/0027 →
FIRST LIEN SECURITY AGREEMENT Recorded Dec 7, 2021
From: VERTEX AEROSPACE LLC
To: ROYAL BANK OF CANADA
Reel/Frame 058342/0046 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 17, 2018
From: WRIGHT, PHILIP; BOPP, JAYSON KAHLE; STREIB, STEPHEN A.; KAVALAR, BRIAN R.
To: RAYTHEON COMPANY
Reel/Frame 047928/0677 →