Author: claimsbot

1. An aircraft comprising:
two parallel fuselages (2G, 2D) spaced symmetrically apart with respect to a longitudinal mid-plane (L-L);
a front lower wing (9) that is symmetric with respect to said longitudinal mid-plane (L-L) and supports the front lower parts of said fuselages (2G, 2D);
a rear upper wing (10) that is symmetric with respect to said longitudinal mid-plane (L-L) and is supported by the rear upper parts of said fuselages (2G, 2D); and
a propulsion system (11, 12, 13),
wherein:
at least the symmetric external parts (9G, 9D) of said front lower wing (9) have a sweep forward (\u03a6a);
the lift generated by said rear upper wing (10) is greater than the lift generated by said front lower wing (9);
said rear upper wing (10) is in direct contact with the rear upper parts of said fuselages (2G, 2D); and
said propulsion system (11, 12, 13) comprises at least one turboprop engine having at least one propeller and is carried by the internal part (10I) of said rear upper wing (10), the axis (l-l) of said propulsion system lying on said longitudinal mid-plane (L-L).
2. The aircraft as claimed in claim 1,
wherein the lift generated by said rear upper wing (10) represents at least approximately 60% of the overall lift generated by said aircraft, so that the lift generated by said front lower wing (9) represents at least approximately 40% of said overall lift.
3. The aircraft as claimed in claim 1,
and which comprises four sets of landing gear (5G, 5D, 7G, 7D) distributed at the front and rear of the two fuselages (2G, 2D) respectively.
4. The aircraft as claimed in claim 1,
wherein said propulsion system (11, 12, 13) comprises at least one turboprop with at least one pusher propeller (12) positioned behind said rear upper wing (10).
5. The aircraft as claimed in claim 1,
wherein said propulsion system (11, 12, 13) comprises at least one turboprop having at least one tractor propeller (13) positioned in front of said rear upper wing (10).
6. The aircraft as claimed in claim 4,
wherein said turboprop with at least one pusher propeller (12) and said turboprop with at least one tractor propeller (13) are enclosed in a common cell (11) borne by said rear upper wing (10).
7. The aircraft as claimed in claim 1,
wherein said rear upper wing (10) has a sweep forward (\u03a6r).
8. The aircraft as claimed in claim 7,
wherein said tractor propeller (13) is positioned in front of said rear upper wing (10) so as not to risk damaging it if any debris from said tractor propeller (13) or from the turboprop that drives it is thrown out.
9. The aircraft as claimed in claim 5,
wherein, facing said tractor propeller (13), each of said fuselages (2G, 2D) has a partially pressurized chamber (17G, 17D).
10. The aircraft as claimed in claim 9, in which each fuselage (2G, 2D) comprises a passenger cabin (4G, 4D) and a rear landing gear bay (8G, 8D) for said rear landing gear (7G, 7D),
wherein each partially pressurized chamber (17G, 17D) is located between the corresponding passenger cabin (4G, 4D) and the corresponding rear landing gear bay (8G, 8D).
11. The aircraft as claimed in claim 10, in which each passenger cabin (4G, 4D) is air-conditioned by a stream of air-conditioning air and has a discharge valve (22) capable of discharging said stream of air-conditioning air to outside said aircraft,
wherein said discharge valve (22) from said cabin can be made to close and to open and wherein the following are provided:
a communication (20) allowing a controlled flow of air between said passenger cabin (4G, 4D) and said chamber (17G, 17D), it being possible to instigate the opening and closure of said communication (20), and
an additional operable discharge valve (23) positioned in said chamber (17G, 17D) and capable of placing this chamber in communication with the outside of the aircraft.
12. The aircraft as claimed in claim 11,
wherein a safety device (21) guarding against overpressure is provided between said chamber (17G, 17D) and said rear landing gear bay (8G, 8D).
13. The aircraft as claimed in claim 1,
wherein the internal part (9I) of said front lower wing (9) has the shape of a circumflex accent that is symmetric with respect to said longitudinal mid-plane (L-L) and has the same sweep forward (\u03a6a) as said external parts (9G, 9D) of said front lower wing (9).
14. The aircraft as claimed in claim 13,
wherein the trailing edge of said internal part (9I) comprises a central cut-out (16).
15. The aircraft as claimed in claim 1,
wherein the internal part (9I) of said front lower wing (9) has the shape of a circumflex accent that is symmetric with respect to said longitudinal mid-plane (L-L) and has a sweep back that is the opposite of the sweep forward of said external parts (9G, 9D) of said front lower wing (9).

The claims below are in addition to those above.
All refrences to claim(s) which appear below refer to the numbering after this setence.

