Aircraft with removable structural payload module

• US 5,975,464 A
• Filed: 09/22/1998
• Issued: 11/02/1999
• Est. Priority Date: 09/22/1998
• Status: Expired due to Fees

• Current Assignee: SCI Acquisition Company, LLC
• Original Assignee: Scaled Composites, Inc. (Berkshire Hathaway Incorporated)
• Inventors: Rutan, Elbert
• Primary Examiner(s): ELDRED, JOHN W
• Application Number:
  US09/158,186
• Time in Patent Office: 406 Days
• Field of Search: 244/120, 244/118.2, 244/137.1, 244/2
• US Class Current: 244/120
• CPC Class Codes: B64C 2211/00 Modular constructions of airplanes or helicopters
• CPC Class Codes: B64C 39/02 characterised by special use

Abstract

An aircraft includes a forward fuselage segment, an aft fuselage segment, a wing structure supported from the aft fuselage segment, a tail structure supported from either the aft fuselage segment or the wing structure, and an engine supported from either the aft fuselage segment or the wing structure. A payload module is disposed between and connects the forward fuselage segment and the aft fuselage segment, so as to form the structural attachment between the forward fuselage segment and the aft fuselage segment. The payload module is disconnectable from the forward fuselage segment and the aft fuselage segment such that the forward fuselage segment and the aft fuselage segment are not connected to each other when the payload module is disconnected from the forward fuselage segment and the aft fuselage segment.

Claims

1. An aircraft, comprising:

a forward fuselage segment;

an aft fuselage segment;

a wing structure supported from the aft fuselage segment;

a tail structure supported from at least one of the aft fuselage segment and the wing structure;

an engine supported from one of the aft fuselage segment and the wing structure; and

a payload module disposed between and connecting the forward fuselage segment and the aft fuselage segment, the payload module forming the structural attachment between the forward fuselage segment and the aft fuselage segment, and further being disconnectable from the forward fuselage segment and the aft fuselage segment such that the forward fuselage segment and the aft fuselage segment are not connected to each other when the payload module is disconnected from the forward fuselage segment and the aft fuselage segment.

2. The aircraft of claim 1, wherein the center of gravity of the aircraft lies within the payload module.

3. The aircraft of claim 1, wherein the aerodynamic neutral point lies within the payload module.

4. The aircraft of claim 1, further including

at least one wing extension, each wing extension being mounted to an end of the wing structure.

5. The aircraft of claim 1, further including

a canard structure supported from the forward fuselage segment.

6. The aircraft of claim 5, further including

at least one canard extension, each canard extension being mounted to an end of the canard structure.

7. The aircraft of claim 1, wherein

the forward fuselage segment has a forward fuselage segment skin,

the aft fuselage segment has an aft fuselage segment skin, and

the payload module has a payload module skin, and wherein the payload module skin is structurally attached to the forward fuselage segment skin and to the aft fuselage segment skin when the payload module is connected between the forward fuselage segment and the aft fuselage segment.

8. The aircraft of claim 1, further including

at least one forward fuel tank located in the forward fuselage segment, and

at least one aft fuel tank located in one of the aft fuselage segment and the wing structure.

9. The aircraft of claim 1, wherein the payload module includes at least one payload module services conduit therethrough, and further including

a forward services interconnect between the forward fuselage segment and the at least one payload module services conduit, and

an aft services interconnect between the aft fuselage segment and the at least one payload module services conduit.

10. The aircraft of claim 1, wherein the payload module comprises a payload selected from the group consisting of a communications antenna, an air sampling device, a reconnaissance device, a launchable vehicle, and a payload module fuel tank.

11. The aircraft of claim 10, wherein the payload module has a payload module skin, and at least a portion of the payload is mounted externally to the payload module skin.

12. An aircraft, comprising:

a forward fuselage segment having a forward fuselage segment skin;

an aft fuselage segment having an aft fuselage segment skin;

a wing structure supported from the aft fuselage segment;

a tail structure supported from at least one of the aft fuselage segment and the wing structure;

an engine;

an engine support disposed between and connecting the engine and one of the aft fuselage segment and the wing structure;

a payload module disposed between the forward fuselage segment and the aft fuselage segment and having a payload module skin;

a disconnectable forward module attachment disposed between the forward fuselage segment skin and the payload module skin; and

a disconnectable aft module attachment disposed between the aft fuselage segment skin and the payload module skin.

13. The aircraft of claim 12, wherein the forward module attachment comprises

a forward attachment strap extending circumferentially around the forward fuselage segment and overlapping the forward fuselage segment skin and the payload module skin, and

a plurality of removable fasteners affixing the forward attachment strap to the forward fuselage segment skin and to the payload module skin.

14. The aircraft of claim 12, wherein the engine support connects the engine to the aft fuselage segment, and wherein the engine support comprises

an internal bracing structure within the aft fuselage segment, and

a pylon structure extending through the aft fuselage segment skin, the pylon structure being affixed at a first end to the internal bracing structure and affixed at a second end to the engine.

15. The aircraft of claim 12, wherein the forward fuselage segment skin, the aft fuselage segment skin, and the payload module skin each comprises a composite material.

16. The aircraft of claim 12, wherein the forward fuselage segment skin, the aft fuselage segment skin, and the payload module skin each comprises an outer layer of a first composite material, an inner layer of a second composite material, and a core bonded between the outer layer and the inner layer.

17. An aircraft, comprising:

a forward fuselage segment;

a canard structure supported from the forward fuselage segment. an aft fuselage segment;

a wing structure supported from the aft fuselage segment, the wing structure including a left wing and a right wing;

a tail structure supported from the wing structure, the tail structure comprising

a left boom supported from the left wing,

a left vertical tail supported from the left boom,

a right boom supported from the right wing, and

a right vertical tail supported from the right boom;

at least one engine supported from the aft fuselage segment; and

a payload module disposed between and connecting the forward fuselage segment and the aft fuselage segment, the payload module forming the structural attachment between the forward fuselage segment and the aft fuselage segment, and further being disconnectable from the forward fuselage segment and the aft fuselage segment such that the forward fuselage segment and the aft fuselage segment are not connected to each other when the payload module is disconnected from the forward fuselage segment and the aft fuselage segment.

18. The aircraft of claim 17, wherein the center of gravity of the aircraft and the aerodynamic neutral point of the aircraft each lie within the payload module.

19. The aircraft of claim 17, further including

at least one wing extension, each wing extension being mounted to an end of the wing structure.

20. The aircraft of claim 17, further including

at least one canard extension, each canard extension being mounted to an end of the canard structure.