1. A motor vehicle, having a motor vehicle carcass body, and with a luggage area having a bottom and with two facing side panels, with a plurality of spaced apart elongated functional tracks disposed in each of the side panels, the functional tracks being arranged at least one of horizontally and vertically in the side panels, the functional tracks further being mounted flush to inside surfaces of the side panels, and being connected by support sections with parts of the motor vehicle carcass body, wherein the functional tracks are formed by profile units, that are connected by support sections (11) to carcass body parts (10).
2. The motor vehicle according to claim 1, further comprising fastening elements operably configured to be insertably received in and affixed to the functional tracks.
3. The motor vehicle according to claim 1, wherein the functional tracks (5 to 7) are arranged in corresponding pairs disposed opposite one another in the side panels (4).
4. The motor vehicle according to claim 1, wherein segmenting parts (8), which are at least one of vertically positionable and horizontally positionable, are provided, which are equipped with fastening elements matched to the fastening functions of the functional tracks (5 to 7).
5. The motor vehicle according to claim 1, wherein covering parts (8), which are at least one of vertically positionable and horizontally positionable, are provided, which are equipped with fastening elements matched to the fastening functions of the profile rails (5 to 7).

1. A method of constructing a widget environment, the method comprising:
responsive to identifying that an application programming interface (API) that is not executable in a current device is called, converting the API into an API call in a Web service format;
transmitting the API call in the Web service format to a remote device in which the API is executable; and
receiving a result obtained from the API call being executed in the Web service format in the remote device.
2. The method of claim 1 further comprising:
calling the API; and
determining whether the API is executable in the current device.
3. The method of claim 2, wherein determining whether the API is executable in the current device comprises:
comparing the API with a function of a Web runtime included in the current device; and
determining whether the API is executable in the current device.
4. The method of claim 3 further comprising:
responsive to determining that the API is executable in the current device, executing the API in the current device.
5. The method of claim 1 further comprising:
receiving an address of the remote device in which the API is executable; and
wherein transmitting the API call in the Web service format to the remote device in which the API is executable comprises:
transmitting the API call in the Web service format to the remote device according to the address of the remote device.
6. The method of claim 5, wherein the address of the remote device is a uniform resource locator (URL).
7. The method of claim 1, wherein transmitting the API call in the Web service format to the remote device in which the API is executable comprises:
transmitting the API call in the Web service format to the remote device in which the API is executable in a HTTP request format.
8. The method of claim 7, wherein receiving the result obtained from the API call being executed in the Web service format in the remote device comprises:
receiving the result obtained from the API call being executed in the Web service format in the remote device in a HTTP response format.
9. The method of claim 1 further comprising:
converting the result obtained from the API call being executed in the Web service format into a result obtained by executing the API.
10. The method of claim 1, wherein the API call in the Web service format is a representational state transfer (REST) API call.
11. The method of claim 1, wherein the API is a Bondi API.
12. An apparatus for constructing a widget environment, the apparatus comprising:
an application programming interface (API) converting unit configured to, responsive to identifying that an API that is not executable in the apparatus for constructing the widget environment is called, convert the API into an API call in a Web service format;
a transmitting unit configured to transmit the API call in the Web service format to a remote device in which the API is executable; and
a receiving unit configured to receive a result obtained from the API call being executed in the Web service format in the remote device.
13. The apparatus of claim 12 further comprising:
an API switching unit configured to, responsive to identifying that the API is called, determine whether the API is executable in the apparatus for constructing the widget environment.
14. The apparatus of claim 13, wherein the API switching unit is further configured to compare the API with a function of a Web runtime included in the apparatus for constructing the widget environment and determine whether the API is executable in the apparatus for constructing the widget environment.
15. The apparatus of claim 14, wherein the Web runtime executes the API in response to determining that the API is executable in the apparatus for constructing the widget environment.
16. The apparatus of claim 12, wherein the receiving unit is further configured to receive a URL of the remote device in which the API is executable and wherein the transmitting unit is further configured to transmit the API call in the Web service format to the remote device according to the URL of the remote device.
17. The apparatus of claim 12, wherein the transmitting unit is further configured to transmit the API call in the Web service format to the remote device in which the API is executable in a HTTP request format.
18. The apparatus of claim 17, wherein the receiving unit is further configured to receive the result obtained from the API call being executed in the Web service format in the remote device in a HTTP response format.
19. The apparatus of claim 12, wherein the API converting unit is further configured to convert the result obtained from the API call being executed in the Web service format into a result obtained by executing the called API.
20. The apparatus of claim 12, wherein the API call in the Web service format is a REST API call.

The claims below are in addition to those above.
All refrences to claim(s) which appear below refer to the numbering after this setence.

1. A process for making a stretch composite from an extensible substrate, said process comprising the steps of:
a. providing a first extensible substrate;
b. providing an application device, said device including at least one patterned print roll;
c. printing one or more elastomeric compositions by means of said patterned print roll, said compositions having a melt viscosity of from about 1 to about 150 Pa\xb7s, measured at 175\xb0 C. and 1 s\u22121 strain rate, an elasticity of at least about 50 Nm at 20\xb0 C., and a percent set of less than about 20%, onto said substrate thereby forming one or more intermediate structures;
d. incrementally stretching one or more portions of the intermediate structures to permanently elongate the substrate in the portions; and
e. converting the elastomeric composition into elastomeric members forming one or more elasticized regions of the substrate;
wherein said elastomeric composition comprises a thermoplastic elastomer and a phase change solvent having the general formula:
R\u2032\u2212Ly\u2212(Q\u2212Lx)n-1\u2212Q\u2212Ly\u2212R;\u2003\u2003(I)
R\u2032\u2212Ly\u2212(Q\u2212Lx)n\u2212R;\u2003\u2003(II)
R\u2032\u2212(Q\u2212Lx)n\u2212R;\u2003\u2003(III)
R\u2032\u2212(Q\u2212Lx)n-1\u2212Q\u2212Ly\u2212R;\u2003\u2003(IV)
R\u2032\u2212(Q\u2212Lx)n-1\u2212Q\u2212R; or\u2003\u2003(V)

a mixture thereof;

wherein Q is a para-ring substituted difunctional aromatic moiety, wherein the substitutions are in the 1,4 positions; L is CH2; R and R\u2032 are the same or different and are independently selected from H, CH3, COOH, CONHR1, CONR1R2, NHR3, NR3R4, hydroxy, or C1-C30 alkoxy; wherein R1, R2, R3 and R4 are the same or different and are independently selected from H or linear or branched alkyl from C1-C30; x is an integer from 1 to 30; y is an integer from 1 to 30; and n is an integer from 3 to 7.
2. The process of claim 1 wherein the converting comprises one or more processes selected from the group consisting of crosslinking, curing, cooling, pressing, and combinations thereof.
3. The process of claim 1 wherein the elastomeric compositions have a stress relaxation of less than about 20%.
4. The process of claim 3 wherein the elastomeric compositions comprise thermoplastic elastomers selected form the group consisting of styrenic block copolymers, metallocene-catalyzed polyolefins, polyesters, polyurethanes, polyether amides, and combinations thereof.
5. The process of claim 1 wherein the one or more elasticized regions are disposed in an absorbent article and the regions are selected from the group consisting of an elasticized waist region, an elasticized cuff region, an elasticized side panel, an elastic ear portion, an elasticized outercover, an elasticized topsheet, a fastener system, and combinations thereof.
6. The process of claim 1 wherein prior to incremental stretching said process further comprises a step of laminating a second substrate to the first extensible substrate with the one or more elastomeric members sandwiched between the first and second substrates.
7. The process of claim 1 wherein the elastomeric members are different in a characteristic selected from the group consisting of compositions, add-on levels, shape, pattern, and combinations thereof.
8. The process of claim 1 wherein the elastomeric members are rectilinear or curvilinear, and at least two of the elastomeric members are non-parallel with respect to each other.
9. The process of claim 1 wherein the one or more elasticized regions are adjacent or at least partially overlapping.
10. The process of claim 1 wherein said phase change solvent has a phase change in a temperature range from about 40\xb0 C. to about 250\xb0 C.
11. The process of claim 1 wherein the incrementally stretched portion of the stretch composite exhibits the following properties in at least one direction:
a directional elasticity of from about 5 Nm to about 400 Nm;
a directional percent set of less than about 20%; and
a directional stress relaxation of less than about 30% after 2 minutes at room temperature and 75% strain.
12. The process of claim 1 wherein Q is selected from the group consisting of terephthalic, naphthalic, phenolic, phenyl and biphenyl having the following formulae:
and mixtures thereof.
13. The process of claim 12 wherein Q is selected from terephthalic having the following formulae:
and mixtures thereof.
14. The process of claim 12 wherein Q is selected from naphthalic having the following formulae:
and mixtures thereof.
15. The process of claim 1 wherein Q is substituted on the aromatic ring with one or more substituents selected from H, C1-C30 alkyl, COOH, CONHR5, CONR5R6, NHR7, NR7R8, hydroxy, C1-C30 alkoxy, SO3H, or halogen; wherein R5, R6, R7 and R8 are the same or different and are independently selected from H or linear or branched alkyl from C1-C30.